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NASA CONTRACTOR REPORT 166362 1102-210315 (11ASA-CL-166362) 1NVBS-T j1411T!ON OF 1RBLATION L's E !FUIL-SCLLE AND CO21 ITWEEN FIVT II- SCALB WIND TUNNEL T33TS OF A BELL U ncia j 113LICOPTER T;E.XTPON OODEL 222 Final 2eiloLt 28567 V A01 (43/05 (Bell Helicopter Co.) 40 1 p 3C ZI 1810 Investigation of Correlation Between Full- Scale
and Fifth-Scale Wind Tunnel Tests of a Bell
Helicopter Textron Model 222 co
Patrick K. Squires
1^ CEII
Bell Helicopter Textron
CONTRACT NAS2-10773 June
w Asn
NASA CONTRACTOR REPORT 166362 Investigation of Correlation Between Full-Scale
and Fifth-Scale Wind Tunnel Tests of a Bell
Helicopter Textron Model 222 Patrick K. Squires Bell Haliccpter Textron P.O. Box 482 Fort Worth, Texas 76101 Prepared for Ames Research Center under Contract NAS2-10773
NASA
National Aeronautics and Space Administration Ames Research Center Moffett Field Calfornia 04035 NASA CONTRAaOR REPORT 166362 INVESTIGATION OF CORRELATION BETWEEN FUIoL-SCALE AND VIVTH—SCALE WIND TUNNEL TZSM OF A BELL HELICOPTER TEXTRON MODEL 222 Patrick K. Squires Belk, Helicopter Textzon, Ina.
Fort Worth, Texas CONTRACT NA82--10775
NASA
INVESTIGATION OF CORRELATION BETWEEN FULL-SCALE AND FIFTH-SCALE WIND TUNNEL TESTS OF A BELL HELICOPTER TEXTRON MODEL 222 By Patrick K. Squires June 1982 Distribution of this report is provided in the interest of information exchange. Responsibility for the contents resides in the author or organization that prepared it.
J. t
CR - 166362 Prepared under Contract No. NAS2--10773 by BELL HELICOPTER TEXTRON INC.
Fort Worth, Texas For AMES RESEARCH CENTER NATIONAL AERONAUTICS AND SPACE ADMINISTRATION rain .y i°ym^3 uC7DG 9 G
TABLE OF-CONTENTS
Pa e
LIS T OF FIGURES ....................................... v
OF LIST TABLES ........................................
xi LIST SYMBOLS .......................................
SUMMARY . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ! . . . . . . . . . . . #.
INTRODUCTION .....................................
1. 2
Background ............ ..
1.2 Correlation Between Full,-scale And Fifth-
1.3
2. DATA REVIEW
3.
4.1
5. DESIGN AND FABRICATION OF FIFTH-SCALE SUPPORT
SYSTEM
5.1 Requirement for a Replica Mounting System ... 10
5.2 Design and Fabrication of Mounting
6.1 Facilities and Equipment ....................
6.4 Test Dynamic Pressure....................... ............
6.5 Three-Point Mounting System Tare Rans .......
6.7 Comparison Runs in LSWT 550 Configuration ... 15
6.9 Component Buildup on Three-Point Mount ......
iii TABLE OF CONTENTS (Conc luded) 6.16 EValuatiox of Roughness and Protuberances ...
y
l.t." lJ
.1 Co mp ari son o: ^ $ ........... 1 7 : f ca e R esu,l
( d` ^ ^ ^ y ^ l y a ^
7.2 Cl'W^4^ Compari son oy{a: e s . ...... . ...... . . .
d-Ox.4 Tar 17
7.3 Compariso n of Vifth-Sca le and Fu ll - Stale
o the Three-P oint
of 7.4 Tare Interference the Three- and n
7.5
Comparison of Fifth-Scale anO. . n.1. =.kale
8. CONCD^ .l 'S IQ^{l'yS^ AND RECQ END.A.TI aN^ . ,.. „ , - , . ,. , . 23
/ i 8 .1 . . . . . . . . . o a ., ^c ^i . o . .. .y ^ ^ a a s 2 12 ^.. ions .
* y / y . 2 Re c 8 ommen dati ons Re c ^JA^L!, A.l-^.y J ,dations . . . . . . . . . . 24 Off` RE-FE:RENCES 9. LIST ............ > , , , , 25
APPENDIX. A - LSWT 630 Tabulated Data A-2
............................ E -
APPENDIX B - Run Schedules 1
iv LIST OF FIGS Figure Pa e Correlation Improvement for Helicopter Drag Characteristics in Pitch ......
•rr ♦••.. 26
2 Correlation Improvement for Helicopter Drag Characteristics in Yaw ••
♦•..• t•••• ♦.♦ r 27
Comparison of Prototype and Fifth-Scale M o del t • • • • • r • • • ♦ • • • • ♦ • . t • • • ♦ . . . r . . • . ♦ . . • . • . 28 Original Comparison of Lift Characteristics in Pitch for Basic Fuselage original Comparison of Drag Characteristics in Pitch for Basic Fuselage .......•.... ♦..♦. 30 6 Original Comparison of Pitching Moment Characteristics in Patch for Basic Fuselage ................
original Comparison of Lift Characteristics in Pitch for Helicopter ..............r......
original, Comparison of Drag Characteristics 9 original Comparison of Patching Moment Characteristics in Patch for Helicopter .....
10 Original. Comparison of Side Force 11 original Comparison of Drag Character- istics in Yaw for Helicopter ................ 36.
12 original Comparison of Yawing Moment Contour Discrepancies of M222 Model.
(side View) ...• ................ •.•..••....
14 Contour Discrepancies of M222 Model.
Cowling .....................................
15 Schematic Drawing of 40 x 80 Mounting .......
schematic Drawing of Single Strut Mounting .. 41 v LIST OF FIGUES ( Continued) P awe
17 Three--Point Support Configuration, for Pitch
and Yaw Run Testing fth-Scale M222 Model installed on Single
is F
i 9^j S upport . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Fifth -Scale M222 Model Installed Inyerted with image System ..............................». 44 20 Fifth-Scale M222 Model on Three-Point Support 21 Fifth-Scale M222 Model on Three-Point Support ......................
22 Pictorial Nomenclature 47
23 Comparison of Fifth--Scale Lift Character-
in 24 Comparison of Fifth-Scale Drag Character- ' Comparison of Fifth-Scale Pitching Moment Characteristics in Pitch of Basic Fuselage .. 66 26 Comparison of Fifth-Scale Lift Character-
27 Comparison of Fifth - Scale Drag Character-
istics in Pitch for Helicopter ..............
28 Comparison of Fifth-Scale Pitching Moment Characteristics in Pitch for Helicopter . .. 69 29 Comparison of Fifth-Scale Side Force 30 Comparison of Fifth-Scale Drag Character- Comparison of Fifth-Scale Yawing Moment
Comparison of Tare Lift Characteristics
in Pitch for Three-Point Mount .........^..,. 7e A LIST OF FIGbWs (Continued) Pa e 33 Comparison of Tare Drag Characteristics in Patch for Three-Point Mount ..............
34 Comparison of Tare Pitching Moment Char- acteristics in Pitch Xor Three-Point Mount ,, 5 Comparison of Tare Side Force Character-
:3 a. comparison of Tare Drag Characteristics
7 Comparison of Tare Yawing Moment Char- Full/Fifth-Scale Comparison of Lift Char-
39 Full/Fifth -scale Comparison of Drag Char-
40 Full/Fifth -Scale Comparison of Pitching
Moment Characteristics in Pitch for Basic Fuselage
41 Full/Fifth -Scale Comparison of Lift Char-
acteristics in Pitch for Basic Fuselage Full/Fifth-Scale Comparison of Drag Char- acteristics in Pitch for Basic Fuselage WithWings ..................................
43 Full/Fifth-Scale Comparison of Pitching Moment Characteristics in Pitch for
44 Full/Fifth-Scale Comparison of Lift Char-
acteristics in Pitch for Helicopter Without
Scale Comparison of Drag Char-
45 Full/Fifth-- acteristics in Pitch for Helicopter Without Wings .......................................
-Scale Comparison of Pitching
46 Full/Fifth Moment characteristics in Pitch for vii
LIST (Co^itinued)
of FIGURES
Pa e
Full/Fifth-Scale Comparison of Lift Char-
r co pte 88
acteris ti cs in Pitch fo Heli r . ........
48 Full/Vifth-Scale Comparison of Drag Char-
Full/Fifth-scale Comparison of Pitching Moment characteristics in Pitch for elicopter ..................................
H 50 Full/Fifth--Scale comparison of Side Force Characteristics in Yaw Helicopter .......
for 91
51 Full/Fifth-Scale Comparison of Drag Char- Full/Fifth-Scale Comparison of Yawing Moment Characteristics in Yaw for Helicopter
53 Full/Fifth--Scale Comparison of Lift Char-
acteristics in Pitch for Eelicopter Without
54 Full/Fifth-Scale CoSypari on of Drag Char-
acteristics in Pitch for Helicopter Without TailRotor 55 Full/Fifth-Scale Comparison of Pitching Moment Characteristics in Pitch for Full/Fifth-Scale Comparison of Lift Char-
acteristics in Pitch for Helicopter with
57 Full/Fifth--Scale Comparison of Drag Char- acteristics in Pitch for Helicopter with Landing Gear Doors Open 58 Full/Fifth-Scale Comparison of Pitching Moment Characteristics for Helicopter 59 Tare and Interference Corrections to Lift Characteristics in Pitch Three-Point for viii.
LIST bF FIOURES (Continued) Pa ge Tare and Interference Corrections to brag in Pitch for Three-foist MI Mount M ount . . . . . . . . . . . . . . . . .. . . . . . i . R a f ; i t f • 4 ; ; 9 ; d 1 0 1 61 Tare and Interference Corrections to Pitching Moment Characteristics in Pitch for Three-Point Mount . . . . . . . . . . ; . . .
f ; ; . R . a ; P . . . s . • t . . f . . . . • . 102 62 Tare and Interference Corrections to Side Force Characteristics in Yaw for Three-Point 63 Tare and Interference Corrections to Drag Characteristics in Yaw for Three-Point 64 Tare and Interference Corrections to Yawing Moment Characteristics in Yaw for Three--Point Mount . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . « . . . . .
55 Full/Fifth-Scale Comp arison of Lift Char- 66 Full/Fifth-Scale Comparison of Drag Char- 67 Fuld,/Fifth-Scale Comparison of Pitching 68 Full/Fifth--Scale Comparison of Lift Char- acteristics of Horizontal Stabilizer in .......................................
Pitch 109 69 Full/Fifth-Scale Comparison of Drag Char- acteristics of Horizontal Stabilizer in Pitch .......................................
i10 Full/Fifth)-Scale Comparison of Pitching Moment Characteristics of Horizontal Stabilizer in Pitch ......................... ill 71 Full/Fifth-Scale Comparison of Lift, Drag, and Pitching Moment Characteristics of 72 Full/Fifth--Scale Comparison of Lift, Drag, and Pitching Moment Characteristics of Endplates in Pitch ................... :... 113 ix LIST OF '171GUFX-S (Concluded) P~age.
73 Summary Comparison of Lift Characteristics in Pitch for Basic 74 Summary Comparison of Draj Characteristics Summary Comparison of Pitching Moment Char- 76 Summary Comparison of Lift Characteristics 77 Summary Comparison of Drag Characteristics in Pitch for Helicopter .....................
78 Summary Comparison of Pitching Moment Summary Comparison of Side Force Char- acteristics in Yaw for Helicopter ...........
80 Summary Comparison of Drag Character- istics in Yaw for Helicopter 81 Summary Comparison of Yawing Moment Char- acteristics in Yaw x LIST of TABLES Table Pa e Comparison of Reynolds Numbers for Full- Scale and Fifth-Scale Tests .................
Ix Run Schedule for Low Speed Wind Tunnel III Configuration Nomenclature Comparison ....... '130 B-1 Run Schedule for Low Speed Wing Tunnel Test .................................... B-2 B-11 Run Scb,ed'ule for Full-Scale Test ............ B-4
Xi
LIST or S)MOLS
drag/dynamic pressure wind tunnel axis (positive
D/a
aft) , : V
L/q lift/dynamic pressure, wind tunnel axis (positive
lap) , ft2
PM/q pitching moment/dynamic pressure wind tunnel axis
(positive nose lap), ft3
rolling moment/dynamic pressure wind tunnel axis
(positive right), ft3 dynamic pressure, lb/ft2
side force/dynamic pressure wind tunnel axis (positive
right), ft2
yawing moment/dynamic pressure wind tunnel axis (posi-
tive nose right) ft3 .
angle of attack (positive nose up), deg
yaw angle (positive nose right), deg
xii
SMARM" An experimental investigation has been pe.,,,..formed to investigate reasons for lack of correlation between d "ea from a fifth-scale wind tunnel, test of the Bell Helicopter Textron Model ',322 (Ylought LSWT 550 November 1977) and a full-scale test of the Model 222 prototype in the NASA Ames 40-by 80-foot. tunnel., (November 1977) This investigation centered around a carefully designed fifth-scale wand tunnel test (Vought LSWT 630 November 1081) of an accurately contoured model of the Model 222 proto- type mounted on a replica of the full-scale mounting system.
Figures 1 and 2 show the improvement in correlation for drag characteristics in pitch wid yaw with the fifth-scale model mounted on -the replica system. interference between the model and, mounting system was identified as a significant effect and was concluded to be a primary cause of the lack of Correlation in the earlier tests. This Conclusion is supported by the results presented in this report. The program documented herein was sponsored by contract (XAS2-10773) with the National.
Aeronautics and Space Administration, Ames Research Center.
The Technical.Monitor was Dr, ,a:;lliam Warmbrodt.
1. INTRODUCTXON The Bell Helicopter Textron Model 222 Light Executive Twin, pro- totypes began flight test development in 1576. actual perform- ante was less than predicted ba r analysis based on drag data measured during extensive fifth-scale wind tunnel tests. This
performance difference called into question the use of fifth-
scale wind tunnel tests to provide airframe drag data for per- formance prediotion.
1.1 BACKGROUND in a joint effort during the fall of 1577, NASA. Ames and BTIT conducted two wind tunnel, tests of the nodal 222 directed to- ward answering this Vestion. The first test, in the 7- by 10-foot low speed wind tunnel at Fought Ae-ronautics Corporation., during November of 1,577, involved a fifth-scale model. The second test also in November of 1577 was conducted in the 40- by 50-foot wind tumel. at NASA Ames .Research, Center using an actual. Model, 222 prototype which was removed from flight status, modified for mounting in the test section, and Later returned to f`?ight status. References 1 and 2 are reports of the fifth- scale test and the full-scale tests respectively. Tables B-x and B-11 of the Appendix present the run schedules of these tests. Figure 3 shows the two models in a side-by-side compar- ison. One objective of these tests was to provide proof that baseline aerodynamic data obtained in the full-scale test of an actual prototype airframe would correlate well with tests of an accurate model of the prototype, and thereby, validate the method of using fifth-scale tests to predict helicopter airframe aerodynamic characteristics. Secondary objectives were to document the validity of using fifth-scale testing to investi- gate the aerodynamic effects (particularly drag) of the compo- nents of the helicopter airframe and to evaluate the ef'f'ect of modifications intended to reduce drag. To accomplish these
objectives, a number of configurations were tested. These
configurations ranged from a basic fuselage, with all major components except the fin removed, to the complete helicopter shown in Figure 3. While data on all six components of force and moment were taken, the major thrust bf the tests was to investigate drag.
1.2 CORRELATION BETWEEN FULL-SCALE AND ORIGINAL FIFTH-SCALE ,(LSWT 5S0) TESTS The correlation between full-scale and fifth-scale data from these two tests was rather disappointing. Longitudinal data for both the basic fuselage and complete helicopter showed large discrepancies. Lateral data showed good agreement in side force and yawing moment but compared very poorly in drag.
Figures 4 through, 6 compare lift, drag t and patching moment characteristics of the basic fuselage in pitch for both the
fifth-scale test (LS'WT 550) and NASA Ame s 40 - -
the • by 80 foot
(
te st f ul lscale). The basic fu sel age configuration as defined
in this investigation included the
fuselage, cowling (with inlets, exhausts and cooling screens closed), nose year door olosed, tail rotor hub, prod ucti o n tail rotor gearbox fairing,
exhaust ejector fairing and vertical fin with 10 inch cap. The
data in these figures are corrected by subtracting tare and interference values obtained i test n the following ways. For
c o
LsWT 550, T&I rrections originated wit h a p revious test of
the Model 222 (LSW',i;` 435 November 1973) . The only
corrections
available for the full scale test were the usual static tares
and wind-on taresmeasured for the support system alone.
Figures 7 through. 9 compare lift, drag, and pitching' moment of
the complete helicopter in pitch for the two tests. The com-
plete helicopter configuration as defined in this investigation
was identical to the flying prototype except that inlets and exhausts were closed and the main and tail rotor blades were removed. Minor, configuration differences between the prototype and the fifth-scale model of LS'WT 550 are discussed in Section 2.1. Figures 10 through 12 compare side force, drag, and vawina moment of the comp lete helico pter in craw for both tests.
Figure 4 shows that the Lift curve slope for the LSWT 550 data is approximately two times the full-scale value and the fifth-
scale angle of zero lift is some 7 degrees lower. Figure 7
which compares lift data for the complete helicopter shows better agreement at nominal angles of attack (--4 degrees to +6 degrees) where slopes are essentially equal and angles of zero
lift differ by only 2 degrees. The full-scaJa and fifth-scale
data show considerable divergence, however, at very high angles of attack. Figure 5 compares drag of the basic fuselage for the two tests. The drag at an angle of attack of zero degrees differs by approximately 2 square feet and the angle of attack for minimum drag is quite different. Figure 8, which compares drag for the complete helicopter, shows better agreement in the location of the drag bucket, but the drag at zero angle of attack differs by almost 4 square feet while the variation of drag with angle of attack is also quite different. Figure 6 shows a disagreement ^n pitching moment slope and the value of pitching moment at an angle of attack of zero for the basic fuselage. Figure 9 shows similar pitching moment slopes for the complete helicopter in the range of --4 degrees to +4 de- grees, although the slopes at higher angles and the values of pitching moment at zero angle of attack are considerably dif- ferent.
Figures 10 and 12 show much better correlation in side force and yawing moment with yaw angle for the complete helicopter.
The drag curves in Figure 11, while showing similar shapes, are different by about 4 square feet in minimum drag.
In general., the differences in the aerodynamic characteristics
shown in Figures 4 through l.2 are typical of those found in, the
remainder of the data for the full-scale and LSWT 5$0 tests
tests.
Attempts to explain the lack of correlation have tended to the premise that the fifth-scale data were questionable due to
Reynolds Number effects, inaccurate modeling of contours and
model details, imperfect testing and data reduction, or a combination of these. Another idea was that because of the unique mounting system used for the full-scale test, a large and undetermined amount of interference was present in the full-scale data, even after the wind-on tare corrections were removed.
1.3 APPROACH TO THIS INVESTIGATION It was the intent of this correlation study to carefully in- vestigate the various possible causes of disagreement between these tests and measure or mitigate their effects in a second well-designed fifth-scale wind tunnel test. The approach used following is detailed in the sections and consisted of the: following steps. First, the data generated during the subject tests were reviewed to check for possible errors in comparisons made or corrections applied. Next, the fifth-scale model was measured in an effort to determine how closely it matched the prototype aircraft used for the full-scale wind tunnel test in contour and detail. As a result of contour discrepancies measured, the model was modified to the full-scale lines. A fifth-scale model of the 40- by 80-foot test mounting system was designed and built to duplicate the full.-scale mount in both form and function. Additionally, hardware was designed to allow tare and interference measurements. A 00-hour.wind tun- nel test was conducted of the corrected fifth-scale model on both a conventional single strut and the fifth-scale replica of the full-scale three-point mounting system. The data from this test (LSWT 630) were analyzed and compared with data from the previous tests and led to conclusions about the reasons for disagreement.
2 . D ATA RE Y IE ► /
2.1 COMPARISON OF TEST CONFIGURATIONS
The data review task began with a comparison of the run sched-
ales and configuration nomenclature of the full-scale and
fifth - scale (LSWT 550) tests to determine if comparisons were Made using equivalent aircraft configurations. There were virtually no perfect configuration matches. In the case of the basic fuselage configuration comparison (LSWT 550 Ruxx 19 versus full-scale Run 58) the LSWT 550 test used the 15-inch rather than the 10-inch fin extension, had no tail rotor hub, and no exhaust ejector fairing. For the complete helicopter comparison
in pitch LSWV 550 Run 22 ~versus full--scale Run 20 several dif-
ferences were noted. The LSWT 550 configuration had the main rotor hub fixed rather than rotating, used the 15-inch rather than 10-inch fin extension, no production protuberances, and no open cowling screens. some of the dif'f'erences discovered would have no measurable effect on the data. However, it is difficult to make any judgment about many of the configuration comparisons because detailed definition of the parts involved does not exist. An examp le of this difficulty is the designation P2 which covers production protuberances. An examination of configuration photos (of Ref. 2) shows that while picot tubes were included in the definition of P 2 they were not removed with the rest of the P 2 items after Run 28 (Table B-II) in the full-scale teso. An additional obstacle to a completely rigor- ous evaluation of the configurations test^d earlier is that many of the components of the prototype and fifth-scale model were one--of--kind items which were documented only by photographs.
Consideration of these facts led to the decision, that for the proposed test, an effort would be expended in duplication of only those configurations for which sufficient documentation was available.
2.2 E'V'ALUATION OF CORRECTIONS APPLIED The corrections applied to the full-scale and fifth--scale data were examined. These corrections were for tare, interference, and flow alignment.
Because of the design of the 40- by 80-foot test section it is not feasible to measure tare and interference (T&I). These measurements require that the model be mounted inverted, as well as upright, and that an image of the support system be suspended from the ceiling of the test section. A detailed discussion of the most widely used methods of obtaining T&I's may be found in Reference 3.
During the full-scale tests a series of runs was made to ap- proximate the tare of the mounting system. These runs. (I through 4 of Table B-II) were made before the aircraft was mounted. Since the vertical strut extended up inside the fv.selage to the pylon mounting structure, during the tare runs
this portion eras removed by fitting a dummy strut which, was cut
off at the fuselage fl r.
oo Interference effects were expected to be minimized by fairing the vertical strut and placing the faired horizontal strut over seven feet below the model. Since alignment corrections are derived from the same upright and inverted runs used for T&x measurements (see Reference 3)r no alignment corrections could be made to the full-scale test data.
The tare and interference corrections used for the LSWT 550 data were made during the original, Model 222 fifth-scale test (LSWT 439). These corrections were measured using the con- ventional upright and inverted runs with and without image system. Alignment corrections were also measured during the original. LSWT 439 test. The older corrections were considered to be acceptable because the fifth-scale model, had not changed ^ 4 ally b•t_^i v - s L bsta'nt ..,.. 4,.eGn ^C^ u^ .
4L. L. .I
Both the full-scale and fifth-scale tests were made with the
model on the center lame of the test section. No wall correc-
tions were applied in either test.
A check of the data reduction for botli tests revealed that the corrections used were applied correctly.
S. EVALUATION OF GEOMETRIC! SIMILARx5.."
Although the original fifth-scale model appeared to accurately
represent the Model 222 prototype tested full-scale (Figttre 3 shows a side-by-side comparison) this Fact was not verified at
the time of the LSWT 550 test, This section discusses the
procedure used to substantiate the accuracy of the model for this correlation study.
3,1 MEASUREMENT OF FUSELAGE CONTOURS
The differences that existed between the full-scale prototype
and the model were determined using a set of templates which represented the fuselage and cowling contours of the prototype.
This was done by transferring fifth-scale prototype lines at various station cats onto aluminum sheets which were then cut to form female templates. These templates were then used to check the modes. Figures 13 and 14 show fuselage and cowling contours at several station, cuts illustrating the differences between the unmodified model's lines ai,%d the prototype lines.
These differences are concentrated in the area of the cowling.
No contour differences are shown on the basic fuselage because changes to the fifth--scale model for other tests -since 1977 made it impossible to determine what the contours had been for the LSWT 550 test.
3,2 MEASUREMENT OF COMPONENT PARTS Wings were checked and verified to be correctly sized and mounted at the proper incidence.
The horizontal stabilizer used during the LSWT 550 had been destroyed.
The fin used during the LSWT 550 test had been modified and its exact configuration during that test could not be veriBied.
The current configuration did not agree with the prototype.
The main and tail rotor hubs showed evidence of having been modified but the current configuration did agree with the prototype. The configuration for tx``z.e LSWT 550 test coulee not be verified.
Endplates were checked and verified to be of the correct size.
Configuration photographs of the LSWT 550 test appear to show tk.e endplates mounted with nose left incidence while the correct setting is 3 degrees nose right.
As mentioned in Section 2, the detail items lumped together under the categories of "production protuberances" or "flight test protuberances" were not well documented at the time of the or de- full-scale and LSWT $50 tests and :many were later lost stroyed. The only stems remaining in this category were the tail rotor gxard t the tail sl^idf and a set of wi ndshield wipers.
d to r epresent These items appeare th- a.r prototype counterparts.
The Model 205 type afterbody (full-scale Run 23 and LSWT 550 Run 27), thin wing (full-scale Ruri 32 and LSWT 550 Run 41) and
flotation bags (full-scale Run 5 and L$WL, 550 Run 34) are
typical of a large group of oneyofva-kind parts which were not documented and no longer could be located for measurement.
4. MODIFICATION OF THE FIFTH-SCALE MODEL
Based on the measurements described Section S, which were
in made to det er mine the geometric similarity between the fifth- ;tale model and the prototype, it was necessary to x econtour, ^odify, or completely rebuild certain components of the model.
pr ocess.
`,,his section describes the modificat ion 4.1 MODIFICATION OF FUS ELAGE CONTOURS '-tae Largest discrepancies noted were in the basic fuselage and cm-fling. The fuselage and tailboom were brought to contour by f.il ing and reshaping the original model. The aluminum tem- plates which were used for contour checking served as a guide to ensure accurate duplication of the prototype lines. The cowling was completely new.
4.2 M ODIFICAT ION OF COMPONENT FARTS A, new set of wings, with dummy landing , gears in the retracted position, and a set of landing gear doors were constructed.
A new horizontal stabilizer was constructed with a removable leading edge slat.
The lower portion of the fin was modified to match the proto- type and the upper portion was fitted with a removable Cap which allowed rapid conversion between the V and V 2 Configura- tions.
other miscellaneous components which had to be made included pitot tubes, exhaust ejector fairing, tail rotor gearbox fair- ing, fuel sump recesses and covers, and pilots sliding window.
S. D4$XGN AND FABRICATION OF FIFTH-SCADV SUPPORT SY$TFM 5.1 REQUIREMENT FOR A REPLICA MOUNTING S'Y'STEM A suspected cause of disagreement between the full.--scale and fifth-scale aerodynamic data was the unique mounting system in the full--scale test. The full-scale system, which is shown in a side-by-side comparison with the fifth-scale mount in Figure 3, was a rather complicated interface between the 40- by 80 foot tunnel's three-point mounts and the pylon ,mounting structur(_ of the Model 222 airframe. Figure 15 is a schematic of the full- scale mounting system which shows the general arrangement and indicates the motion of the model in pitch. Figure 16 is a schematic of the single strut mounting system used during both fifth-scale tests. An important part of this correlation study was to evaluate the tare and interference effects of the full- scale mount by modeling it in fifth scale and obtaining complete T&I measurements. A straightforward approach using an image system to duplicate the articulation of the three-point mounting was too costly, and instead, an indirect
approach was conceived
using two separate mounting systems. First, the model wo uld be mounted on the usual single strut system and tested both upright and inverted, with and without the image system in to
order
measure T&I corrections in the classical manner. The principal advantage of this method of evaluating T&I's was that the image system for the single strut would be quite simple compared to the image required for the three-point mount. Using the T&I corrections obtained in this fashion the single strut data would be processed to produce a set of "model-alone" aerodynamic data for all representative configurations. Next, the model would be mounted on the fifth-scale three-point system and the runs made on the single strut mount would be repeated. By subtracting the previously obtained model-alone data from the raw data with this replica three-point mount, a set of T&I corrections would be derived for each of the repeated runs.
5.2 DESIGN AND FABRICATION OF MOUNTING HARDWARE Based on drawings and photographs of the original full-scale mounting system, BHT designed and fabricated a fifth-scale replica system. This replica, shown in Figure 17, duplicated the original very closely in both form and function with the following exceptions. Because the 40- by 80--foot test section would correspond to a fifth-scale 8- by 16-foot section it was necessary to shorten the replica mounting system by 6 inches (2.5 ft full-scale) in order to locate the model on the center- line of the 7- by 10-font section. The portion removed from the fifth-scale replica was at floor level and not considered to produce a significant contribution to interference because of its distance from the mode.. The other exception was in the representation of the xear pitch strut of the three point mount. The pitch strut in the 40- by 80-Foot test section is a series of nested lead screws of graduated diameters which are rotated automatically to change overall length and thereby pitch the model, In this replica the pitch strut was represented by a strut of constant diameter, The replica three-point system was also prov,Lded with removable vertical fairings and a dummy vertical strut„ The vertical wirings were removed for yaw runs during the full-scale test while the dummy strut was used to represent that portion of the support strut below the belly of the aircraft during wind-on tare nuns. In addition to the hardware associated with the three -point mounting system, an image system for the single strut mount was designed and built.
I . WIND T=NEL TEST During the period of 29 October to 16 November 1981, Bell Heli- copter Textron conducted a wand tunnel test ox the refurbished fifth-scale model of the Model. 222 helicopter in the 7- by 10-foot test section of the Vought Corporation Tow Speed Wind Tunnel. Reference 4 is the Vought Corporation report of that test (referred to as LSWT 630).
6.1 FACILITIES AND E}uIPMENT The modified model employed a BHT designed and fabricated pitch mechanism and angle of attack readout module which interfaces with Vaught tunnel hardware. This system, including actuators, sensors, remote controls, power supply, and readout devices, is independent of the wind tunnel operating and control, systems and may be moved from model to model. The purpose of the system is to allow the model, to be positioned accurately at a given pitch angle. This device is capable of positioning the model to within ±0.1 degree of the desired pitch angle. Yawing of the model is accomplis:,hed by rotating the external balance turntable. The support fairing remains streamlined during yaw.
Reference 5 contains more detailed information about the balance system and its capabilities.
Figure 18 shows the Model 222 mounted upright on the single-- strut mount. Figure 19 shows the model mounted in the inverted position with the image system in place. This image system consists of the image strut which is attached to the model and the image fairing which is attached to the ceiling of the test section. There is no contact between the image strut and image fairing. Thus, with the image system in place, the tare of the strut, the interference between model and strut, and the inter- ference of the fairing on the strut and model are all included in the measured aerodynamic data.
Figures 20 and 21 show the fifth-scale model mounted on the replica three-point mounting. In Figure 20 the mounting system is in the pitch configuration with both the Large stationary vertical fairing and the smaller vertical strut fairing in place. Figure 21 shows the mounting system in the yaw con- figuration with both vertical fairings removed. Patch motion is accomplished,by moving the rear strut vertically which pivots the model about the trunnion located inside the horizon-- tat fairing. Yaw motion is accomplished by rotating the balance turntable. The large vertical fairings over the main support struts between the floor and horizontal fairing rotate with respect to the turntable to remain streazaalined with the airflow.
6.2 TARE AND INTERFERENCE CORRECTIONS
T&I corrections were obtained for Low Speed Wind Tunnel test
630 by first making a series of patch run g with the model inverted and no image system for ten representative model configurations. These runs were then repeated with the image in place.
By taking the difference between corresponding runs the tare and interference effects of the single strut mounting system were isolated. These T&I effects were then used to correct the runs made with the model upright on the single strut.
6.3 OTHER CORRECTIONS A flow alignment correction was obtained using the technique outlined in Reference 3, which involved one additional run upright with the image system. The lift data from this run were then compared with the lift data from the corresponding inverted image in run. When these two lift versus angle of attack curves are plotted together (with negative lifts plotted as if positive), the angle of attack variation between the curves is emial to twice the ali gnment error. The al acE?1?1e?Lt error determined by this method was such that when the indi- cated angle of attack was zero degrees, the actual angle with respect to the airflow was one quarter degree.
Static weight tares were measured for each significant model change and applied during data reduction.
Following standard practice in the Vought tunnel as detailed in Reference 5, solid and wake blockage and compressibility correc- tions were combined into one expression, which was then multi- plied by the desired test q to obtain a q setting. Thus when a test q of 75 psf was desired, the tunnel was operated at a q setting given by the equation, thereby eliminating the need for blockage and compressibility corrections during data reduction.
The cross-sectional areas of the model and three-point mount are 1.78 ft2 and 2.17 ft2 respectively which produces approxi- mately 6 percent blockage of the test section. The reduction in q setting which results from this blockage is approximately 3 percent.
6.4 TEST DYNAMIC PRESSURES The majority of runs during the LSWT 630 test were made at the model design dynamic pressure of 75 psf although a few pitch runs were repeated at q = 100 psf. Yaw runs were made at q = 75 psf and 83 psf.
Fitch runs during the full.-scale test were made at g = 62.5 psf
rather than, 75 psf as originally intended. Yaw runs were
conducted at q 16.2 psf due to structural limitations of the
be noted that this
mounting system in yaw. However, it should
value of dynamic pressure corresponds to a velocity of 70 }mots
which is realistic for flight at high yaw angles.
Table I presents a comparison or Ri4ynolds numbers for the two
tests. There seeds to be no generally accepted reference
length for .&el.icop zers. Therefore, the table uses a unit value
or Reyaolds ntober per foot which is quite useful for comparison.
scale while the RN/
Nate that this value is expressed in model
ft of the Vaught LSWT 630 data (shown in Appendix A) was given
as an actual. full-scale value. In addition, calculated Reynolds numbers are given for wing, horizonta.4 stabilizer, fin, and mounting strut.
6.5 THREE-POINT MOUNTING SYSTEM TARE RUNS
Table II presents the final run schedule of the LSWT 630 test.
Configuration designations are defined in the pictorial nomen- clature presented in Figure 22. Table III is a comparison of configuration nomenclature used for the LSWT 630, LSWT 550, and
full-scale tests. As ska.owii in .,.ab.,.e I,. she first sex; l+V1+,.4N T.,lere
Made using the three-point mount installed without the model..
Runs l through 8 were made in yaw configuration although Run 8 was actually a pitch run. small changes were made to the model during this series of runs in an effort to match drag levels with Run l of the full-scale tests Run 10 was made in the same configuration as Run 3 of the full.-scale test. Run 6 supplied wind--on tare corrections i:n yaw, while Run 10 was used for
all runs with the model on the
wind-on tares in pitch for three-point mount.
AND INTERFERENCE RUSS
6.6 SINGLE STRUT TARE
the
Next, the single strut moulting system was installed with
model inverted and a seri r <,. of ten representative configurations
were run, beginning with the complete helicopter and concluding
with the basics fuselage. Following this series, the image
system was installed and the sauae ten configurations were
rerun. By taking the difference between corresponding runs of
these two series, TO corrections were derived for the remainder of the single strut runs. After the T&I runs the model was run
upright with the image (Run 31). The data from this run and
the previous inverted image--in run were combined to yield the
flow alignment correction. Next, the image was removed and
normal data runs began with a repeat of the ten representative configurations of the TO series.
j.4 6.7 COMI)ARISON RUNS IN LSW 550 CONFIGURATION After these baseline runs the model was modified by the addition 02 and a series OE seven.
tran,^ition strips (42 through 4a) made waLth congigurat, ions identical to those of Runs 15 th^:ougjl of
20 and Run 24 the ^$WT $so test. The purpose OE these runs
was to determine the effects 09 modifications to the model since the LSWT 550 test.
6.8 COMPONENT BUILDTJP ON SINGLE STRUT M=TING of Runs 49 through 73 represent a step-by-step process adding or removing components one at a time to match representative configurations of the full-scale test for which comparisons were desired. The g ull-soale rune to be matched were Runs 14, 20, 21, 22, 30, 31t68 and 69.
The data from Runs 49 through 73 after correction for T&I and alignment would provide model- alone data to he subtracted from later runs on the three-point mount, yielding Tal corrections for that mounting system.
Two small configuration deviations were necessary. The run schedule called for the addition and removal of the exhaust ejector fairing (F,) and the production tail rotor gearbox of fairing (Y.). Since these items were modeled clay, their addition and removal was rather time consuming. Therefore it was decided that after their removal, these two items would remain off and their effects added to or subtracted from the data as each configuration required.
6.9 COMPONENT BUILD-UP ON THREE-POINT MOUNTING Runs 74 through 124 were made with the model mounted on the Runs replica 40- by 80-foot three-point system. 74 through 76 were made before it was discovered that the model was yawed 0.79 degree nose left. These - r uns were repeated after the error was correct p d. Runs 77 through 107 are repeats of aon- fia,urations tested on the single strut mount in the series from Runs 32 to 73.
Note that in order to measure the. angular deflection of the of attack readout entire three-point mounting system, the angle module (aicknfuxied the ' l ot bubble") remained installed an.
model. By comparing the actual angle of the model, measured by the a bubble, with the indicated angle from, the wind tunnel balance the amount of pitch error due to system deflection under airload was determined. The maximum errors were limited 'to one-quarter of a degree. After verifying that the defleo- a bubble was removed.
tion of the system was very small, the Pitch and yaw runs before and after the removalof the bubble of (on Run 95) were made to evaluate the effect external wires readout devices. The effect of associated with control and a the wires proved negligible.
is 6.10 DVAriTUATION OF ROUGMSS AND PROTU7 EPA MS
Beginning r
with xmn 108 as effo t was ma de to match drag levels
of the full-scale test through "tuning" the model by usauig grit
strips as noted in the configuration nomenclature *
Whale grit
is normally applied to
wi nd g unnel M o dels fo r the purpose of
assuring transition to realistically turbulent boundary layers, the intent here was also to simulate the characteristically rough surface, as well as multiple jo^.^ats,
cracks, and' snail
protuberances of a prototype helicopter. Run 123 was intended to measure the effect of the more significant protuberances on the prototype aircraft.
6. 11 DATA REDUCTION
Six component force and moment data (lift, drag, pitching moment, side force, rolling moment, and yawing moment) were recorded from the external balance during each run in units of pounds and foot pounds. Data reduction was accomplished using Vaught computer programs.
In
the case of the BSWT 636 test, all the basic force and
AllaA6leAAt data were d- Mu by the test dTnamic
pressure, then transferred from balance resolving center to trunnion to model moment reference center, converted to full-scale values and finally corrected for static tares. Blockage and compressibil- ity
corrections are automatically applied in the setting of the
tunnel q as discussed earlier. Wand axis data in this form (i.e. before tare and interference corrections) for all DSWT
630 runs are presented in Part l of .Appendix A. Th ree ether
seta of data were also supplied by Vaught. The first was data for the single support runs corrected for Tscx. This could be referred to as "model-alone" data. Second was three-point mounting data with wind-on tares removed, and finally, there was ^ set of three-point mounting data with the appropriate single strut "model alone" data removed. Wand ala s data from these three sets are presented in Parts 2, 3, and 4 of Appendix A.
7. PVrSENx, TX0X AM DISCUSSION OF =ST DATA This section, including Figures 23 through 72, presents selected data from the LSWT 680 test. These data are representative of the test, trends in the data taken during And are discussed in five related groups.
7.1 COMPARISON OF FIFTH-SCALE RESULTS
Figures 23 through Figure 31 present comparisons between the
original fifth-scale wand tunnel test (LSWT 550) and the LSWT
630 test. These figures show the effect of modifications that
were made to the fifth-scale model. Lift characteristics
appear to have changed only slightly for the complete helicop- ter, while the basic fuselage shows a positive lift increment ranging from almost zero at positive alphas to approximately 2.0 ft` s at negative alphas. brag is as much as 1.0 ft 2 less in the LSWWr 630 test with the basic fuselage data again showing the greater difference. Pitching moment data showed good agreement at positive angles of attack, whale negative angles showed considerable divergence, particularly in the case of the complete helicopter. In addition to differences in the model contours between tests, some of the disagreeJ: e- ki" may also be due to an improvement in the technique of sealing around the clearance hole where the mounting strut enters the Fuselage.
This later explanation is quite plausible in - he case of drag which is lower in the LSWT 630 test reflecting a better job of sealing. The apparent cause of the large increase in pitching moment discrepancy for the complete helicopter is the difference in stalling characteristics of the horizontal stabilizer, possi- bly due to a change in the slat configuration between the two 'tests.
Figures 29 through 31 show that comparisons between the two fifth-scale tests for side force and yawing moment versus yaw angle of the complete helicopter are better than that of longi- tudinal. data. Drag versus yaw angle is approximately 1.0 ft lower.
7.2 COMPARISON OF WIND-ON TARES Figures 32 through 37 compare fifth--scale versus full-scale
wind-on tares for the three-point mounting system in patch and
yaw with the dummy strut (as described in Section 5.2) in place.
Figures 32 through 34 show lift, drag, and pitching moment characteristics versus angle of attack. sift is seen to be less than the full-scale value and drag is as much as 0.5 ft2 greater. The direction of these differences is expected con- sidering the disparity in Reynolds number (Table I). Pitching moment compares surprisingly well at positive angles of attack.
The reason for the difference at negative angles may be related to a moment shift in the full--scale data of approximately 4 ft3 at zero angle of attack.
Figures 35 through 37 show side force, drag, and yawing moment characteristics Versus yaw angle. Side force differs by a considerable amount pa. ,,cticularly at negative and smaller posi- tive yaw angles. The dull-scale data in this case appear questionable because the side force is non-zero at zero yaw angle. Similar comments apply to the yawing moment charact- eristics. Drag data compare exceptionally well throughout the yaw angle range. This excellent correspondence in drag prompts the thought that the reason for the discrepancies in side Force and yawing could be that those quantities were too small, relative to the full-scale balance system's limits, to be accurately measured.
7.3 COMPARISON OF FIFTH-SCALE AND FULL-SCALE DATA ON THREE- POINT SYSTEM Figures 38 through 58 compare data from the full-scale test with LSWT 630 data for which the model was mounted on the replica three-point system. These data have been corrected by subtracting the wind-on tares of the mounting system alone from the raw data. The configurations selected for comparison were those in which the fifth--scale model could be made to closely match the full-scale aircraft tested. Some of the configura- tions selected were identical to full-scale. Those which that compare with full-scale runs 14, 20, 21, and 22 differ in the open screens of the prototype could not be duplicated.
Figures 38 through 40 compare lift, drag, and pitching moment versus angle of attack for the basic fuselage. The lift curve slope of the fifth-scale data is greater than that of the full-scale data and the angle of zero lift is displaced 6 degrees. Drag shows better agreement with the maximum differ- ence on the order of 0.6 ft z at negative angles and closer agreement at positive angles. The angle for minimum drag and general shape of the curve are also close. Pitching moment cu=e.s agree quite well in the mid-angle range. Note that for Run 103, grit was added to the fuselage at several locations in an effort to increase drag by simulating the roughness of the prototype airframe. This roughness produced a small increment in drag with little or no apparent change in lift or pitching moment characteristics.
Figures 41 through 43 show lift, drag, and pitching moment com- parisons for the basic fuselage with wings added. In general the agreement between the two tests in terms of slopes and shape of the curves is good. However, the effort to adjust the drag level by simulating the roughness of the wing walk with various grit sizes produced some rather large magnitude changes lift
in and drag. These drag level adju5t:.ments produced agree-
ment. within 0.5 ft', although the additional roughness signifi-
cantly decreased lift. Because of the wings' location, these
adjustments had little effect on pitching moment correlation
which re g ained good. In addition, it should be noted that the
full-scale data show what is apparently wing stall while all
the fifth-scale data are stall free.
Figures 44 through 46 compare lift, drag, and pitching
i,4oment
versus angle of attack for the complete helicopter minus the
wing. Lift differs very slightly in slope and by about 2 de
grees in zero lift angle. The fifth-scale ;Lift diverges rapidly
at negative angle indicating stall of the horizontal surface.
The drag curve shows very good agreement in both shape and angle for minimum drag. Pitching moment slope agrees well, but the angle for zero moment is shifted approximately 1 degree and
data at larger negative angles exhibit the same divergence
noted in lift. Runs 99 and 100 were made at q = 75 psf and q 100 psf respectively before the addition of any grit. Runs 120 and 121 were repeats of Runs 99 and 100 after grit had been added. The change in Reynolds number has a noticeable effect in the previously noted stall behavior at negative angles for lift and pitching moment in the smooth condition and very little effect after grit .•:'as ad :edI. crag in way: smooth condi- tion increases with increased Reynolds number, indicating that a laminar boundary layer existing on the smooth fifth-scale model transitioned to turbulent flow with increasing Reynolds Number producing higher drag. The improvements in lift and pitching moment indicate a reduction in separation which is consistent with a turbulent boundary layer. With the model in the roughened state of Runs 120 and 121 the drag would be higher and change little with Reynolds number.
Figures 47 through 49 compare lift, drag, and pitching moment versus angle of attack for the complete helicopter. Two full- scale runs are plotted. Runs 20 and 21 differ only in that the main rotor hub was rotating in Run 20 and locked at a 60° az- imuth in Run 21. Bell Helicopter experience with rotating hubs has shown that a hub locked at 60 degrees exhibits approximately the same aerodynamic characteristics; as is shown by Figures 47 through 49. Lift characteristics of the smooth model agree rather well except for the apparent wing stall behavior at positive alpha in the full-scale data. Runs 122 and 123 with the roughened model and added protuberances differ in angle of zero lift. The drag data show good agreement in the shape of the curve and angle for minimum drag. The drag values of the roughened model are 0.2 ftx to 0.8 ft2 lower than full-scale.
Pitching moment data show very little correlation except in the shape of the curves at nominal angles of attack.
Figures 50 through 52 show side force, drag, and yawing moment versus yaw angle. In the case of yaw data the Reynolds number of the fifth-scale data is only different by a factor of 2, due to the lower test q used for full-scale yaw runs (see Table x).
Therefore the yaw data show better agreement than the pitch data. The side force compares well. The smooth model drag data of Runs 96 and 106 compare almost perfectly with full- scale. The roughened model has somewhat higher drag at small positive yaw angles. Yaw moment data show very good agreement in the slope and shape of the curves which all exhibit the characteristic unstable region or "flat spot" around zero yaw also noted during flight testing. Yawing moment data for the roughened model exhibit a divergence at Large yaw angles..
Figures 53 through 55 show lift, drag, and pitching moments in pitch for the complete helicopter minus the tail rotor hub and mast. This configuration is virtually identical to the smooth model configuration of Figures 47 through 49 and, as might be expected, exhibits very similar characteristics.
Figures 56 through 58 show lift, drag, and pitching moment characteristics for the complete helicopter with the landing gear doors open. The smooth model lift data agree well with full-scale, while the roughened model has Less lift throughout the alpha range. Drag data for the smooth model are approxi- mately 1.0 ft 2 less than full-scale. The roughened model data match full-scale drag almost perfectly for a = 0 1 to a = 61 with some divergence occurring at negative angles. Pitching moment correlation is poor except that the shape of the rough- ened model data matches full--scale.
7.4 TARE AND INTERFERENCE OF THE THREE-POINT SYSTEM Figures 59 through 64 illustrate the magnitude of tare and interference effects measured during LSWT 630 for the three- point mounting system. Figures 59 through 61 show lift, drag, and pitching moment versus angle of attack, while Figures 62 through 64 show side force, drag, and yawing moment versus yaw angle. In Figures 59 through 61 four sets of data are shown.
First are the wind-on tares measured without the model from Run 10. The remaining curves of each figure are obtained by sub- tracting model-alone data measured on the single strut from the raw data for the same configuration measured on the three-point mounting. This yields a tare and interference correction for the three-point system which may be compared with the wind-on tare. The three configurations treated i-n fashion are the Geis basic fuselage, basic fuselage plus wing, and complete helicop- ter.
The comparison shows some very striking differences between the wind--on tare curves and the measured T&I curves, implying that interference effects in the full-scale test data were not negligible. In the case of lift corrections the wind-on tare
is almost a constant 1.0 ft 2 while the s &l with the basic
fuselage is zero at a = 0 °, but has a considerable negative
slope. With the addition of the the T&x curve shifts
wing
upward approximately 2.0 ft2 while the negative slope steepens slightly. The curve then shifts downward and steepens for the complete helicopter configuration. T&x corrections for drag are roughly twice the basic wind-on tare values. Most the of difference appears to be due to the fuselage with smaller increments of interference added by the wing and the remainder of the items which make up the complete helicopter configuration.
The T&x corrections for pitching moment, unlike those for lift and drag, are much less than the wind-on tares.
Figures 62 through 64 compare wind-on tares and derived T&x corrections for side-force, drag, and yawing moment versus yaw angle. side force T&x corrections are approximately equal to the wind-on tare values at zero yaw but the variation with yaw is four to five times steeper. The T&S corrections to drag are approximately 60 percent greater than the wind-on tare varies, but the variation with yaw angle is almost identical.. Yawing moment T&x's, like those for side force, have a much greater variation with yaw and exhibit stall-:Like behavior at larger angles.
7.5 COMPARISON OF FIFTH-SCALE AND FULL-SCALE COMTONENTS ON TEREE-POINT SYSTEM Figures 65 through 72 compare fifth-scale and full--scale lift, drag, and pitching moment versus angle of attack for the wing, horizontal, stabilizer, slat, and end plates. The LSWT runs used for these comparisons were all made with the model mounted on the three--point mounting system.
Figures -65 through 67 compare the lift, drag, and patching moment characteristics of the wing-alone obtained by taking the difference between runs with and without the wing. The smooth wing data from LSWT 630 have approximately the same slope as the full-scale data, while the angle of zero lift varies by 2 degrees. The full-scale data show a stall, however, which is not evident in any of the fifth-scale wing data. Correlation is poor for the roughened wing in lift. In drag, however, the roughened wing compares very well while the drag of the smooth wing is too low. Pitching moment data are qu o te scattered for both full-scale and fifth-scale wings. Pitching moment slopes in fifth-scale are lower than full-scale values and there is very little agreement in any of the data.
Figures 68 through 70 compare the full-scale and fifth--scale aerodynamic characteristics of the horizontal stabilizer in oth : ft and pitching moment show very little correla- pitch. t: tion ,le- or zero angle. Drag compares very well except at the _ .-J ger ,-egative angles.
ampares the effect of the slat on aerodynamic chap— Fi r,are 71 ' acteristl_:3 in pitch. Generally, the agreement between full- scale a----d fifth-scale is good, particularly in the case of drag. T,he , e is some divergence at the larger negative angles except in the pitching moment data. While the pitching moment data from the full-scale test shows considerable scatter there is good agreement with fifth-scale particularly in the shape of th ; curve.
Ylgure 72 compares the effect of the endplates on aerodynamic characteristics in pitch. Lift, drag, and pitching moment data agree extremely well throughout the range of angle of attack, It should be noted that, because the endplates are vertical surfaces, the data presented in Figure 70 should be considered as endplate effect on the lift, drag, and pitching moment of the horizontal surface. The primary effect of the endplates would be seen as variations in side force, drag, and yawing moment with yaw angle.
S. CONCLUSIONS AND ,RECOMMENDATIONS
This section discusses the conclusions which were drawn From
the data obtained during the fift1a-scale testing of the ^iodi-
fied Model 222 wind tunnel model and the comparison of that data with full-scale and earlier fifth--scale data. Figures 73 4 117xstrate the through el present these summary comparisons and from improvements in correlation obtained testing on the replica three--point mount.
.1 CONCLU'S IONS The primary cause of the lack of agreement between the fifth-
scale data of LSWT 550 and the full.-scaie data of the Ames test
was the effect of interference related to the three-point mounting system used for the full-scale test. The effect of the mounting system was most obvious in the drag data compar- isons but was also noticeable li£t `and pitching moment data.
in When the tare and interference effects measured during this test are applied to the full-scale test data, the drag is seen
to be low- e
substantially r than ori ginall y believed. The proto-
type drag value at a = 0 0 was reported as 73.5 ft2 (from Run 20) after the full-scale test. If the wind-on tare of 2.84 ft2 is added back in and then the fifth-scale tare and interference of 5.8 ft2 is subtracted, the result is a corrected drag of 10.54 ft2.
Several other conclusions aye suggested by comparison of the LSWT 630 test data with the LSWT 550 and full-scale data.
Figures 23 through 31 show that the effects of contour differ- ences were minimal.. The differences seen in the data (primar- ily in lower drag for the LSWT 630 test), could be explained by either the cleaner cowling of the modified model or by an improvement in the sealing of the model in the area of the mounting strut.
Reynolds number effects were concluded to have been a relatively small factor in the lack of correlation, except at large angles of pitch and yaw. in these instances the fifth-scale data ex- hibit ,tall-like behavior which might be expected at lower Reyn,L.-ds number. Runs which were made at dynamic pressures of 100 psf, as well as 75 psf, showed an improvement at the 15 percent higher Reynolds number.
Some of the disagreement between full-scale and fifth-scale drag data was due to the unrealistically smooth surface of the model. While the flow on the model was generally turbulent, it seemed necessary to further increase skin friction by the addition of grit to adequately simulate the rough surface of the prototype. This roughening usually did not improve correla- tion in lift or pitching moment, Correlation between full-scale and fifth-scale data for the wing, horizontal stabilizer, slat, and endplates was mixed as shown in Figures 65 through 72. The only obvious Reynolds number effect noted was
a premature stall of the model hori-
zontal stabilizer in the negative angle range as shown in
Figure 66.
8.2 RECOMMENDATIONS
Based on the major conclusion of this investigation it is re-
commended that the determination of tare and interference cor- rections receive greater emphasis in full-scale wand tunnel testing. This greater emphasis is of particular importance when unconventional mounting systems are used. The technique employed in LSWT 650 to evaluate T&I corrections by testing a scale model of the aircraft on a scale model of the mounting system seems to be a promising alternative when full--scale T&I measurements are not feasible.
With regard to the use of small--scale testing to determine T&I corrections, some further recommendations are
offered. As with
any wind tunnel test, complete documentation of,uodel contours, configurations, test conditions, and data reduction is crucial.
The small--scale test should follow the full--scale test so that all runs and configurations of the full-scale test are known and may be easily duplicated. This is particularly important in a typical development testing situation where unforeseen
runs and configurations may be added during the full -scale test
based on data from earlier runs. The disadvantage inherent in this testing sequence is that the corrected full-scale data are not available until the small-scale T&I's are measured. This
problem could, however, be eased somewhat by running the tests
concurrently..
An effort should be made to ensure that several representative full-scale configurations can be duplicated exactly for the tare and interference measurements. In addition to the expected
faithfulness of contour, this would also include careful seal-
ing of the full-scale model to eliminate any airflow or leakage which could not be duplicated in the small-scale model.
REFERENCES Ol.denbuttel., R. H. , A LOW SPEED WIND TUNNEL T4 0T OF THE 0..20 SCALE BELL ;HELICOPTER. TEXTRON MODEL 222, Vought Corporation Report LSWT 550, 1977.
2. Rester, K. L., Ri ALTS OF THE FULL-SCALE MODEL 222 WIND TUNNEL TEST, Bell ,Aicopter Textron Report 222-199-002, 1978.
3. Pope, A., and J. J., LOW SPEED WIND TUNNEL TESTING, John Wiley and So- New York, 1966.
4. Oldenbuttel, R. o, A LOW SPEED WIND TUNNEL TEST OF THE BELL HELICOPTER TEXTRON 0.20 SCALE MODEL 222 INVESTIGATING AERODYNAMIC CH-7__ZACTE'RISTICS, Vough.t Corporation Report LSWT 630, 1982 5. Holbrook, J. W., LOW SPEED WIND TUNNEL HANDBOOK, LTV Pub- lication No. AER-EOR-12995-B, November 1979.
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f Complete H el icopter ^.
.:E s f'
t 'rti C onfigu rati on
^4 , 4 1tun vull Scale O .E z 7 ^ 't 'E ^' f
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LSWT 630 Fifth Scale Run. 119
;`_ {::.
is :c t•. t t ^; E. f ;.
r ^ t . { ^ - 36 .
1 r ]t t •: 8::' :2 T Im -; :2 0' t a:: .... ..: J.:.:
1-7
.# .
j:- ,.
':: -Z6{'' i=_8{: ` -32i 4i: s' r 2 4 c0:I :$ E'il6 ` . t 32^
l
II e u l:l• ::: :r•:.
ff.
....
Figure 2. Correlation Improvement for Helicopter Drag Characteristics in Yaw .^aA
scale Na22 model in Vough t
b y 10 Foot Wind Tunnel.
0 by 80
Foot Wind Tunnel:.
Figure. -Comparison of Prototype and
Fifth Scale Model.
OF POOR QUAD i n w3rp.
I to An A C* OVull Scale Run 68 .............
- FEE* Toot HP I YV ^z I.; W . ......................
jjC3 L 6WT 550
TER :11 A A T*_ El . . ........
.
T 1,11 "74 1-i-
14 THE Imi 'f i ll .. 0 ,i l i i7i
Of - 1 x ham, tot t=1 AM i! , 1mi U.: , v: I.
%' .1' I W E oil
INN. Ali q u m l l^
M
N 11 oil
mmx: I
W Q 1
....
.. ....
P I . T "J , ......
1 a-deg UUM
. ' J ` : ^ i
J.
i m
7 1
F ly; Q4 W 7A r 't 77. HU E ll 7 X X rii.
.1 yj q En t: .4r Ri ga m 1 :l C
1 . - '
" i f i 1 1 1 " _1
M 111111. M 4 F A fol EN r
MAY son i n - -' n
Fe Lt UE.
pg.
lot T 0 !r* j J - . . . .............
...
4 L.
H::1 :I.
P fit
T U gi g
Of
Figure 4. oxivgmnal Comparison Lift ChiractaNstics in
Pitch for Basic Fuselage A 1"^ L F OF POOR QUAD - AY It:T 0 Full $cale Aun.
)D/ • $50 X4S WT 1 9 . 1 1 NI; N V.
. .... ..
......
":I M, .. ... ... It TtIm v l- jr^ P "14t :.It IV R-H .... V"T ....
V 1!: :I- ! : p w.
v. ,. wi . H IN .
iZ iW tj t I -4 ' b' ; 14 =4 r —!—V L '" 7 TrI T *!" i : V I 1 0 q- t 'TI it: ii j;:, Nt ley III,.: W.
Figure 5. Original Comparison of Drag Characteristios in Pitch for Basic Fuselage ORIGINAL OF POOR Qum a O Full Scale Pun 68 ...c =i .i.
q ' LswT 550 Pun 1.9 its 1 - 4 ill* it S t l 1 t 1 SS i F Y i {.
r 1 t 1' 'T :4::1 -deg t { ._:: tx: cs ♦1.
i '' ^Ii ,, [? +: 't-., ♦ t , ' 1.^ T3 ,.li ".
'... .t : [ T -• - •^' 1 - . 'i I'. :It t 77 1 1 ;. .
'i li t n - ri .
t •Oo I I l ,} i .^ e•1 i.
't :'i: ^. 1 ',.
tt Y. I ;t, i i = r . J 1 .t1 :t« ryry'•e7 '_ r7 . Do of Pitching Moment Character- Figure 6. original. Comparison, istics in Fitch for Basic Fuselage 00 uv ,.
1..
• t : tt. = 1' ..SS '.:: l i .. t T ,r Year .
•aia` t.yl. Si 1• ti, a 'I, _ it 3^': t f a i ; .l.
—T!, t l ' ' At t ! t 1 • Y ♦ ^ L 7 r IS 1 p,: ^1 i 1 s .i ``" t 2 =;' -8.' 1 0 4r =` ..: 12L 16t `^ `! e8 II° ! ; t t :! t w : « a- c^eg i . . . . w I C.1 ,:..t r ^ _. !^ _ ^^ t !•. /. Ir ^' 1 :.! .i. :i.: :Ll 1. \ ^ , 1. . ♦ . $I[ 1!. ^t.I 7 r ih I 1 } }.
, IIt ,.
O Full Scale R^ 20
• 1 E,,r t 1= i 1 1 • _ { !. t 1 t .t :i.0. ,. f f a . I s. 1 t S i«^+-e^- y t T 1 t 7 t ' `,rai.W+7.rL:: 1 1 ta..^. Li.:.' LL...,. LS. 1 ta..^ 1 i h.l ,..p i= ^^ 1
LSWx Run 22
RR rvl r' l Iti ♦ i' i{ . i • ! . u. \.i! {',. .Li•. l.. a. 1 .i.l Lf.i ♦ r!F tt 1 11 • .t ^v!'
C Z^.
r . i i' tLi= i t- 1"= t ! = Ci, a! . a1 3 0 ' '1 i 1r, `i r ♦• w I 1 '!t , L..
it, r I ^^ =t ! i + , I1: ! =. t !iii i..^. ` .i t ^ :1. xttl ` IM 21L
i = 7I , `
l r k2 t. •t' t 7 ! .. t
-T T
t r r
`"°' i^ t . 1 !' till C ri `li, TH:.D .
Figure 7. Original Comparison of Lift Characteristics
in Pitch for Helicopter
ORMWN1. pn ,^7^— — -L-A Uj
OF P OO R QUAD
w I l M I . I 1. q v , r.I I 1 . . !4 .:i I *.I I . - t. i - In. -1- J." mn % : I ]:;: I "; -N I if?
f f !" I, .. : -;. : -I q . , ..:. v ?it } .
I: ! . Will- Wll , 1 1" I " it . I . I . I . i f n.
Scale Aun 0 Fu 11 2 0 * 1 * 1 ^ rrV 41.11.
710 LSWT 550 Bull 1. . 1 . t .
- .7 . . . . I I . I . I Tfl: I I i:, IT I ,: I: I t! j • oi I I I. .... 1. IT I '- -t- -1 E ll, 4o t V:! *111 N.
I t i . . it ;ri- !..- :, I -, 14-1 3w .
R: E, v, IT: -tv- M!4 1 . 4 li t IE nu.
. .
+ .... ....
:j D/q-ft t- .:: 4- TI;; j!'. % i: i v .
It .7 H I M .... Z1. ..
IT I t z :i .t t ' t t I^ 7 ME t t , ' pl: rl: 4 1;;.. N I V ° ....
.1 1 1.1 I.1 ... M 'l 11 1* .... ..
1 .
1 IT:. I t , IT; ^T V, I :;TV IT t.
J v- tj4-: !R- .... .... ...
L . t : ti l l ;T77 7.,77 I ln- i , it I .... ....
..... .........
i. I ....
.... ...
n T: i.
:T-,l MA It" ... ..... .. .. ....
4: 1 7 , ^iJ8 - t .. C .
-deg I Vr.
Figure 8. Original Comparison of Drag Characteristics
in Pitch for Helicopter
L C r7 2U11Z;,/7._ + Ot t n.
-;14 it ;1 n 1 1 1 1 . 1 1 1— T . + It 17 4 M I i n It .... F Sr M n ". ^: r;; I an 1i t 4 l *1 1. 1 . 1 + tzt M4 • t . 0 t I q-ft Sc Full le Run 2 .tj ... H . i_,Tj- 4. ... .... .... . ...
t! ^ ...
11 4 U-1 H. M: M Ill R 11! -4.4 1.
tI 'nn 4::: n V; 4,4L i " ; ...i .... .... . . .. . LSWT 5$0 R=2 2 ' ^i tr 6 C.a 1: t.
Jv , I,.- iii , .*,:: M: -Un T T.- :* I RE t p It L, S It! ?: i r HIM I . I.n:= r:vT4 IUMNI: 31 W Lt.; j i v ;nT _ 14 n - "IMN . I L . i i + n , " :iR - '-11 q 4 H^: .; i '-- - i : - f^ ^ : lr;^ v r. V ., + -t . ; - r . 1 . 1 T. I". *Z It ... ...
t.
G :1 XM I 74:: 111* t., W 7; t" I t, Ntt .114; IW Via * I -: N, n . • ju, ^T 11 1. 1 11, H1 : t; i - i. M: ir ;TT =^ . ... . .... I 0 ....
1 ., "i lz-; ;Hi I t H..
.. . ... ....
:I- I- .... .....
.
i !^ . . . I t 41-1 .!1 1! 1! -1 X * : .1-i It.
4= N -%q i - - _r w t- R, ii; 'n; :ri ; ;U W., W. ! , i v.. :t V", d t' n ..;V it., 7r^ .. ...
- :TIT F., ... ....
..
Z T + T: . . .
. v. . 04 -80;: 7*T: !TIt n- V T T- .1 F, 16. 44 - Figure 9. Original Comparison of Pitching Moment Characteristics in Pitch for Helicopter P r up%-g4g.
(C)F POOR qjv"!-r v ! i It ^.
No to v-.- it 0 50 - iH H U..
4 1 h 111 j - - ^.F! 0 W W j Jvi S - i QH 9H HU 110H. 1! 4 1 . it oil 1 it Mh A hil l ;df N fl. ..... .E.-- , WITU HR. , ; 31 9N NNE 41 M * 7-A 1 i - I it r!
.
WIN u Al ti : H.: ::. ...
..
W . A . H HUI H- H ! 2 .... .... .... .... ....
.
. . . ... .... NO ME H . ". K Hu tt H 1 R1 Q No I I fill 19 M A;; HE 151 No OWS' aH N 0 4 1too! IT RA VIA f ... .. . ... ....
4 0 :A VA A.- Y, WARD A.1 1 0 M E.... I.R.
T 2. t' 2 HF J- E.
.. .... ..
M Ti 1 0 VA H i t , i T.
14 T OF' u p 14 K: ip ..............
....... .... . ....
:
AN ^ d
y2 y
! i - AF T i n 14
vo yam A l l q
icy ST..
.... .
3eg .... K ....
....... ......
i t Vis! it: . .........
OWN I Full Scale Pon 30 17 7 ' 7t Run 24 q LSWT 550 1HI 1j; 4.1 lot!
wo all Figure 10.
Original Comparison of Side Force
Characteristics in Yaw for Helicopter
ORIGINAL OF POM QUALMr Full Scakle Rini 50 4 41 ' *r ' 0 ^3 .1 r i1 i f ^.
^ r i ^ 0 TJSWT 550 Run 24 -;14 Or!
77, T.
-..2 W rT T.--2 it.
IE::..: N.
..^t ni -^- 1 2 OIJ V!T ! l In, 41.
4. 1 um l l Mv !qI 6^- VI!, IVV Vi T: Tr : .
J 7t- V: i U.:^ M i fl i - 1111 41 1 *1, 1 .... .... .
; - Air 14.
MV I .. ... ...
.... .... ..
2- 3 i- H' 2- 41- T-deg ; 7 Figure 11. Original comparison of Drag chRracteristics in Yaw for Helicopter — 1 Pal
OF oo , 41 QUAMN
.1; t .... ....
2 4 0^ InK I: M lit. I it.
YM/q Full Scale Run f *!* N = 0 i 550 Run 24 q T45WT Ahi: % N .......
......... .. .....
7.7 T v :"T 7 14-- I;IJ U ., 1 w, P-1 i !
--i-7i ' 11 !i: 6iffi - T124.'
_111V !0.mv -.7 .
! -d e g t . 77— 7r t: -78 .. ....
. . . .. . . . . . . .
7 7.11 ... ...
Rii t _;Tt 7r^_ZT 4 11 1. 1 x
i L I
E
J.
4r.
.... .......
. ... .... ... .. .. ... .... .... ..
.. .. .... ... .
ti: .... ... ... . .... .. ....... ... .. ....
. .... .. . 71 ... ... ..
-3201::,(
TT!T T t77 I o. w-
X*.
Lt.
Figure 12. original Comparison of Yaw: ng Moiqexit Charactex-
i •tics in Taw for Helicopter
w
co y^ ,E 43.9 d o-. f g^ rc^ a^E c ^hh
Figure 13'.'
Contour
Discrepancies of M222 Model (Si.deview)
- Prototype
550 model
------ LSWT r STAt74.4 STA 71. 2 W ko ^'XA 4 b . 9 STA 43.2 STA 45. 0 % STA 38.0 STA 36.0 STA 35 + 0 STA 40.0 STA 42. 0
Figure 14. Contour Discrepancies of M222 Model Cowling
n 112— OIpIIIQI'I'1\InI7 OF ?OOP, Balance Resolving / Moment R I C Tunnel, Centerline r
C
trut tI on or Figure 15. Schematic Drawing of 40 x 80 Mounting
Moment
Reference
Figuxe 16. Schematic Drawing of Single Strut Mounting
Yaw Configuration Pitch Configuration .«a i- z Support Figure ` h , Pitch Run Testing.
c PA 57 E t sLA(;K AND WHI'l 4J 4-4 .klq fAD p!
:
^
^
^
m «:
^
^
^
.^
: :
^
Figure 20. Fifth Scale M2 2 Model on Three-Point Support
(Pitch ƒ:= Configuration).
A ON : X
M222 Model on Three-Point Support
Figure 21: Fifth SC*\%
(Yaw Run Configuration)
13 3mooth ft s lags and tail ,rotor.
C Prototype cowling, Figure 22 Pictorial Nomenclature.
C, p 14, were Canted Endplates stabilizer.
Endplates on horizontal E, 3 0 nose right Exhaust ejector fairing,
E
a
-ut d
ure 22. Contin
Tail rotor guard antenna.
-70
NACA 0015 horizontal stabilizer (with T.E. tab) set at
H +
(+) superscript indicates that a leading edge
incidence. A slat was installed on the stabilizer.
Figure 22. Continuged.
A P,14 m Main landing gear t,"etracted with dciors closed.
no doors.
*1 in landing gear retracted with M 2 Figure 22. Cc.)ntinued.
j"AR AP H" N Nose gear retracted with doors closed N Nose gear retracted with no doors !shown) 0 4 All screens on cowling closed, See photograph of BW configuration.
Figure 22, Continued.
N"i^']II"WRAPIA
P Product i on protuber
a nces: pitot tubes, w indshield w ipers and
pilot's sliding window on L. H. side.
Fuel sum,,p recesses covered, P Fuel stmip recesses open.
P Figure 22. Continued, E G -panuj=oo 'jZ eanbla -qlnmTzv 09 ju Jos sloaluoo fIsvw t qnq w4ol TTVJ I I NO ST In pur ozo;) qinwTze og ir ies sloxquoo jorm !qnq aoqoa UTPW T'h 0, jo qdvabo4oqd ' uO T4 vxn5 T; uw i OP S * buTTAOD OdAmold vo sao4supe qsnvqx p pur IOTuT pabbnTd LAE T' QUAI 9Vk A Poop, ,OF (TS) 1 No. 36 carborundum grit on f o ard and rear struts of Ames
rw
type supports.- (TS) 2 Transition straps of No. 50 carborundum grit applied in 0.125--inch wide bands to the model as follows;
a) nose
windshield outline b) o) outline of engine inlets on cowl (2) bands on cowl aft of inlets d) e) top of cowl parallel to airstream f) both Sides of vertical fin 5% aft of L.E.
(Top View) 1.69 e 5% aft
of L.E
s--17.5 8.0 }-^--^ 1.75 Figure 22. Continued.
BLACK AP,411D r AP14
(TS) 3 (TS) 2 plus wing-walks made of No. 80 sandpaper on upper
surface of both wings.
+V ^ (Top View)
180 sandpaper on upper
(TS) (TS), plus wing-walks made of No,
surface of both wings as for
(TS)3' Firpare 22. Continued.
-panulluoD ^zz aanBla x0buTis qjTm ul; jvoTqxaA dr, qouT-ST pup , Cgsl I'm of spumxo) TWITIZaA MO a; POAOM01 1716 q4 TM - ( - I) UO Yva nb TM O D 4(SW M Y sqj woa; Noeq seqnal gZ , o aazjjjqv4s W P O bu TP VO I ;o aor;ans aesol U - v aS wnpwnaoqavD T P I UOZ T aO l 01 MA S og *ON ;o d MI S AWR uoTqvinbT;UO; 01) O PI m K U T-01*0 MTM , abpo
bu T P VO T OU MO Q S W OU T WO AT04VUT
-xolddv NO W SUTPUO IXO SOIVTdPu VO T UO I T16
P A 06 P O bu TP
wnpunaoqavo j q !A P
os 'ON
X UOT4TPPV A M u0Tj vxnb TX uOD GAW
I ll , I i'll"Well, t") % " 1, c
C ' "-', ; ^" f
SLAICK,E i ''OGRAPI4 F'HOT V 151).
Vertical fin with stinger and 10-inch cap (extends to W. L.
wing with standaid tip.
Prototype NACA 0035
W
I
Figure 22. Continued.
M te, X Pumew 40x8O type mount with no fairings on 'vertical support strut, Asterisk denotes 'that wiring which was taped to support struts was removed.
Ame 0xSO type mount with both fairings for vertical support X * strut. Asterisk denotes that external wiring for bubble package wasremoved.
Figure 22. Continued, mount with dummy strut and no fairings.
4000 type
X3 Ames
Fences mounted on hori,zdatal fairing adjacent to support.
ORIGINAL ^z OF POOR QUALITY
X3 x2 configuration, but with material removed from hori-
zontal fairing as shown in sketch.
Figure 22. Continued.
X2 Co nf.,gux ,orx X3 with ambber loose added to near strut as
at showxl to increase diameter..
OF POOR Q?^AM u ^ (Deg) (in.
--15 -15 x.3.25 0 7.75 +15 2.50 8.25 Rubber Hose- L ^ 0 1 Shown) (Side View, a = X3 Configuration X2 with simulated joint at base of dummy strut as shown. Joint was made from foam material.
r Strut 3.0 Figure 22. Contin ued.
odified as shown in sketch.
X 4 Joint of configuration X3 m strut GM.nMIM M I z q) of POOR UL5 i1 d 3.0 X Configuration X4 w ith dummy strut removed and fences off.
Figure 22. Continued.
A[" OIR I G I N PA, IE!
BLACK AND 'AMITE PHIO"I'O"GRAPH X X 4 config-,=ation with dumy strut and small fairing I as shown in sketch, Y original prototype tail rotor gearbox fairing.
Figure 22. Continued.
ORIGINAL 'PAGIZ
E41-ACK AND WHITE PHOTOMAPH
Y
Preliminary "production*rotor gearbox
Figure 22. Concluded.
Figure 23. Comparison of Fifth-Scale Lift Characteristics in Pitch for Basic Fuselage # } ::1 -iI21 2ii :IT - a#f: ur 41 M: 111_14 il..r 40 . ,}t :.i T ' +ltf ^.. T, ,, I S * ,_ x ^ = I 2'. r , II, 1 d.
l:i ll' 1 r 3 + r S f }ri 2 2 ry + atj7 I dS `: ,:I .. i ..
^t i^ t . .^ ^ 2 , + .
-,: e.r ,! r, +r t^ , , .i , +i +d r a S^i ,.12^ } i * Ij 2 i :i: I} + ,1 1 t r!
. a, ' . ;t, . , 1 I,S 550 } N.
WT 20•` Run ft L/q .} if : 1 + ^} zi .t i.}^ } t ^tiT r ::: 1 • « t"2 :^ T: Vii.
.~ 'ZSWT 630 . 1 Run 42 t t } ' til } t t t './ ;^ }c t t 1 ,i t iT: .z :I' , i :,} : i U,* .30 ;. t I : .tl ii.} . 1 i t i , t TM?
'+ :r 1 J! t ii:?
T.
oa.
'i i ! . i ;i r a Y ,r.. a z :a 1. .1 • a.... .... ..
»i^ • + a.. .M1 11 ^. _ • 1 •2. +• * .t I. 1 t;:: S;r a i} i ^» :z +.i i.
}t '#! + 'tt? is ,:: 1 T +1ii : "t }t• 4 1 4 . 4+4 ',.
Mi ii! f,r2 [:YS ' i . ^ T j t iii + . ,r :+ 1 t{ t f. i + i r i .' 3 . 1 ^, ' ^_ ' tr Y ' ; + 2 i ?
( i 1 ^: i 2 in. it I, . ,d *..: at. ! T. r. :ii : 11 rt ♦ z t ° t.e:' tv, :•1 +,t L I}: w ' r + «. ,!« i1 . « t: r!_ ' :3': ;'Y: ,: i•, 0 0 .t 'h; ,i • J..: } { 7^ ?,{'t «Y11 ii' :i: • sa;l i J!( `:I.
} «t" '( }:.r i;^ t .+^I .rL. SS .I [ , , ; 1 :. .1. a 3 ♦• 1 1 0 a 2 • I' z + :t i. I Ir f l Sl ► .^}: li '.2.: :2r! iz L :2: .f.}'F i}: • a: '! :3 S- :J}- ,i {z: }}? , • ? ^ 1 Q1 ` } :} * it:{ •:^.: i ^ it ? a r. si: « !i ii? ' ? ?}:: :i: iu t 1 .ji+ +P.
is Crr+ . S 1 $ , ., It tji 1 p,2 ';Z; .S i':t 'i 2T} , ji .:' I1}j :S :i:: + !i* +i 3. 1 1 fit, - 11.
;«:; :. ., _ , :; :, r , r^ ++ •j^ :i ^-• •^• ^ !riz. i tl ^ T1 1 r• :t :. .t } ' itr: '^ .t; '«7: 21; 2 + .} 3 ; , . + 2 ^ *+ ♦ };i • S . ii :i' il:. • ':i .^ ' ' t i}... t Y-^ fit ♦ t^ti -^..'::^: 0 !
J lc2 -:t 8 : 16} { ? 20 24 +. c J ^=a ' -16 +} •F' -12 S I:;I 4i 12,. ? : , r_TY +r +2 il.
?3 1 '= 2 , _`$p ' 2 ,t $,. •1t iI . i ''+:^ i, :il yr I'Y :'+ r 2 .
...
Ma r r t `, + , + , O H i t 12 i f } 2 - h: I.a1 .}I. ii}: 1 :I t .t +; } t. +. I. i. "7 .,- a i, i i a #, .t• : F.. }' 1 ' a ::' T :i ;3 , .1} it. {• I 1}, 2' ; ♦ j t' :T ^ 2 •'^ I 2 i _ _ ^ 2^ #^}; 1 .I 2$Sixi+ r ^i • i,t :} T +^.^ :rs fl , 2 1 :;• N+ r .
H I T :, ::; c,: fi u' + , ,i ua } UT.
i< 2 3 !' t it:i t !" •^ ' il ri3 } :':, -2 0 M i; :i: ,' aJ2: ` } 2 ' 2. ii ''2 ' 1 :' 7 fY j + :I Ji.! ..
lit! :7 :rti:2, : . r , ii F + c 1 F„ {• # ,T`i i1?
.t f 3:?:: 1 1.. '^? * i::i :.' S 3.
l , + t ♦ 1 .: i:2 i^,: F.+2 ' t ? +ftli t:.i I.^.... •_.
I» 1 ^{ :t{3 «t^ i.t^ Pi t ,rli r 22 22 }, 1 r a ..{ . 1f t ++r I F T { :} r ' I°} J +^ , I +I 1 2' ?
a. ' I ++.ItT to .♦ , ! T}: t „i a ? 1. ,t + + f T1:. { is } t itt m M.
:i2. T *I , i :lit t t « : r?
3, }^?. S t j ;jai' I }' }# ,;.' 71_. tF . c#. M.
# i i ,♦ : I 1^ 44 iL4.
+, , f ^I # + 2 T " +! !;', ,t .
i'F, :2 i j}j T 3 I :si .
«^ r 2 i ! + } Jf r , +.«+ ., t + t .rj.# *: TT: I :ir t,' : }.i .
i . ,: 1.., l :.. I , , si: +, # I3^} i1+.:: ''"+. 1 ♦ 4. 'j «t, a,+ rF q :.ty .++{ a /, {•, 122 + t + l r t N i t ^; , ' 2 + 1 - , I ;^, i1j12 - ., , ^ * I + } a?Yi ti' to , + ': . 1j...1+27 +.
•j. I. :Y a f •a t : f l 3': +„ .t • . t + II^2'' 1 * fT i•L } .StI + .;., 1 t , tf/ ,ri f } r C [! { " l: L I I • I : ,+ !t 1T I + + i i + , , + S + : `+ +. + 2 i[If +,: itrr i it
i I t 1 . , . , , , +
t r # S +t; , 1 ,+a i Q + It + t tr - I i ^[ F: 2' , F - . , I ` }.
: ii 1 r + N f i +i a ^' •: •' .•: +' ft a ii; i;yT ^ li .J ,/ .I t + "? 7 i } i^it t.f i + a1 ^, t: 2 + +^t« } a :ta } Salt y + ++1,,F .+ +- }T'! a, , L.I "^ jtff I k. 2 .i ! ' } 7 t ♦ ,.. > . ,+ f l .., 2 }+ f a }« t t. 4.i TI.I ".2.. i{ I ,I :ra , . :{ { . ♦ +.
iii} t j, x t , t ++t if { i r Figure 24. Comparison of Fifth-Scale Drag Characteristics in Pitch for Basic Fuselage . .... .... ... .
.... .... .... . 550 LSWT Run 2 0 I; !-.;I vt a6 I .... I... I....
... .... .... . . .. .... .. .... .... .... ..
LSWT 630 Run .
u.
z T 7 . .... .... .... ..... .. .. ....
4= ... .... ... ...
... .... .... .... .... .... .. .... ... .... ....
.
. .... ..
.... .... ....
:77= .... .... .. .::: :::* .
.... .... ... A .. ............... ... * .. .. .... .... . ... I'll .... .... .... .... .
14 ... .... .... . .... .... ....
. .. ... ....
... .... ...
.... .... .... .....
..
D q-ft ..... . .... .... .... .... .... .... .... ....
... .... .... ..
.. .... . .... ..
.... . .... ..... ..... ...
.... ....
. .... .... .... ..
I:% .
.... ..
......... .. ....
:. 3 W 4- 1 : . . ..... .... .... ...
:: 1 .: T*. _ H -N .. .... ....
... .... .... ..
T- . .... .... ..
N .... .... .... ... . .... ...
I. .. ..... ... ... .
.... ... .... ... .... .... ..
.
....
. .... .... . I .... . ......
... .... .... • . .... ....
.. ..... ....
.
. .... .... ....
.... .... ..
.... .. . .. sw . .... .... ... .... .... .. .... ..
.. .... ..... I ... ... 1 -4 . .....
.... .... ....
M ... .
. t t TP T o n4 ♦
L n
... .... I T.. tam ... .... .... .. .... .... .
.. .... .
.... .... .. .... .... .... .... .
.. .... ....
.. . .... .... .... .
... . ... .... ... .... .... ...
. T+4 .... ..... .... .... TIM ... ....
I iT .... .... .... .. ... .... ....
" - f .... ......... ......... .... . .... ....
. . . .... .... ..... .... ..... .... .... ...
.... ....
.. . . ... ... ... .... .... ..
H:: ....
7t7... ...
. .... .... .... .....
. . . .... .... .. ....
N.. . .... .... ..
.... .... ... . .... .... .. . ..
. .... ......... .... ... .... .... ......
......... ... ... .... . ... ... .... ... .. .... .... .... .... .... .... .... ...
.... .... .... .... .... ...
. .... .... .... .... " . .... .... ..... .... ..... .... ...
7 ... .... .. ..
... . . .. ... I . .... .... .. . .... ...
.. .. .. .... ...
... .... .... .... ...
.... .... .... .... .........
.... .... .... .... .... .... .... ..... .... ...
.... .... .... . .... ...
. .... .... .... .... ..... ....
.. ... ..
.. .... .... .. . .... .... ........... . . .
....
.. .... .... ..... ..
.... .... ....
.... .... ...
:,**! :.:! ^:: . .... .... .... . .. .... .... .... .... .... . .. .... ...
.... .... ..
.... .... ....
A r ... ....
.. .... ....
... ..... .... .... ...
.... ....
W ... .. . .... .... .... . ::, .. .... .... ..
... ... .... ... ... .... 4— ... ..... .... . vt... .... ... ... .... .... .. .... .... .
2- 7:.. .... ... . . .. .... .... .... ...
...
.... IT: . .. ....
. 7 .... ... ...
....
. .... .... .... ... .... .... ..
... ... .... . .... ....
..
.... .... ...
. ... .... ....
.:n 2 1 . . Mi l: + 2 4 ' .. .... .... .
-12 * : - 4 4 J.
7 7* . .... .... ....
Figure 25. Comparison of Fifth-Scale Pitching
eiit Characteristic -WMI ill Pitch for Bastc Fuselage ttl i th 1t#fl: 4.
4 tit i t I I 1 Ui i:u .1 ..I. it.. 1 j4 t- I t T -1. ;I. t IT. 4 ' M I M it; AIR I 4 .
+ '14 l ij i 1 1;4 1 1:.: .ii : • :.t*: I T Ii 4 4 4 1 t I .^t4 i 1 It I l j ; ^- ^1:i 1:p :I t m: H14 H I f l -' MM, m, 1. 1 ... M I M. I .... IT IM01 1 t I I I IMO: =It i km/q-ft I t i it 111.1 t: I N, .... .. I ... .. ....
it .... ....
.. ....
M, 4 0: N, 0"I tit - t f + q jj+ ig 1 1 UtHI; - 11 H . M. %.I I -.;.I Mt •U i t It 7 t. IV t - I T I, If I 4 4 t o l t .. I .... .... ...
it W I 1 pi . 1. 1 i !: *.; 1; IM j4 N, NE,;. I 1.
. .... ...
it ;at ;;q --i. I T . 1 I.: 'n, "I -;n + W.E.
1' ..
;..; .2.
t nm [tit ti 1* 4 1^ It . It; rF 6 Vj' +, 12-.: ::.1 _j.
... ... I.I. N I Oi ... T I ..... ....
tM , :: i i;v 1 .:1 41 M. I 4 1 1 i 1 .: In, A 10 I I It. 1. I cc^ it I.— t i It M , tit T I II MO i Mll ! i IM ' M 1:1: IT .. . I . .!!! ** :1:, 7 1 . 1 .1 1!.: 1?:; : 1 v.1 ."S 31% 1 t ti I CC) tit , t i: TIT it 0) J A I np ill: ii % -.1 I .:: mn . . . I :i V in 1 . 1 M: M; IT IT • Tit. I I . , I ' t 1 11i I M; m i Fl. ii 1;!T.. ip; ,..I IN 114 ' t! i t WHOM, I I t , M, I, 4 0 *1 I ti V I t i .I H It A HT + 1 1 . 1 t ! 1: 1* + ...1 IT t li t , i!j! J:;" J . 'i M.
I tit j I :z:: T^ m: " - ; i , ; i i t1p : ll -.q T: trf IN it: T n. I I .... ^.;4 I 'til I li: !I i , . , ! ! * i t=* IT.: n t i t 1 44 41 tff ll fl I ♦ ii t i 7t'- .... I ... .... .... ... .... .. H . .... ... .... .... .... ..
+ + -i t - !... . I I .
I II a .
41 , 4 - T , 1:1 W? ^:W I lit i l l , til M * 1 4 *1 1 , it 'i" 'L Run 2 550 SWT .. .... .... ....
lit tIff a I ♦
Ru n t
It +1 it It t . 1 11 11 t t I R.
I l M t Hillit": I H H I M I . .. ... ....
1 :'14 Il I H P..
O t t It ! ,' H M.
I I!- N " I ... 'it Iv! IT; N. it. I I I't I. I: I .... .... .
RE . 1.. I _ 160! - 1 4 - gn .. 4 ... .... .. ... .... ..... .... .... ....
I lit , I 1! ; 4 I l I . To I T ♦ l 4 H W I T W M, U, . * " M + p.
X n. M I .. . ......... .... .... .... ....
T.t 7 t. .4 i E. , I. I 1 - 13 A IT !lit t t![ . ... ...
q ' s t .. .... .... ...
+ i .... 1. .... I... I . ....
! IT. .... .... -. .. ..
1 . v 1 1 2007 - .4o I +1 w i i, t::1. : 1 :* IT*.
m :iliii: . 4 iffl- M - T if f il, RH 1: q MM I f 10 f t f TIM .
: !It; I f I T t I n 1 4 * T it m - 4 W IR, :. .. .... . I. .... . .. .... .... ... .... ........
IT: T .... ...
z I III. 1 ... 1 .1 11 4 .1 .1 ..
t tit . 91; T W, - .... ;.;* !:: ;;;1 IT .... .... ..
° i 'nit 1 1 11M 10:11 --i ...
1 14 i t I 14ft , I. .... ....
I'M 'tt I- I I T.
I T t _T;71 1^ I ^^ I ......
..... I .... .... ...
IT ... 4 1 or"IMNA , Cll:-^fl-"" :'El Of POOR QUAUTY ..........
Tt- mzm- Vr— Tt"t :J ii I t i ^ i4 .r4 .... .. .. .... ... . ..
to t-I ul Fzi, -r4 ld
C)
. ... ...... . .......
LL -A EA -p tf4 co dJ J."T Cd m 41 7 v r 1 P4 T-1 wH tH 0 p EH _i..
^, f _^.: .,_ ^ i ^ i:. -^--r- -ir-'r - • -^cn ^- r =^ .
.c a t - r .^ •^^I ^ ^ I ^i ^ w TT •0 -p T"t (d 04 P4 f^ 0 0 rj •r4 07' CV ILL—* F:7 7 j ;: 'I -.-1 -' : 4 11 '...T . ' 1'7 t t to Ims.
Figure 27.
Comparison of Fifth -Scale .. ........ .... . Drag Characteristics - in ...
.... . .. .. .... ....
T:: I— . I.
.... ... .... .... ......
Pitch for Helicopter ♦ • ... .... ....
LSWT 550 Run is .... .... ....
I ..... ....
. .... .... . .. ....
... ...
I.
:3 r .
LSWT 6 300 Run 47____ .. ...
. ... D/q-f ... .... .... .... .. .
t !V: ... .. ... ..
.. . .. ....
- r7 7r:7 .. ....
....
.... ...
.. .... . ... ... .. .... .... .... .... ... . .
I. .... ..
• r t .... .... .... .
1:w...
....
...
.... ... .... ..
!-ITT N 1: ... ... ... ...
IW .. I .. .... .... . .... .... . .... .... .
:Ili j n - 4 1. ....
iii .. . .... . .. . .... ... .
... .... .... I . ....
.. .... .... ....
I ... .... .. . . ... .... .... ... .... . . ... .... .... ..
ILI. :: , .... ...
.. .... .... ....
0... .4.. mv i.
I t 2:7 .. .... . 14 . .... ....
.. ....
.... ..... .... .... .. .... .... .... .... ...
14 1. 4 t 7:4: . .... .... ...
i .- " i. i44. . i. o tM In- :T: .. .... ....
... .... .... .
'M ti l l t I" ♦ Ul; M . .... . .... ... .. . .... .... .... ... ...
.11, 'I J IM ....
.7.T.
.. .... I . . ... ...
tit! - til CC) I = ... ...
W.
7 7 T= .... .. . ....
CC) aYa .e• .. ....
.... .... . .. . .. I n-1 ?T .... .... ilu . .. ....
; i*i ...
-=12F ... .. ... ....
I lb E l l .. ....
CO O .... .... .. . . .. .... .... ... .... ...
m 4:1 Z. I 1 : w .
1.: ":1 : : .. .... .... ... ....
4 It .. .... ...
. .... .... A i * t4i IM t i ll ^iwa - am... - . .... .... .
10.: . ... .. . ... .. I w_.; w ....
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-:3 ni: ....
is .... ... ....
.... ... ....
..
. .... ... . . .... ...
q'; "It . .. .... .... .. .. ....
Lill ... ....
nu yy I .... .... ....
.... ...
.. . ... .... . .. .... I i:v i.
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.... ...
. .... .... . .. . .. .... .... .. I .... ..
..
. ..... .... ....
W. • .. .... .... .... .... . . ...
...
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tjy + ... ....
T'7 ... .... ... v.
14 :?t l "n .... ...
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;IR
Ri
♦ T IT 17. :F F! .
ai 64 .
!;:v. .117 ttI77-, .1 i s Y .
` igure F 28 .
ii :t j iY i . ' z t .z }i` :a# Comparison of F e
+r ifth~Scal pitc hxx>.g +
+F I.S. tF 1. ; I: «.:' `t f ` : :i r1 £ Z" :j} t3- I' #..' }'£: ' #I ID S : "T j t. ' ' I oment Characteristics in Pitch i.
Y.
1 4 ...
+Y. „3 t.
f : } 1 ^ tax He a0^ter '} f t - • li r i.
3i f^a- ^Id + '}. + q 'J{ is `^ ! .t r °' s y .9f t t ? 7t: } ' ♦ I } t!I , I" .l I ^1: I i '+ :ifa I: P f :t :: •i:^•+ 1 t rY t , ♦ 1 ,. fit. +:• i t) t 4+ , 3 :' } i ♦ *.
i I :'•' ' t; . 1 St , 1 ' # li itF 1 " f r '} I J i t i t 1 1 #} : : } f:i - O W r#2 , i' }'" Wit+ f t 1 1 3 " t i I i 8 # . iti.
+} . i } 2. I "; M it.: ; , }} { 1 i is ;1 f :i }i#c }.
tift f? f t ! fi» # : I N t ; s f • ..
:' II I1.. j ' .• • I •! +^^ . •.. •"ri ^, f. .
! C (t 'p '1 i ; i: t; t: .i i , i t t*' iM ,i c?t :.:• F . ` +t} tIi t#'" ' II} + I ` ' } . : i 1 ;.,a ! {`" •,{ 1i 1' " f' ,i,1.. t 1...
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LSWT 630 Run? #}' I.
:t I i :t t :r ^. :s::::t ir ff,i i f :1 _i. Iu' # 11, ^t ' 9 :l. f S -f • : :i: ;: i,i :,- "! "+ 4 , : : * I 1 i^: .+ I d , .$ -I#S f ♦ i + :r I+i 't' : :1 af. 4 ,f. 2 a. t > :i: ..:.
i !. :+3 ,t' ; .
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.
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.. + } + !'. t ' "7 t ^^ j t I• ^i. a Si" , a ° 9 t 'a a + i t + t , - ', t. ♦ D I ' 77-i' •} F I Yt { + f i , . '- Y .f T !} + v Y . fft # a.. i f1 i'} t , } r 1{ t' 1* ' 4 0 .*,,I +, " r I t{ii i t: 13 ,«; F:'I F ._. tt +.. ".,:, lsa: 1 ' + f I Fj I 1 I., f'I i , =r`- ; ♦ , + t F1 2 , i 1 + ,IT T ri to t t.: t r UUU ' uo- pgg p U » .. .... ...
':Q =: .... .... .. .... .... ....
......... . .... ...
. . . .... .... .... .
I. .... ....
... .... ... .... ... .... ... .... ... .... .... ....
II .... .... ....
{ . ^_ .. .... .... :; .... .... .... ....
IN: W.: I,.:: I: M. I: V^ 1: 1 .... .... 1 :. • i I i 1; i i i 4^^ `® .... ...
. . ... ....
i7 "r1w: 1 .4 "1 111. 1 1 1 ... .... ...
... .........
... .
f"r ... ..... .... .. ..
TM ....
'12 0,,^ ... . :T TV^ T .... rTr t= Tr="^^ ....
... ....
... . . . . ...
T-rr . . .... ....
... ..... ...
, -deg . ... . . .... ......
Tr^ -20t .. ... ....
LSWT 550 Run 24 ...........
1.
f 630 LSWT 4 A . .
. . . .. .
A v 71 w •.
0; A 6 01 . .. .....
on; 1. t
Figure 29. Comparison of Fifth-Scale Side Force Characteristics
in Yaw for Helicopter OnIGIM 11 1 PACM'" Is ()F pOOR QUALITY ... ...... ...
..
.... .... ..
31, LSWIX 550 .stun . ..........................
1 T4SWT 630 1^= 4 8 ;v 3 41^ VIV I!*.!Vt,' 11 V V . .... .....
it .. .... ..
A IA U 11 1 11 ".. ::I.; ..... ..
4 v;:;:-:: :t, . ......... .... ....
u « :•1- IN. Hf* 4 ... .... ..... .. .. .... .. .. ....
.................
It: .. .... .... ....
I U.
C, Zt., I= D 4 44..o. Ll i. :4 4 J * . , 1 1 W.
. 11 :1 N 1 *1 1, M * 1 I* : a, : M.: . 11 *1 + :..ii i s' i a r.
..... ... ....
1. 3 . 4 ♦ ..... .... ... 4 ....V— * 1: 1: t I L I Z r : 2.. 1 1, =4 k :U1 H I T 1.4 g^.
. .
.I nn ... ......... . ......
...
= 4 rr.
.::t 14P =4 % Eff — f- Ell, Etil • 4 71i: 4: I F Ir il i n: +E T _ R. - 4^ M.
_ 11 ^ i ll u l= 4r.
4- ff a + t + + a l RsEt =Z =+ I E ^44^ 4—i E ;ITZ .4 44 + RER 1 XIII I . T : T== _- I tr:z B+«}, E +.« lz^ + 0_4 Mz EE MH 11 :4E 0 __ 4 .1 ^g^ , 3 2 :=T 7 l ... ... E4411-1 t Fig=e 30. Comparison of Fifth-Scale Drag Characteristics in Yaw for Helicopter gv I. .... : r. t I'M !I It S I. 11, 1 4 1 H: H I I N 1.
I- 1. '1: n . .... .... ....
..
nq h , M. 43: 1. .... V T .4.o . I". III,.
4 .1 1 tir I M 11 . * ' 1. 1; '1; 1 mil 1 t 1 M ^; t l: ^iIt .... ...
IT. Ti i s tt _1 I.:: H f. 1 tt 4 I— I.R LSWIT 3,5 0 Run 24 M: I 'T 44 iT + i : .
' M + LSWT 630 R un I 1 1.- I, I. M! I I I 4 14 H - 1 1 , 1,11 "ll 0: 1 "1 ItIM.- I* YM/q-ft .. .... .
..... ...
I-:- HM : -7 I.: ' .1 t —I :1 : ' I'M I .... ..... I in : :3. 1 U:1 r:.*, Inv It" IT 1 ..:, 4 .14 1 I LI: til l f i v!
....
ZVM: = ♦ I. .. I ... .... U.
In-, .t * -1:11 :^t: " I * .1 r 1 1 1 -1 4 1. I I. ........ ..... I . .- 6-.
i% eg . ....... I V I :.77---ttt T — ...
44 =4 vi; H EN 1.
:3: t l! ;.4: T! * .: "ra Iv; :u 80.
tt, Z lrll W1.1 p: rt -;xv t, r_ l t t:.
Hi2 ilL ..... .... ...
.....
.....
'Itt:......... 1 4 4.
:m!v— r: '=*tV ni nz- MI.
Ul.".1 11:11 .......... I t, ... ...
TI I * W . El ..13l ii^ i I t". ti."!1 t= M. ^4' t =T.
T:::— .
S4 iHi^ .
'xt ... ....
I.: a :M tz: T: -:V, qj.
Figure 31. Comparison of Fifth-Scale )'awing Moment
Characteristics in Yaw for ReUcopter or POQ1 k--))O' QUA -UTY, ...
K .... ....
t t a='n
' - ft I 2
x 80 Full Scale R un 4 0 1.* 41:
L/q _ft2
LSWT 603 Run 10 ! .
.... ....
13' 4 3" U.... N U I.-T :.!a . 1 1 :1 M..
2 1 N 4+.- - - mo VV "TL - Z-z Z^ + . 14 . ..... ....
V 'N % H + .. .... ... ... 4 - . 4 S^^ .........
-46 t : . .......
I v.--ov t jt4 tj4 'Mt
a--deg E=1 1 = I=
M^ ^.o 4= 1 4'^* i+ + L -r ^i: HK lRi + 4..
+-o4 4—' ^ i4- 4 44. 4— J— a t M, 437- • +-+ + =M :^i.= += gr ...... -q R'" a t 4 zm4ttt 5.7. L.
I. ....
m4- +
.... . .
i1i 4: + rM.
11 Ila UM: i1B
Figure 32. Comparison of Tare Lift Characteristics in Pitch
for Three-Point Mount
ai 't2 is t t!
{. ti
i`
D/q-ft
t• :> 40 x 80 Full Scale Run
t.
LSWT 630 Run 10 `
= ii ii ii _
t. 7
kt.
i _1 • _ ' J: 1t , Oi.
-16 ::121- -8 -4 14, f 8 ` :{ 12 i16
cx-deg.
LE 21 a...
Figure 33. Comparison of Tare Drag Characteristics in Pitch
for Three-Point Mount
OF POUR t . ... .... ... 4 M. t ... .... Ml 3 M F. c r- s t i .... ..
Pm/q — ft .. . . .... .....
.... ......... .... 'M x; - n ::::*9* ; I*: H ... .... ...
:U 1% ; * 11, " I :.,.* I— .. ... .... . .... ...
. ..... .... ..... ....
...... .... :... . ... ....
. . .. .... ... ^ '... .;' ^=. • .:* M I l N . .... .....
11. 1 . w— =N11I.—.^ ZN:1NIN :.'n I + s. ..... .... .... ..... .... .... .
i ir: .... .... ... z; .
... .... ..........
44-: —12 12,"; M: r t .f pi l ... ....
si ; ;U , 1'ttl na I V. :u ... ....
a—deg U N 1. 4 ..... .. it M. ... ....
_LU ... .... ....
.
^i i t r I t , T' N.
I ' l -i Nr I =4 11 714;S Z, =. 'Z a l +;4- ; ; 1 . 1 -;r- uu t;' ^z n ^yy .
t ::- 4 e - ca .' L. 1.1' 40 80 FU 1 4 .4 IM: = 1 l . 1 t 1 0 lUt : t=. l ::! t '1: 630 Run
LD M
+1 I V. F, N; ltt^ 4 t"r=.t" -.rut V.
30f f t m i uf r 4 : Iii Elln'H ttz4- 't Iii - T : MU - 4= =Z = - Z 31 - .1 ^4 ... ..
^ 4 Z; MUT .=Mt: 0* auu: ' lz:: l . ` Z:1 :r_!
M+ lU
Nn' !
U M T.
'-' k__r4 F F_ Fl..
Zt 1= R Fo: *Z: *4 Z=7 FM ta L * . * W:r 4 1 +z : M - + 3rr + 4 4= IF M_ if= ; n . _f -v ^ -..
bi !Z=M + -B. ffl#P- if :Trr_ Z M t;.
m +M. , I — * +: EM 111. .=I + — - - RE I Figure 34. Comparison of Tare Pitching Moment Characteristics in Pitch for Three-Point Mount QUnUVU.
Few, :tN E ;
40 x 80 Full-Scab :Run I 1^
j;T I 40 x 80 Ful 1 2 -Scale ^^Iun 2 t..-: 14SWT 630 M :4 .... ... 7777. .. .... ....
.
rt
1r: TI: ,- q ft Y/ is .. ... . .... .... .... .... .... .... .
.... .... qv
is fi M!
.. .... ....
. ....... ......
.. .... .... ... .... .... ;6; V 8 4 .... ....
I qf+_ . 1 4 ......... ..
t; i i+ .. .........
... ....... %: .. .. ... ..
.... .... . ...
.: 7* • ...
V.:A: .... ....
... .........
.... .........
% ... .... .... .... ....
.. ....
IF -72
Comparison of Tare Side Force Characteristics
Figure 35.
in Yaw for Three-Point Mount
(OMONY.^% Pt.,(7 'z- C3 OF POO R QUALITV nz ^jp M un i a n Zt.
l i t .. .... ....
_E4:*.*1.:!*. I 1-11 E.- ... .... .4t ...
.... ......... ._**4'.M 4_= V1 ....
_I -.4 "f V. :Z:t ^14 m_ * .*=4X:!:.' VM I Tt V : 1 _ 1 . r '.T*+j-*.*.+!: 4 til.:: 4-M M.I....-I.... t i. , IZ ....
7 t . zl= I r*.
: ,I« : D/q-f 80 1: 40 Full-Scale Run 1 .1 E HIIH - LSWT 630 Rian 6: ^j A 41i, H: =tZ=z = ++
.. 7 = . 1 Z 4 1
l E
2.- =M 1 v 'r 124 1, Figure 36.
Comparison of Tare Drag Characteristics in
Ywa for Three•Point Mount
Uj U OF ... .... 3. ;1:1 1 tv. ^!:I: in. 4-1 N'4 1 . ..... .... .. .... .
4 1 :3 S r• I M.... .... ....
= 2 Tz- .. Tr^t .... .. . ... ...
---i tti^*L ntu "W IIN . ... ....
. .... . ...
.... .... ....
N s *1 .... .... .... 1 4 1 : 1 J!
+... .'. + vii .,. 3 .Run .
..... L I-I t :
40 x 80 Full-Scale un I'
YM/q-f t ' fill s0 Full-$cale Run 2 W1 4 0 4^4 .. ....
L8WT 6 30 Run . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . . . . . . . . .
1;;,: Iv! t 1 4 . . . . . .
• 1:.
. . .
. . . . . . . . . . . . . . . . .
....... .... I .k. t ..tt L *. :^u: :lM I!" gn . 44. .... ...
.... .... .... . ... .... ..
T tit : 1L, " A ... ... .... .... ... . .. .... :- ......... ... v".
ttr .... ... .... ..
.... .... ... .... ... V: 1.4 V.. —a— ..1 . ... ...
. .... .... ..
. .. .... ....
^-deg I . - I-q- ... .... ....
.... ....
.
7 71 14- 1... .... ...
........ ...
- P -i in ........ .... .
j: ..... ..... ...
.. .... ....
.......
... . . .
mr I n' I V. 11 : t l .: : 10 7-V ..........
.......
....
-at: Figure 37.
Comparison of Tare Yawing Moment Characteristics
in Yaw for Three-Point Mount
^2) Qr . Poor. QmllLrk", .... ... 1: ::.v.
'I.: . ;I: , . IM, 1*:. 1 : 11, .... .... .... ... .... .... .... .... ..... ..
'tl ... .... ...
..M :XT: .... . ........
...
71,7 ...
.. ....
-.M .. ...
gi 1'. .. .... .... ..
.....
........ .... ... r : 1 ... .... .... .... .... ..... ... .... ....
J!V ... ....
... ...
V U :. .j. . ♦ .. ... ..... .. ...
. .... .: 't{{ M v i • I l — M * t ; i . tint Nt tif J;.:: ..... .... ..
it .
3.
In . .... .... ...
In nn it I"! It rt i t IV. 7 4 .... ....
.... ...
...
.
... .... .... .
.... .... ..... ...
... .... . .. .
... .... .. . . ....
.... ....
.......... .... ... ..... .... .... ...
....
. . . . . . . ......... ......... . .... ....
. .... .... .... ......
....
.... .... .... ... ..
.. .... .... .... .... .... . .... .... ....
::I.
....... .... ... . .... .... .
.... .... .... ... .... ..
.... .... ...
t :S Ut.
... ...
.. .... ... .... .... ...
-deg 3- 2 .. .... ....
'ti .. .... .... .... ....
z I= s1.
t.
.... .... ....
... .... ...
40 x 80 Full-Scale Run 68 .. ....
LSWT 630 Run 85 630 107[ LSWT Run Run 108* LSWT 630 LSWT 630 (with grit) Run 109; V ^4 M.
t. 2.
- of Full/Fifth-Scale Comparison Lj,;ft Characteristics Figure 38.
in Pitch for Basic Fuselage OF p0a, I= v.
. ::2::i:: ... ..........
I. ........
H IVII 8Q Full-scale R un 8 :; 4Q ... ........
L$jI 7,T 63 0 R 8 un 5 H", 1M:I - , .' v i M: 7_ LSWT 630 dun 107 1 + Run rm g; . 4: 1 . =M* - LSWT 630 (with grit) Run 109 rx . B. Z . : i! : -. I-E R' ":: t BSI 2 21 r .r. rm- — -.4 is
M
FF ru .4 . 4.
8_4
:21 va -M =V^ j Ri = 4 r lz Rr a--deg + M.
39. Full/'X 'Fifth•Scale Comparison of Drag Characteristics Figure in Pitch for Basic Fuselage OF POOR QUALITV .. .... .... .... .... .... .. :... .... .... ........
.... .... .... .... .... .... ... ....
.... .... ..... .... .... .
tn' . .... .... .... .... .... .... .. .... ... ... ... ... ....
.... ... .... ..
.... .... .... .... ...
. .... .... .... ..... .... .... ....
-f t3 '*15.17- nn mTm- .... .... .....
i.
I N H ..... .... .... .... .... ..
I:: V!l IV!
41- ... .... ... ....
... .... ..... . .
.... ....
.... .... .... .... .... . .... ...
. ......
Ir .... ....... ... .... ... .... ...
16 t 2;
19 L
' :7. V.: rt . . . . . . .. . .
.. .... .... ......
. .... .... ....
. . . .... .... .... .........
.... . .. .... . .. ....
S. 71: n .'!:4 .... .... ........
... ... ....
.... ....
:S.
D. . .. .... .... .... .... .. . .... ...
... ....... . .... ...
.... ......
---r r.
-T- ... .... ....
. .... .... .... .
...
-40 x 80 Full-Scale Rurx
: 120
LSWT 630 R= 85 LSWT 630 Run 107 LSWT 630 Run 108
630 (with gri t)
LS WT _ Run 109 -160 Ei.
. . .. ...
........ ....
.. ...
^* .. .... .... .... .... ..
200 ^ .... .... .
-V ...
.... ......
of Fig-are 40. Full/Fifth-scale Comparison P;Ltchinq Moment characteristics in Pitch for Basic Fuselage C m L/q-f t2 . .... .... ..
* A t :: V :IH 1R..1 12*.-.:..,.
a-deg 40 x 80 Full-Scale Run 69 LSWT 630 Run 86 LSWT 630 various Run 110 LSWT 630 grit Run 1.1.1.
LSWT 630 patterns IRun 1,1,2 Figure 41. Full/Fifth-Scale Comparison of Lift in Pitch for Basic Fuselage with WAIIIngs 1 1 333. s 13VI: M;: N V ** r., V., . .. ... .....
.. .... .... .... . .
. ... .... ..
.... .... .... .... ..... .. .... .... .... .....I...... .. ..... .... ..
R
IS..
..... .... .... .... ...
I t2, ... ... ..... ..... .
A 7-: .... ...... .. .... .... .... ....
.... .... its.
..
......... .... ...
... ... .... .... ... . 1 0 .. .... .... .... ....
—, .-.- .z 75 -..:I D it . .........
-LL Lid
sT
M .... .... .... .... .... ... ....
H. HN
... ... S X.T 1::!
... .... ...
. ... ...
.............
.... .... .... ... .... ..
... .... .
. ....
. .........
.... .... ... ... . .. ....
.... ....
.. .... ... ....
40 x 80 Vull-,9cale Run 69 , 4 LSWT 630 Plun 86 t.
1 LSWT 630 various Run 110 ... .... ..... .
... .... .. .... ....
LSWT 630 grit Run Ill I1 i .... ....
patterns
LSWX 630 Run 112
2-
T
... ..... ...... . .... ..
1 —::*L4.
I. -T ^1-8 eg .. .... .. ...
44"
.... ..
Figure 42. Full/Fifth-Scale Comparison of Drag Characteristics in Pitch. for Basic Fuselage with Wings .. .... ....
r, r4 8 0 ... ...
* ... . .
XW . .... .... .... rn . .... .....
.
I I T ..
.... ....
.
.. .... ... ... ...
i .... ... .. ..... ..... ... ... ....
... .
PMAJ-9t, ... .... .... .
..... .... .....
1 , I LI . . . . . . . .
...
Z: 11 .1: 1:: . . . . . . . . . . . . . . .
01 ...
.. ....
i ^; w 7;T . -Ot .
... .... ....
ip .... .... ..
i!* W.
♦ ♦ 4::' : ':' - j:; - t . . . . . . . .. . . . .
. . . . . . . . .
.1 . M ... ... . . . . .. .
I le M . j . . ........ .... TL7.
....
VN 'N I— ir .. .... .... .... .... ... .... ..
-deg nt' -^-r ; ^, 01 .... ..
"m I UIt ::t: V.1 1 N I V 1; N Z I..: tr I_ N %:g: : . -%.
t:;. : .... ... ....
• 8 .... . .. ..... .
q. - ...
... ... ......... .... ...
40 x 80 Full-Scale Run 69
WT 630 Run 86 LS arlous 630 Vic Run M L$WT 11 0 l !";%. n ^.=_, 7*7_11 -1. ... ....
0 ... .... :4 L^3WT 630 grit Ill : .. . .... ...
Run 630 patte=n Run 11.2
L SWT
v_ :,R.
........ ....
14 S 7 M: =4 200 ... ...
4=7 =;T T. V 7-71 .,Mft:..
T: Figure 43. Full/Fifth-Scale Comparison o4 Pitching Moment Characte--istics in Pitch for Basic Fuselage with Wings M . I I . . . . . . I . I I I I I I . . . . . . . . . .
ZU.: I: m i M. M , III . . . . I . I I I I . . . I . . ; .;k ... ..... .... ... .... .... .... ....
t-7 !F Mt.
NI .... ... •W • .... .... ::. l . tynr{fl V=1{ + I .........
III M tv. I. ....
V.
r 4 1 I I I I I . . I I . I I I . . I % I v U n, ... .. .... .... .. . .... ... I .... .
L .... .... ...
... .... ...
M. UN .... ..
4, M 1, 4— I .... ....
% 1 N , I N V • mu. , 4^4 1' a 1 v I ;. I tu * .1r; nn:v, UT t ... .... . *:LJ4 I :* I I ::t 1 1 1 In . W.: 3= at— ... ... I na i+". .... ... I "" .... 3 U, .. ..... ..... ...
..... ... .... ....
81. , .... .... ... ... .... ... ... .... ..
.. . I. .... ....
1--- 4.
N": .1;1.
1 M -4 I 1.::: . ......... .
... .... ...
... ....
. .:3 ... .... .. .... .......... .... ..... .. ..... .... .... 'I ......... .... ....
2[; ... j . ...
L V.
+ "n ".11-UUN.
M U eg M- ........
.............
=111*! M.
r v 4311, Ull N M H i i ... .........
41:4 t!:, I 'N *1 1 1 4 .*r!r:: IT n = W. I.
El i I is :is I U. 4 ::U U ^R 111 '41 :11 '. * ..W * I ' I; I 3= , Tt M. —4o ov. 40 x Full Scale I R un 31 80 .
. .. M U' v I I I M I : v I .- , I, I q- 75 L$WT 3 ....
7::; X, 2 q=loo 12un I go LSWT 630 X 1 q-75 dun 1.20 LSWT 630 with I+ t tj q--100 Run . grit LS'KT 630 1 4 t: .-:4-4= Eli =-t 7=1 M. .IMM: 4 0: Lt uz !;.t 1*1: I . M: ggl g M .1: n Figure 44. Full/Fifth-Scale Comparison of Lift Characteristics in
Pitch for Helicopter without Wings
OF Powz Q,,UALVrV . .... .... .... . .... .... ...
. . . . . . . . . . . . . . . . . . . . . 11 . I n 0: ... .... .... ...
. . . . . . . . . .
+ I M. T, . ....
. . . . . . . . . . . . . . . . .. . . . . . . . . . . . . .. ... . ... .... .
+ + + ... .... ...
+ . . . . . .
.... ....
,.tt .. .... .... .
.... .... ...
...
...
... .. . .....
- 4— ... .
... .... ..
.
.... 40 x 80 Full - Scale Run 31 'D/cl - f t Run 99 .... .... ... .... . LSWT 630 q= 7 5 Run 100' 1 . ......... L SWT 630 q-100 4 t.'.
0 ' ... .... . .... .... R unt 12 q= g LSWT 630 with 7 5 6 rit: q= 10 0 Run 121t 30 . .... .... .... ..
. ... .....
....
. . ....
+ 4 1 - 4i t . 4 1— .. .. ....
mv"....
_4 1 :*1 .. ... . 4 ;: I U .:41' 1 _11 A:4: 4— rn! I. 9r. — .... .. ..... ....
4.
+ + + 4 +.;4 4 4 + + +.; +.; +.; 4 1 . .... .... 44- : + !
d ar +r HHIM, ^ ali^ TH' ' E .. .... ... .... ...
i i ^ 0 Ya 'i-H - H E t: MUT + rt .. ..
.
+ M -4 4=1 + F^7 44 t4t= =Ivzi ++ 4--4 =t^t Z:T'^-4 71. t f'.
=-1-- + - 1 I;;.+ 4= :4 4 +
"` t r 0
L
„x + 4 .
ot-deg 4 rz.t L". , I I, r EZ zT=+V_ -4 LIL_ Figure 45. Full/Fifth-Scale Comparison of Drag Characteristics in Pitch for Helicopter without Wings :1 :V 7. X: .... .... ... .. ....
. .... .... .... .... I .... ....
.. ......... .... I .. .... .... .... .... .. . I I . .. I . .
.. .. . .... .... I I.
..... ..... .....
.. .... .... . .... ..
.1111:1 . .
:Ot . L t • i t I - IT: ... .... .... ........ ... .... ...
I. M: I to i t; I.::: M" ::.I I I: * IT: , .... .... ......
It . ......... I...
IT 1 * 1 ... .... .... .... ...
ii 0 x 80 ^ I ull-$cale Run 31 ^Idjq - t 3 ... .... ...
K 145WT 63 0 q=75 Run 99 . I., .... ....
Run 100 .:.:W LSWT 630 q=100 s.
v:1 '=1 1 I M q=75 Run 120 LSWT 630 With . .... .... ....... ....
..... .... 630 gr it ^q=100 Run 121 LSWT :iV SS .... .... .... . .... ....
.. .... .... ... .... ....
..
I . .... .... .... . .. ........
.... .... ..
.... .... .... I.
f Im . .... .... ....
... .... ... ...
.
4. ..80. 4... 1. . II.....
I .... .....
..
.3 1 .. .... .
...'i kL.. ! .1 41 . 1 id -:1 ... .... ......... ... I tv: ..
.... . 0i 7 ....
r.
.. .... ......... .... .
lZ ' I. A , 6..
I 7= 1 tilt ... .... ...
IM- _7 1.1" .1:41 1 I ... .... .... .
- 8 0'.
"I* .... ... .....
Figure 46. Full/Fifth-Scale Comparison of Pitching Moment
Characteristics in Pitch for Helicopter without Wings OR 'g , IGINAL I or pooR QUALITY .. .... .... .... ..
... ...
30 . .... .... .
....... ...
... .... .... .... ....
L... ..... ... ....
... .... .... ......... .... .... .... .... .... .. . ....
.. .... .... ...
. .... .... ....
... ...
I. . ..... .... .... . .. .... .... .... ...
... .... .... .... ...
... .... ... ........ .... .... .... .... . .. ... .... .... .... ... ..
....
.... .... .... ....
s 0 .... ..
t ......... . . ......... ....
I MV 1.1:..
.... .... ... ... .... . .... .... .... .
.. ........ .. . . .... ....
In ......... ...
.... ..
.. .... .... .... .........
.... ... .. ...
Till IT^T :N; ;I " * 3 * ! * Z =V M.: 1. : 1:1 1 1!."
.... .... .... ....
.... .... ... ...
1 13 1 ^ 11.: :3 ....
7. 77t7 ... ...
N I.
. .... .... .... .... ... ..... ... ..... .... ..
.... ..... .. ....
.... .. .... ...
.
is j; .. ..... . ... ....
. .... ...... zn: .... ... .....
0 : 8 ... .... .... ... . ... .... .... .. -deg IN .... .. 11 .. .... ...
su:" Kil I M 40 80 )Full-$c4le 1 ^ = 20 I N . .... .... 11 '..
. .... ^j:L -Sc 8 Q u R un 21 .e : :40 ... ... ... ... Iv .... .... ...
Run 101 *: XjSWT 630 2 01 ......
*_N* 11= II : N, 12 L$WT 6 3 0 (With ',2 4.4 I^Uil 123 Y.
Ii8WT 630 ...... .... ..... ....
M. .. ....
**I . .. .... . . .... ....
..... .. 4., In: . .... ... ....
.. .. .... ......
.... ..... .... ...
.. .... .... ....
4 IN: LIM of Figura 47. Full/^'ifth-$cale comparison Lift Maraoteristics
in Pitch, for Helicopter
8 , 8 g IG Ir4AL PA I DE Is O ()V p O OR QUALITY ...
M.- .... .... .
-40 *4 -
80 Fu ll-Scale Run 20 x
....
x 80 Full-Scale Run
:4 0 21 ... .... ...
- '-f-gin". I M E' .
.. 1 1 .
630 Run 101: Oz .- ^.V: I .; M Rat - :h .! .
I ., ..:. I. , -.1 ,
LSWT 630 (with Run 122-
un. M;,i IT:, " :tt.
i z it DXq-tt V L 630 !*il
$WT grit) Run 123, r r 4 r. 1 11 1 4 1 -4 !T Vt4 211* 31. + i - " . . 'i ... .... .... ....... % . :V` ZI:; VVI JV_ t:: . f l V_ ... ..
4 V` .- .... ..... .....
;T: !v1Z It- N: :V 1 13: 1 ^ t .. . TV . ........
9, 1 _ 4==:. + . + TVIT. l i + M: ti. 41 M 77 x I' 7 1 .1.1: . * 1 1 . T -
F-7 T +
.... .... .....
ZV I % = 15M fflf f J; gg t.
' 4 41- 5- 4 L I -M .... .... .. 4 1 WE I -.nun.: + :1. 1. t I.
"'I= _1 .11 j . 4 ... .... f^ 41' 4F.
4 M : ',j+
j.1 . 14*
V_ q .. .... .......
4t t. u SH I UK-E.H-1: 10 2 - : It= 4 .... . .
4 11.
!7 - 7r!
3;:_ :=a=j::. t
Figure 48. Full/Fifth-Scale Comparison of Drag Characteristics
in Pitch for Helicopter
ORIGINAL PA M 10 ' c) F poor, QUALITY :IN I... .... .... .... .
I M :9: :I:: :It:. 14. W tx; N V : , ......... . M .2001 V .... ........ . .... ...
04-1-1 ... .... .... P t M
. ......... .... ..... .... .... . ... .. :-:: 0140 x 80 Full-scale Run 20 X 80 Cale Pun 21 Fu ll- 18140 IN . .. .... ... I 630 Run 101 r.
:L22 !
.... .... .... 630 (,with LSWT Run I.
VI: LSWT 630 grit) Run 123.
.... .... .... I.
.... .... ....
2 .. — ... .... ..... I. 1 W .
I. .... .... ....
I n. .. .... .... ...
.. ....
H!
....
... .... ....
I M: I .
Ill I Ill., . .... ..... ...
* 1 I::Z MUM t. 1m .... ..... ...
Zt...
Hzz ...
x.
. .... .....
4 0.. .... I. P ' 1 : Zvi Nil ... ........
:_ 1 1= ^* .44 WM:% IV IF Ur.
Hl M .4 ::VU qv .V i i 11H . -.1 F. I Z.
-deg *.rn: l *M =.Tzz: q. I ' l , "'M i n
W + 1, 1::= 11 ::= I ZV ...4 .. ... 1+
0 +
z
1VT
TI
zrn ... ... Ivi 4 *=r= 1-1 : " I:- I lm I, r . m.
+ *:I:. * =1Z , ZI Ef: .4.
8 =tt ;r ; ;7 V.. . U.- =+ • W ; tm zt _17M Ei-1 . 1 4 =MT =MT111 -Tr =4: =4H 1.
=V= .I= L - O ff , -Iff .
ffl lgfi^`V* I: MI T. Tl: Itt, + • I+ T_ HTr .... ... ..
i m Figure 49. Full/Fifth-Scale Comparison of Pitching Moment Characteristics in Pitch for Helicopter OF POOR QUAD 4 141 . . . . . . . . . . .
+ 0 P ... ... .
+ ^V- ... .... .....
7M. f 4
M: z. .. MR ......... ....
+T . M . ..., — " — .. .... ...; .o.. 'i— ...I na" s:.
i ii .... .... .... ..
3.. In if tmS 2 ! .,:i i.. ... ....... 1... 1. u.
+ M R IN El .4
i. ! . +If jijl ;I+,- - i f. U1.4
.... .... .. .... .
..
au... ! 1 ;1.1.
. 41
M
.40 . ...... ....
t + 1 +1 AIPM.,
! M - 1 . 1 1: 1 I M tht: +*
Lt^ t . .... .... .
...........
.... .... ....
+ + im 4 I.— + t I. .... ......... ... ....
gr
U Nula ''. 4 ; : I; i:, :1111 t g:. - 4 1
!
I . : !1.. 4 1. 1...
Tr t 'I.It*
1M r. I
... .... .... .... ....
% ........ ...
... .... .....
.... ..
tip + .A ^ !:: 3 i i`.- -16 (6 "l 6 24 2 45 i i 8 -8
- T7 r
^L g
$ -de .. 3 .... .... ......... .... .... .... .
+ r V.
... .... .... IN: -Lt4-L .. .. .
... +4 ...
.... .... .... .... .... T.....
M.. Mt M" i r + 40 x 80 Full-Scale Run 80 1 L5WT 630 'Run 96 ... .. .. +=
630 106
L^3WT Run I.M* i L^3WT 630 (with Run 3.18 630 grit Run 119 LSWT 1 S. ::714 7:: ... ....
U- 0 . .... .... ....
=t Nit -=—trn M.-I 4:1 - 1 =3 is xw. " n li ^ 41=1 . .... .... . I— + ra *3, 1 =+ 4 =I: .74 tt :4.
_t:: * nit t ttt.
Figure 50.
Full/F i fth--Scale Comparison of Sjcj,,^: a. , ^
Force Cliaracter- i5tics in Yaw for Helicopter OF POOR QUALITY 3..: . 1 : : 1 .1i MU . .... ...
.... .... ..
I T. .... ... . ....
U. IT W., 2. i .... ... .... .. ......... .... ..
.. ....
.. .........
.. .......... .... .... .... . .... .... .... ...
....... .... .... .... .... ....
... ... .... .... ..
. .... .... .... .. .... .... .... ... .
t.
....... ....
.. .... .... ... .... .... .... .... ....
_Ts t .. ... ;4 ..
*3 IT, ER .. .... .... ..... ... . ..... . ... ..
.... .... .....
j: - Tqq=' ^ M . + + P: M , .
+ = . .... ..........
T 1 4 4. 1 +n ' - ! =ry Vz.
=+ m--: : =4 M:i 4-1 .... .... .. 4..
..... .........
..........
. ... U r i, ........ .... ...
.... .... . M 3 d * It . . 7.
K: G. 2 + .4 I _ + 'uT T=
I . ... .... ...
I N 1* : TV IT. ........ .... V 1 =1 41 I ITT + 11 =341:1MIT.: T *." 4': Ml ... ......
.... ...
+ L:4 :T. 1 . .... .... ..
+= I.N. T: i+ 1 4 1 . 1^ ; 4 L :* 1: ;.- + . .... I. ....
q 28 It; lz: 4 *z .... .... . . ... ..
+ .........
q., M ,7 + + , I .
IT1.1 I =1 .1 It 7 71 .71... 1 zz 0 f.
IT Mt: * -1. 1 + *4 El- I= Z: IT- + TIT =__ + =+ t.y +
=ITT x 80 Full-Scale Ru n t:^ =
40 .;T LS WT 630 Run 96 + IT L S W T 630 Run 106 t: =z_ .4 IISWrX Run 630 (with 118, +
EN US WT 630 grit)
Run 119' M t- -3 M_ TM i4_ t+va l 5 =HE Figure 51. Full/Fifth-Scale Comparison of Drag Characteristics in Yaw for Helicopter nfl.- ir . M . ... ...
qu .... ........
...
... ... .... ..... ... .. .... ....
... .... ... .... .... .. In . .... .... .... .... .... ......
1 .-1 1 ... ... I t7:7 17:: 240 ^ ; .2 1 . .... ..... .... . r .............. ... ... ... .... .... .
U; I,. u m, ... . .... .... ..
i ... .... .... ....
* M v ...
! ... .... ..
n a . I :;:. .... .... .... .... MH t '4. .
.. . ....... .. .... .... .... . . f•;4 .... ....
40 x 80 Full Run 30 -Scale 0
1 . 4 IW . .. ....
.. .... .... x.60 LSWT 630 Run 96 t- YM/q_f Run 106 .... ....
LSWT 630 t ... LSWT 630 (with Run 118 I—, t.
.... .. . .... ....
LSWT 630 grit) Run 119 • O^ i+ ... .... .... ..
i.
.. .... ....
4t- nli %2 ............ ....... ...
i:.: it: T. i :i .... .... ..
I.
:23t..
V-deqr .. .... .... ....
ii ir: .... .... .... .... . .. .... ...
77.. '-8 7,!; .. .... .... ...
.... .... .... ...
... ........
VIT - .
......... ....
Z5 t - T."7 7r= .... .... ...
...
IN .. .... ....
.... ....
.... ....
.... .... ....
... .... ..
..... .... .... .... ...
. .... .... ..
......... .... ..
n ` -32 t V.:V., .... .... ... ... ...
.... .
is .... .... .... ....
-40 Lv i;i
Figure 52. Full/Fifth-Scale Comparison of Yawing Moment
Characteristics in Yaw for Helicopter
ORIGINAL pac"a lon O F POOR QUALITY, .
.... ..
L". V ^%t:j; t.
... ... .... ....
..... .... ....
. . . . . . . . . . .... .. . .... ...
.... ......
0 :nlm....
.... ..... ....
1 nn .
L/q-f .... .... .........
mi ... .... .... .... ..... .... ....
.
Tri;: MM"." .
mn 1=1 I *M: ... ....
3: M. it 3 ^4 J^'; ILI ....
T. ... .... ...
.... .... ..... .... ..... ..
V: : 1=1 41 .. .. . t nn ... .... .. ....
1::., M I : ti : ";.i .. .. ';^T "n 4 **: 4 4 1 1; 4 1 :L 1 :1. Y.
.... .... : 1 .11 .1 .. . ....
. .* !iT . m: . I .... ..
M: 1: .... ..... .. ...... . .... .
t 14.1 M ... ...
vr ....
f. ........ i fi 1-::: fli, .. .... .... w ni.
.
. .... ....
:V. ZI N iJ t.14. - 11; 3. 1. 1 .=_ n it it V.
P4 rZ 1 deg it. . . 1. 41- tz I - 2: 4 .. V I..
t -it lzi: .. .... ....
44.. 1 2 4 ........
-10 1 1 . — 4. i i 7M . - 4. '"i M!
* 1 1 77• I' r F - -.1 1 -r m Z n r it^ r. L r: +* + :t; n I.-_ - 1E il U a 11:4 , T I M . iffi M I r g M T: !V.T .1= r. '17 17* M MM .
nr MR, 1, w . + z q 4.. . 1 *.1 1:4* {t T •t 4 _f 0.
• 7 t Run 22 Full-Scale 40 80
hv!z
630 Run 102 Z'M 4Mv n ii: LSWT
ii:J :LE .
0.
t 2 41 + i 1 - tv t
I NE-zi
i- E l i -401 4- 1...
+ 211 + + 14- +» :ttt Figure 53.
Full/F ♦ fth-Scale Comparison of Lift Characteristics
in Pitch for Helicopter without- Tail Rotor
OF POOR QUALffy I ... .. —.. 7= ... .... .... .
O^ ....
v I;;I 11 %
.... ... ... I- 141. 444
• it t t:^ U: i 34- ' Jil l x 80 Full-Scale Run 22 • "0-40 41t 'm I go -it. l . M ,s i.:: +1 Z -t4' 14 ix « -.M: I. .. ... .. .1, ... .....
L5WT 630 1021 I'M .11.
00 ' i..v t .... .... Ila.
S . SS T.
... .... . ....
..
U .. ...
2 .. . ....
D/q ......... ..
... ........
. .... .... .... ..
-mqn— 6k i i rrt :.I * M: il l :: MI.
.. .... .... . .... .... ... . NI: M-.
:::t+ M ^ MI 1 .:: . 11 - 1 .11 : 14.1 1 ":. *t ........ + M ...... nj I Ott .........
v 4 . -M I t.: .... ... m i . 4 Ut- ......... .... ...
N."
ri - m un M. MIV: . 1=Z1 = 1 + i 7:. I tt tt- ', 't ii. .4 .... ... . . ..... 13: .2 .;A ... ....
tr.
Ilia+ 7t_ rM -.41. 4 + 11 1 . :T+: I .41 4 N 11 ZZI; -affm 17., 1.1 4 . - . ..
M., n M . -+ I. - -L - 1 11 v I t I M T.
a-de .......
.........
;-- T-I --
Figure 54. Full/Fifth-Scale Compar•,son of
Drag Characteristics in Pitch for Helicopter without Tail Rotor OF POOR . .... .... .
... ......... 001 .. ... .... .... .....
. .... .... .... I PM/q-ft .... .... .... ...
I .... .... ...
+ t..
1*4: fit- Oil ia; *H 80 Full-Scale Run 2 2 0 x ...
WT Run 102 1 ..
LS 630 e ........
... .... .
...A k ... .... 12 0 1— .- .... ....
.
t..g . ..
I is
.. .... .... .. .
t: 41 1' -* 4 11 ,!E - " I., 44.
T. I =t 7 t: .41t.
I . r -4^40 ... .... ...
i t , t: F *. n Z - 11" ', = 11 r . " = =; I'll, ;R R +-I. -o- 4..
I. .... .... .... I 7. 1 *:; 1* 1: 1: 4 1 I. * I •+ , I 1= 1 . 1 1 ,: :,- - I ==, *- TE .i8 : 12- 8 1- . 4 't + I F1.
It- I I +1 a, deg I I .... .. - Z= — .,:7 IT: , - I + 4 1.
I *r I.= 01"" rr 44, H -T : ' =14 -=:r - t -80 It= z t + Tit- +•.:t L-T+ a g -Bi ERB
MR tr
11 14TI 7.
+ I - V t t +- - I R , Y Fig-are 55.
Full/Fifth-Scale Comparison of Pitching Moment Characteristics in Pitch for Helicopter without Tail Rotor ..... .... . . .... .... .
. . . . . .......
-1 i'M - .. .......... .... .... ... .... ..
It!: M , I . .... .... ....
.... .... .... .... ....
..
I M u ;i: ..... ....
4: . .... ......... v W ......... ...
.... .........
T ... ... .... . .. .... .... ... .... ...
.
... .... .....
r.
.. ... .... ....
.. .... ....
V. , !: N.; .... .... .... .... ... ... .... ....
..
. . . . . . . . .
:.I i .:1 : , It r n. I I I I I . . . . . . . . . . 1 : 1 In E. i.
:1 N i. . . . . . . . . . . . .
.......... ...
8 VI it . ... ... ... . .
14:
a-deg
Umv .
... ... ....
--------- f t ---- ---- -------- ----- -o_.i_ M V4.
j.
. .... ....
—. 1) A!
0 x 80 Full Scale Run 14 LSWT 630 Put), 10 5' .... .... ...
LSWT 630 (with grit) Run 124 ,3G ..
.........
....
. .... ... ...
2S ..... .....
.. ..... .....
0.
.... .... .... ..
nu.ft.
...
.... ....
Figure 56. Full/Fifth-Scale Comparison of Lift Characteristics in Pitch for Helicopter with Landing Gear Doors Open OMGFv r J- ,P?f1 1 14 i^, OF pC10% , qup, ..... .....
. . . .............
IN ............ . .... ...
.. .... ....
.. .... ....
.... ....
.... I .. ....
... .... I. .........
..
1 1t .r . .... .... .....
.. .... ..... .... ....
I. I I V=:4: .... .... .. . . 'V ..... .... I. I.
I .. ... . ..... I. ' lot I ' ll t,tt I.,.
. .... ....
I ...... ....
80 Full-Scale, Rtin 3.4 IM 16 l I ..... ....
LSWT 630 li t h 105 :11^ .......
-o. o " .... .... M. MR-in .
I _.. Jj.8WT 6 3 0 Pun 12 4--; grit) (with H-4 as.
. .... .... .... .... ... .... ......... .N 1 4 --1... .... I. .... .... .... . .. .... .. .
i x , m, :I: . ... .... ..
1 ... .... .... .... V:: Z1:1111il!
I M , ...
....
. tr:T -= ....
.... .... ... ... I. I.
.... ..
I.: ... ... I I.
M: I. .... .... .... ....
I. ......... .... .....
I.
. . .. .. 4 . - — —=44-4 I *- ****,**, I ' ll ... .... .... ... .... .... .... .... .... I. - .... .... ....
..... .... .... :NUMN I. .... ....
. .. .... .... ... .... I.
N.
........ I..-:: .... 1—:, .;, I I....
I I
M :1— .. ....
: IU
.... ... 3:. *.V 1— M) I.W
4o.
I ... ....
..... .... ....
. .... .... I .... ..... ...
I N.
is I r:a: IN
:v I.
ii.
,.. w 1 i
IM • ::t! T t I la
Rio
... .... .....
,I:. ju .... .... ... . .. ......... ....
-,V 1 :.: .. .... ....
M
... ........ .... ... I.
.... ...
. .. .... .... .............. ..... .. ... .... I ....... ....
.. ........
....... I .... ....
...
......... ..
M-de q!
Full/Fifth-Scale Comparison of Drag Characteristics
I Figure 57.
in Pitch for Helicopter with Landing Geair Doors Open
UC CO OF .77 1 ......... ...
... .... ...
......... ....
=1 t E C W4 1 _1 44 . ...
.... ..
PM/ q—f t , M nt M.
1+3
40 x 80 Full-Scale Run 14
.. .... .. 1 0; - 17 71- 9.* . 3- 'm. u , "T. I= VM ey LSWT 630 Run 105 -M iTI.
ti.
6 3 Q (with g3^it) Run 124 LSWT .... .... ....
41.. .1.1 V.
1 I,.:: V 1 .1 T41 M: `=1;1 = . .........
=M*.
_Mw 41 11 . I 4 44 it.
it m n v: vm 4:V; --I , -1 ' N :i -,u. q ;t + * 4. 44- 44^ = ^4 4+ T " j ... z v n nn tt : I - + 0 j m Ar. ::M. -;tm + M. + 4- t I 9- 41' 11 1 - Hi4: M.- !,:, =15 ++ 41Z + I _ 1V 444., + El l Vzt IM I Zz= a....
Z_M + EiS =14 4. I— ISt : D "+'« It - 'fl AIR + 7;. E -.4 1 1 : 4 LO U t", +: :-4f I ZI 1-: 1 - 7 + - 4 = v g + .
- z mm i t - a - deg I t 4 T'Ll' Z.
r--- ♦ H -Mi; it' :j7.
+ 7..., 4 0 4 jj_^ M + * 4 4 + + + #4' + H.
+,« *' +^ w;.. . ti .^+. +^'i a Y. i +$ Y^ ^ t•. •N 1^". 1 * +.'« i4 • E!# . w# «. t.
+ Figure 58 Full/Pifth-$Cale CoxnpWrzi,8011 04 Pitching Moment Characteristics. in. *Pitch for Helicopter with Landing Gear Doors open 'WIT o r. POOR Q U AL ITY, .
4 '. M! t!" , yq.
)RUA 10
I-onTare 'nc
.. .... U .... ...
. .... ..
Ut t MC .
'H:
Bar-:Lc Vuselage T&I A=s (85-49)
4t I Vug e+ 'Kingr TE^l Auns (86-52) .. . 1 1* 1 * 1 1 W It.* .. i 11.: R. ....
nim IN I—.: I.
He:Ucopter Tsil ^ !! Tj J., -69 Runs (10a. .0; M ... ... 11.^.:,.l 1 . I.
... .... .... .
... . I ^T, I.
... .... ..... .... I. I. .... .... I ... .... ....
77r ... ... ... .... ... ...
nir VU i-ii qv= 13 . , .1... ..... .... ... I in. IN; 4— 1 P
.. .... .... .. ... .... I. I .... I
" I . I N I . ::: 1 1 :!:: :.N It IN: . , " **.:, , .... .... .... .... .... .... I. .... .... . .... .... M .... I
13 1"
. .... ........... .... .... ..., .... ... ... ... I....
A.r
1 1;: I. .... .... .... 1.... ....
.... .... ... I. ", .... I .... ....
;Vt
-Av-:an
ML t N. -
• IM
t^ On M: a!
it l i I! M Lt.... :vl m..
.... .... ...
L. — rj .
tff .!V %w a.< , RR ... ...........
IV NI- . .... .... ... . . . Z. .
.. . ... .. .... ....
t NN .... ...
it N X .1 3 3* 1., .1N .. . . ....... I. .... .... ..........
. 1 N lZU! .... .... .... .... ....
"'I P. I in- . .... .... .... .... ....
1: 11n. l..- mI :N* l-,;.
.... .... ... X;t 7;" .' 4 ave. . ... I. I. ....
22: 1 4 . 1.
... .... ....
Hat T10.1R. Inv, M q;jm if:
Figure 55. Tare and Xntertereace Corrections to Lift
Characteristics in Pitch for Three•Point Mount
OF FOICYPI MN , 3:1 ri--11; M. inq.!i .S 11 4 1 1 I t.
x C$ 1: I M I 111.
la 1 1 i f :% i i«.
P ' K^nd-on Tare L E *11 4 1+ -.11 Run . .. .... .... ....
U4 i IN I N I : t 'N" (D Basic Fuselage T&I T= • Mi .. .... .... .... ... . • ...
.... ..... ... ... .... .... .... .... .-'.-T
)? , un 8 (85-49) + Wing T&X . .... Basic Fuselage .....
R ....
......... .... .... ..
Runs (86-52)
icopter T& I
H e l H
P l uns (101-69) 43 3 1 4♦ .. j T^ J^: ji . I . .
.. * I .T. " ": ...' - — .. : " I ' li A A 4 . . .
. ... . . ... .. .. .
t [ 14' + 1I 11 11 M Otl ".1 T ':t ma :V iv uv- .. .. ...
... ... ....
;:.*4 = F— . M Rut, .
E -4 Utz ... .... ..
. ........
::t 4 :. '—arn I In!
M * ++ ;. t M 3 N IV x» M r.. I ... ...... H.-E T.
nr M tn!
111 1 5 t!l ^M4 de (ax-de aaa f "I + -+,F- 19 1 r:
Figure 60. Tare and Interference Coxrections to Drag.Character-
istics in Pi.tch, for Thee-Point Mount ORI OINAL ^S QUALITY OF POOR .
, . ........
IN
Tare
.... .... .....
Run 0 . .... .... .
0 Basic Fuselage T&I
't
(85-40)
Ru ns
.... .... .... v
.... .... ........
&x ding
Basic Fuselage +
nz.
Runs (86-52)
=1 0: MI T It . .
It iiil I: 413*1^ I 1.
Helicopter T&I
+ I; I M . .1-11 ..ff r
Runs (101-69)
t + qqqm: MR.
. .. ... ....
4 1 119 j; ... x:. 3 16.
1 4 ,
... .... .... e
U..
*q- - + r =+
.4
M Vi.: -14 U Il a V- 4 t: M M, " :I tI: *+ + ;i .11n.........=.. 11 + i + W. r-- . - I T I. :4.
H.
IT;. It 4 -5: U_ t:a+ + ^ t + + ml.
I ST N i 71 11, 1 . IRM It ........ ..
-4 7HE + rA :t 4 1 ft: j.
, 4414 7 i, t.4 4.
[ r +! . ii M v: a Rr ^.V '.'• ..
+= ^ q 4 l Z g i7m E il-! M=1 4 l I+ I vit= N11- ox , 4.
B^E IF— HE + R r - TE + R F'.
xz+ + + A__ —it 4^ + I ER iff + + Z;1 ME- + !+ + +4 tm zzz .14Tq -6 Hit ln =+i4 ff! N =1 =E_ ,••.
T. z --:: : 23" . 1 -Z + + Z E9 i-^T- WE
Tare and interference Corrections to Pitching Moment
Figure 61.,
Characteristics in Pitch for Three-Point Mount
OF POOR QUAW .... .... .... .......
.. .... ... ...
... ...... ..
M:: Z _ *1 tit , ... N., r4: 1 . HE. . —I I., IV= +. U ! E - a. tit z tu+ i 11 ' 4; J' .... . . TO V.
S.
4m 1i i ut IM t-l'..* Ye t . ..... ...
q Ay .. ...............
F. ^^ -.4 4. nn =-:1+1 .
tt^ 1 -t f .1 V: r. t =1 '14 t^ m. =:t r! . . III n =111+ .
Iw 4 U a .
+= 5_ ' it rz iR —mii T, r:; t . j 29 ^ ff I 2 4'- .. VM 1 . 1 ^ ^7 .
-deg F;^= + 4- 1— 4.".
_,.jttT+ " I I - nd -on Tare Run Wi
}„' Helicopter T&I. Runs (96-63
re P;.'.
i^Y tv; T • iii! U!
t!
Figure 62. Tare and Interference Corrections to Side Force
Characteristics in Yaw for Three-Point Mount
o p 'laMPL p4zm- m OF POO R QUALITY 1.:I : :41; : :1 • 1 .11 : -. 11713: * . .... ... .... ....
.... ....
j .: un vt I ' ll " "" tit" S» 4 1 .... .... .
...
........ .. .... .... .
..
.... .... I p.
f t , ln* 'IBEtt ...........
.... .... .... I.
. ... .......... .... .. . .
M 2
_n^ :f -I , 4 .11 1.1m,11.1.1 t. N .E. i.;.
t1i, 11. U t. . 4- . 1 v i M.: * ;* l = T V.
A D/(^- f t 7;:t I M W .
. T . 1 4^ : It t 1 I .v i;lT 4W. N .
...t t'. lay, . ....
--t44 ...
f t iZ . .... .... .... .. .. ....
.. ......... .. 1.
;V.
M: .... ..
............ . ..... ... .... I.
t :: 4 , :t VVI . .. .... ....
... .... :;1.1 qtt: :,Zll ...
Al ... ...
4!
.,.I 1— 114 I ::* 1. ....
- I t4. 4i 14- 1 4 .
4 - "1. :31 1— 4.4.
...'t H nt. 4...
It— -Fil :VV .
Ha ii-it V V iI ... ..........
l" — g r I n. i :- zu n Wi nd- o Tare 1^un 6 411.4 ;:v iii Helicopter Tt4l Runs *x 14 - nrt: 4 - K, M lil lt MM .17: ",a"..
i2 4 g: g: t 1 4 .1- ; 'H* -deg T:t
Figure 63. Tare and Interference corrections to Drag
Characteristics in Yaw for Three-Point Mount
vq'57, .... .... ... F. .. .... . .... ....
V, ^ O f i^l ... .... .... .... .... ...
... .... .... .. .... ....
.;5; U: 1 . ,M l t ! 11.14: * Z: ti .... .... .....
. . ... .
.... .... ... .... ....
F .
: 1 n .... ... .
I .. .... .. + ... ... ... ........
T I J11.
_111rT. .
. ^4 m i- r !.+ ' 1 • H^ 1= :V . .... .... ... ... l+:t t 7 1 ... . M.51 E f V.
.......... .... .... .. ....
V t. . .... .... .... .
+ .. .... .... ---A YM/q it , tlta .... ....
U ... .... ....
. . .... .... ...
1 4 j ;.v + 1 * 4 2 .... ..
. . . . . . . . . . . . . ... .. ..... .. . I.
Tr. + tI .v+::.,.:. M Run 6 Tare n Wi-on n 96-63) e1Jcopter T4X Runs KiE . .... .. R; M M4 =3 1 Hi t + + 1EN + + ... .... .
+ ii-EHHU , ME i t .... ...
U=: Ml: =t tar irv. F. r 1; 'Um .4 Ir. -^vl =+ +*.I 4 . ......
+ + • = ..t .3 N: .FIN R t wk + l_+ 4 M, "t =n l u - UV I ♦ :llutll = 1 ....... .
;;7 + ' 3 2E - 24 -3 -1 8 .Zr 'Zi a- ilir tftt . 4 1.44= 41 ^ +L ^ + . 4tl H4.-L; ...... ...... ......
:2 t= 7.7= Hf :,17r U t + .4=. rp 7— t== 4. T 1. 111;; + 4M ., t .- f . V I +4= + + =Z4- 1 1 439- 1: IF + Ea:-+-+:.
419,11 r l li^l^ ia. f; V_ 55 H 1 Et Yy+ += Ing 7: 1. s» - 7M . 2 2 1 1
Figure 64, Tare and Interference Corrections to Yawing Moment
Characteristics in Yaw for Three-Point Mount
10-5
OF P0^ 0'! NU a u^
'igUrIE2 . 65.
Pull /Fifth -Scale compari. son, of chazacteri,sti.cs...
Li4t
IN
Pi.tcll for W:Lngr
in
^^ {.. 1 L '2 ^2 ^ ^.. T ^ , ..'I.
1 j.
t: xarC •" Xt2 r I r I : + +r :^ , t} r l f 1 Y 3 J I i^ 1 Y $6 i f .f.
:n» :r, ii F»$ :3I ♦ '• Yr...x.. +` 2 t i' lifi ::* .+11: +, . ' +1, a 2 + `'•• " t:, ;: r r { ! 3I 8, . 1 S I::i Si * i ce , ^m i*` ti 'mot 1 2 t T itS1 I2 ." _ w: I I Eli _ Hr.
-- SI vt + { 2 }+r• ..
` Y^s ^, t tr II 2" t S • . * t' :. I + ITH W in— v^ a μ.
Sr 3 t : i HH»++{ r.+ t `+s ''" :w ....
IT" =.0 .. r:« 2 + . + Z. r ri H il• ++_ +4t :^ .Ha` 1s. {$ 2=:. _ +r+r ' 4w f` { ♦ a`°deq w ..^ +^ tie f.- + * . ' •• ... ' .
♦ - ... t"i.
+i+ Tk rt _-. a i^ ^+...« .f.
f.-' ri - M *' .y-!4+ Iw .... n ^ - I.i i aH r +,'M ' N..
.,+ *., tz.
,. t± M -^ 0 80 Full- Scale Runs ^(69-+68) w I. ? LSWT 630 Runs (86- 85)
LSWT 630 (with grit) Runs (11.2-109) t
t -12 r ...1,.
. . .. ...... ...
N hl b r.1 -1 b.
μ ++ • r o.
H pOOR q i;.
1;!, nl: 4..: l 4 - r 1l i t: 4 - tj: tr ' ; IV. ..
Vt,t f... J!'?] P!t ..
......... .
..
Mt.
^L SWT 630 stuns (86-85) i ^ . i. v w::- 4-- r: LS (112-109) WT 630 (with grit) Runs I .: 1 - F ! I t t4, IM I .... .... j- I.. R T I D/q-f 7: 1; 1 .1.. }+i } ._ i ^j .. .... .... ...
... .... ....
;.T,_.. j4— 7 t Mll .11:t .J4 r. vlz , :4t ... .... ... 4^ ..... .....
S , t tt^. , 4 1 t;.. Ml ... ...
iM 1.
;Nt V : 4 * 41 .1 In a-deg E.
T" Mt.- ld;
Figure
66. Full/Fifth-Scale Comloarison of Drag Characteristics
in Pitch for Wing
oviGNAL OF POOR QUALITY
Figure 67. ]dull/Fifth--Scale Comparison of Pitching Momen
Characteristics in Pitch for Wing
............. ------ ----- - --------- --- - ------
MIT B7 L.-Hr H
, .+
1"M
i.
I?yl/q-ft3
TU
ii
a-de
40 x 80 Full-Scale Runs (69-68)
(86-85)
LSWT 630 Rdns LSWT 630 (with grit-)Runs (112-109 QUALM^?
OF PGZR .... .... ..... I.
......... ....
v.
.... .... ... I ....
at: P 3111:1* :T.
+ .4 U. HU I • 1 _1 1 M I . . t — Sf t : =.: tv M =1 1 31IM;1. I' i t, 0 x g o Full-Scale 1^uns 60- 61 +14 , _:1 +
5 _11 I ' M 't
SWT 630 Runs 113-112 ;f+t; , ;14= I M t . ... 7:1 . Ij M 1 MI: L/q-ft +1 M tu: t q zt^^, 4- -.
xr.
tn 1 x iff l ff a t n , tm I ", t M I t: L. U .
i I.: I. 1. I.: ....
-"Mm ^t l - I MH -I 1t 1 It '. I.- R - _V .... 1- f. .... M. .1 Mr. - == 1 3 4 M 1.7 It' R I= t1L I: i., ^ r;:' f 1 V 10, k.l... H al Rlt r^ a-deg -I: 44. ^^ ^44 7=1-- i4 . T — v CH t iN E ' t . , t tT z: - li S ,tS 1 14 r-7.
Fs t 3 = - sL' I 1 +5- 1+ - -. ;:. g += =MMM: I r- , + = • . ......
"a g a ..... .....
TU . . . . ..........
;23 _.tt _,:rtt + + W.
Figure 68.
Full/Fifth-Scale Comparison of Lift
Characteristics in Pitch for Horizontal
Stabilizer
OPJGINAL
^
OF POOx Q6ZTY
:4. ' t" Ttf T. - I . 11. - H
r. 8
. .... ... . ..• .
-:44 4 4 .... .. I t +.
4 1 r ♦ I * I - M r .. ...
J + 11 - 1. - 1.1 .....
*.!.I t
0 x 80 Full-Scale Runs (60-61)
.... .... .
630 Runs (113 WT a in . M Eli, L I nt rm.
Ir T IT . .... .... .... .
... ...
;+1 1U. IZI +:=r4 -4 ....... ...
= 1 V tt z K - .. 1 41-- IV V t 41Z I t— Full/Fifth-Scale Comparison of Drag Characteristics Figure 69, in Pitch for Horizontal Stabilizer PAC 1 2 11 UPI OF POOR QUARL17Y Compar;Lson 04 Pitch; * Iinq Moment.
Figure 70.
Characiteritstico in. ^?Jiitch fox Ror:Lzorxtal, StaWlizer It IMI ..i =I W" N*.T "I i m I . .... ..... ....
0I 8 t .... ....
4 +f:^.
44 . i ftm; t ....
H I 2
0 x 80 Full Runs 60-61 2
MI.: qz.
:Runs SWT 630 L J4 I..,: 41 T::U*+.'
it: -it- -- 4 ] . :+ j . at: "1114 F. -Ev.. E W' + t.;r I of + V =u 11 411. T" 4,;.
f + I I :_ I Z r IT : I rti ^Z'g M H. U. I' + -nt I -1 + W. = :* M ii; UI V v. ^4 H Z I L E iH l M4 .5.4 ifl. *4 IFE: i... . 41 -+ M PT i^x ;' ITI 4 ..i.
• M_ awa 4 t + t^ 4^ t ^ t4tti N St •SYF . 1St ggr I= a2.
r St.' T:..
- 7 t — 4 ,;N 4HK r tmm; Ta* + p
t ra OT 7
o ME Ito: RIT t4t =1 I' M :+ 4 -4 4=1 BE a-deg 1 tl T tr= 4= - i t+lt I.- !; vpif i l + S !Ei ill - 1 1 = 1 1= 1 =-I im if M. 1- + im H'a ill P _,O QUALITY °:
V ,guxe 714 calllpaxx. soxl o4 p a5f
14:etr x axe d
' PitahiR^ag M
omen t ChAractezits i Cs 3Z
N ' Nr U.
in n do a^-deg t ♦ i F ^° :ii 6 t ttJ R + t ti ♦ l.; ....
w. t Crr •1 h t •' ♦ M. + ' t ! " 4 .^ ...3 i «.4i : J e /«^,..
4 141 -r t . II. r _ tt t t , ...
IN F F et : t --52 ) r^ 0 x 80 Full—$ G ale Ptuns (51 s} } .; ^ M.
ttiris ;LSWT 630 (117 t • k.
tl t: ♦♦ ♦ 1 / -}tt « w.
ttt.'
e - - R x .iii, Yf t { S« t t Z x y ..t tt ' x t { to .1 1 Y i t t •1/ ^/*. +a k{ •.^ Ft•1 J. .. .Jt t ..t4 t•r kt•• r r ♦+ r t t J Jr tr t 1 ..
v: n .; 8 ^:: a^ ^-•1.6 -»^.2 i 8'` z p z^: ' F, --^ z 1, 2 • , y... ^ „4 F..a ^: 6„ ♦ ,, {+ R 1. 1 t.k R +Rtt t t R I M F J { f « l/ {♦. [ .w 1 1.! a—d • 1 .t t { I. ♦ R F R M t. « eg 4Y ".. a w'1 ^ y }} J f^ R sh t ;t J.
s + i P I•f, w L. F ...t.. I.Jt k .:: 1 111 1 1n.. .•^•^1 « I.a • i ..1f t . o Yt 1 r^ r ^ !♦ 1 t t s M 2 y+-3R « « t t 1! 'IYrI ' titfrr^ ^:t ' w T . t «" F J« tj 1^ ^t U 3^`«r i « ^ +p h t+r .
x t ^ PM/c^`-ft :ss « I .
«.: ...i. «t,. t.i :. •F.a `t ` t» ^ ..« . L«C:+ Rut :.t t x « _ :^: .4t as r. s ..•r .
. ,•• e 1':F a +a. .:x: .J.
`*` 2.`t 1 « J- ..1':J " ' :« • ♦ i ± . t- X:4 '^ - S j. « ' .._ } t4-«+ «#.
.L:1 -»:: 1 2 J:^:.
.t. r.•:.JY r {.1 0 k TM :a4 .1.. 8: .''t .,:.
+: . # ri k: a- deg rza" Mr Vllt +^ ..+ :t t ♦ C St Rrt t ;tf t4' R C« +^* M.
x . . $^dw « +r !+» :1 t# Y . XXF }t Eli M fit: ♦.♦ .Ri # 4ta +-Ht r +t +f... #Y+a H T r • ++.. M Jti F b n } «1 r^ •#^^('$^t^+ } J i: + Y^+M «HIMi pR,• ~« +; ..2 t :ta +.« «ti " wCw11 + .p R F:a 4L F i } y M# X .«: F Ls. ;. . r +•: t: :: « » Y • fl.+• i . « R .ti .. tR.^ 4t# _R « *l+ R t: .^` , t.. J x .. . t x: x w . .r . . J.c . .J . s #F: ♦ - • ^° ^ t + '* r"^^ •"t . M ^.."' a J II '^ t ^S ct i u R.w .:.y - ..{'^• Y Yt `" .♦ «t « Y ^.^ V30R QQ,jALRY .:....I y t •r ++,, rer Mr. ............. rs.i .t. .r.^.-.Itt.t+.r r, m,+ ..t,^ s ♦. r.,,. ,.,•. a ,., »vY.,w .. .t•..+
Figure 72, Full/Z-'U th-Scale Compa f L ft, Drag, and
rison o Patching Moment Character ,st cs iii Pitch fox Endplates K S I'j.1.. 251 tt :T.i::.. '2.2221 «jST• ^i:.TT« :Ai r.+ 1—MM.;. .1+ 2 rt.z IM -ft t r ^" s L x ,.+ .. , ^s: 4. ...
^y j{ •L tt _ L SY N •6i ^r.
T^ 4++ Y• •• + ++ + T +# ^^ ^ rtM ^ i iai: iFAi ..1 iN -ar ri a 1.i^:.,, +# A ' .zit ff + "` u i T. + +.
+:z ?ri. {Ir :r? +;ii +•:: «.
t 1 14 (a, SF + • ,^ x ' n 'T •+ - H: r . • i .` .r « S «CS + +• F' r Y t{+^. 'TTTi ^t'. TT2! TLY('l TtY' T. Tart tt7!"iti • t .TTt tY.h 2''•t' fTt {TT'( ei 1'
Runs (59-60)
40 x 80 Full-Scale
630 Runs (114 - 113)
L$WT " r
•" .++a aL .r. r-. 2: L. .;i..i. LL .:+ 2Ti _:5 . 12 T lilt .t. LI. lTU.
' w ^.*; ++, ..t+ t ' + ^ t ..
+ " z. rii: it s rt — 'a. I.ii a : + »..
; '$ .. , , a «. .+ + + y 1 :7 ':I ` ^.$... +l :+^ ++e» i' .. F +a F. r ..•+ v '."1 ... -?:i i.• r , t, "+ • T 7525 u2 • ^t 5... :+ '+rL ,i +..
.l r, y ^y..
N N 'S" r•'. •Tr+l •' ^i . L jj I.
F'a+ +H.
+.. ++ _..•+ k ^+ i • F .. .-. • r. .+ 1aaH +9 ^L%+^] +.a• +.^ ^ !'y. 1+ ria . .
+^ + ` .
ri• ...Z.. .r + i ^'. {..+ {1 ^j^ +w li++ i ^ ff M ^, y •+Hff h+.•. I • ^ i.
H } ^^ I ^ ^f a^a^ Jr i + 1.+. .s.
r•7 ^ ^ r^ ^ •+in +H : i : . . a :' — ..,r. «^: L .^'• .+..:12. . r: i2' +:i:r 272 .+,.
I NU .K ^: f^; • k ; 3+ rw. w; fir, `"'a-deg fz : L : s;:: :.^^', . :.^ iii : r^ + *f M:z .: ,.^ , «+ " •.'^..'^ ';^ , • •^ •:t iYr .Mf+ ^^ 1 fhM+3 —• er.•.• irt.+ ^ 1•' *^. L +Zr F 1 r ^t W =uw ^ .+^. ^ I ^ t. n. • ++++ ° , 1 Ly .+.. ^'^ +w ,i.L . +1rt K riL .a. +,+j "..• a' ry 'S, .ayM S r" TYaH +2 w j' _ +»:S + t Y i+r , .
N .:Si Li:a + t.
, L ... M.—, ..I• ate .•.,` +' .5+: r.`i.
•+a .L +•+ ya.
PM/ q - f t saμ 4.
I.Y a^..
_ ~^: 0 _4 ^3 '^Y y u 4 " 8 12 16 .
.. +; a ^ + : ^ _ .^ - ^:.
a-deg H' .+r •• 1 a • 1 ft +W1. ^^ aia 2+.
i.
t• ++a•+ t7.+. tt +t.f Y.
OrMA I NAL PAC!:: IG OF POOR QUALITY T V 1.
Scale o r ull 60 r . 7. t
H!
i.7 M: I , "; u.".
V I I! ;^L:! 1:^, 550 Mr r7"T Run Fy f r .... .... .. .... ...
j8 IN, 109 itit T_ A14 SWT 630 Run I 1 1 :;. 3V :I:i I;, v. U;4 . Mr x-In 11 T.
ji.
WI : t I N 4'. to J; * IT I I I I t N I.
it it.
up .1 1 t.
, : t . t:
I S
I T I P : 6 , 41 ., V.* I n M.
, 15 i I I .. .... .. ....
Ys' 4.1 - 4 41 I t: UT, .
IUL !VIt I _ 02 V, ; ; i n I ;TI. 1 -.4 ...
vp v; w it. I q v v 1 1 . 1 . 1 1 1 T y l I I I: I VI :V! .. 11 ^ - i t ' 7t7:- Hj v, IV i.
I I w r ' .. v:- il n a.. %: V 1.
TV 7:!t.*.l U' . ;
E li li_ - .t~ I 44 On: ;.t - gq vv i Ki KnInt, I . !t v.: I ti I Hun . 4
ra " 6F -'flf"fl: J 1 7'1 : 7 ' n • '..n. !wu. , . i1i, 4'.!
%-deg N 11 4 H " RH11I .IM4 I a U .
1 , i l l ; I M: ' : 4 'l.. f 4., . .
-.; tzI ! 1 , t 1 .1 1 1 i 1H - t P1 I t -?tt 1 14 4 M.
.
J .1 , I ' t p , I-.
TM I . . . qM f 4-a i 0t . : P z . :v In: Ij Hi: .
--v.
r :.,d- AU IT I +I; i Z .... .... ....
....
IT' ^^4 3_ M: tttl 4.
M tv.
- L. 'I I= M M _4 * !zr i.o.
I V. jj: ♦ t z :.!
4.
f f H I .. 4 I T. - ' I T I!
tt i l V it 7 . - T + - tt t I'll 1 - 1:31 ..
.71 4 2, q tr ; 1-4, 1 . • 1 . . =- I! Z j : _ 1 - -' 1 1 _ ^ I I I -: — M ir .
I I. - t - I I: L : I I 11 ; - - W, t.i pAi N H 4FIffil 1 : 1`n`4 ii . - - .1 It* IN
I
Figure 73.
Summary Comparison of Lif t Characteristics in Pitch
for Basic Fuselage
_Vlnrc mas - 10 U
0) 1 1 n ' ^07 1 O v POOR Q. UALk ,,ry - • Full Scale Run 68 i" T ^i.M . ;j. 1, TM -'.Z TF^ ul-- *".::, .... .... .... ..... ..
, * W i, . m T, :'tit t2 IT4 LSWT 550 Run J. q 19 LT iii- .* j-, U T 6 3 0 Rua 109 Tr^.
►► M Nt:v I t. Im Fit I I 1 4 IN VE 1. V 11 , 'I U"r i; v: 4.; ' 11' i. t4 HE i' T! I I n t 1.. n. : ;4 ; i it lit E 4 i ti ;lit i ; : +it Ll ill , tit: I:! it. i N O !1. N. : t :t lit ;z: ;T M! i4 ^m • i t , ii. 1 14 4 1 l .ti V Ott " 1 1 - f f lilt , 11.
H ., t v.: it ti 111 is ;4:4 1 j 4:1.. n :i Ji, it 1 7.1 lit, t i 1. - t ;v it - .T T7 77 t 77T T rr. _ 11, wi I t :721: JI 12' W: M, .4' L 4-deq nt, itIMM
Figure 74. Sununary Comparisoa of Drag characteristics in
Pitch for Basic Fuselage' OP POOP, QUALITY l .r , 1 t i . f fL 1 * . ', `` t ,.3. ..f t t". SF ' : I. i. } t « a ^- Ca Full, $cal a stun 68 : t i s J I t t t J Jt ! riE ` J' J 3x , r t. : ": ,^I r. t 4. i l i$n TE , t , t i, i,. `{- {. :it e !
.. ....'J t«.;I: ,'t£ I.. ^i :;}.
[ t
V t t i ,' i r i t . ' T I , « « J ji
«' t :^ t « J i i LSWT 550 Run 19 , r ..tl ..1 '—^ ,, .;.; *lre 'I:: i :+1 r: .1. 1 ' . I t tt f 1 iiL: tI' , .1 " 1 J t` ' S tj, PM/C T 1 3 4 LSFiT 630 Run Z09 ' ,..
1 ;.
T } is t. cr .
p-T }.
777 -7M , !+ p • -N .. .,, , F 1, tl :I t I a' + ' r }tt::tti :^. ` TL!
+^ —L6} -$ 3 —4 : to.
;c decd 1} ; a — .^ : i3 . ' it ' iiii '' si `' x ' i. ^,! iIK' .) .,3:: t , t .t M r ^' :i t11 ° cL T * I . i , t i . ":. r T tr- -;t! ill ' !
c !
1.
...
, J I^ !r1 1,:• I{ SI ! i' .j1 T t ' ,,' r: .t 1^1 '^3 Y. %ail C f ,. ,,.
:JC !:: '('I« e,t: ^^E :' .{ }•' :12 11 'Ii r .,at .}: i:l S .;; .,' it .; .Efj r Vii; .} t. * t.' ^, tr 2: ».^:_ '^ 1 'i2• `.3 t I a12 a 1 is 71= 177 O t: ..
J s^, t` 41r t :TI 3114 I ii r „ ^' + t 1. rr FS ,' 1 Jr , [ 7 1 }+ I S '..'' TL I J :t [ 11 t! '..
lilt :J:.
't T t • .
t + T .I t.
+ ? I ! t^ 0.
:^ _ _ r i I r J 1t t _.- t 1.
75. Surunary Comparison of Pitching Moment Characteristics
Fi..,^ure
in Pitch for Basic .Yuselage
1 MG0 1 M R 0 L rR7 7 17 7 M) OF POOR QUZ^MW 1 4 V. ;T ; T T. Ail.. 111 : ;11 . 1 1 . 1: 'ITT.
.:, I j''1 1 4 t T!
:qiu-jii I n 11'r L TT.
F 'il W 4: 1.
J 1-4 l it 1TJ* A tl _4 ^%, er W tl l : __-n tt L/q-f t . 1 .7 . 7 Irl "i." j! I U 1 V 'Zi sT 1W .O.
AW 1; 1 . j .4 . ,I 0 1 1 r 1 "4 2 " 8 .77 .,d # T1. 1 IT 1. 1^ 1.
ITT*, I ti ♦ T` J.
t!' r. a-deg :f.
:V i;4 •-- :% iT i ! 1 1 1.
-1 - -V ---. i 1 1 1 . r .. 1 • 1 Z. , T • la 4 q1T1'," I ; i j. , J!
R, I tr. 1; w 4 . 4 .- .1- 1 :i . 4^. !::! :p, 1. . , V + -^W4 i + .
i., ^ t . a4 i4 .... ..
r:: 4 I := TV ' t "T + t .4 t ii - 1 rg L :-JEr. E lf— 5. .. ....
0 F 11 Scale Run 2 0 lv Uvr. gq T !
• :! 1 ! R AN.." 1 41 + 1 IT 4' LSWT 550 Run 22 !
C3 - ♦ I M 11. r 1 1 P 4 M I . * , =1 LSWT 630 R 3 4.= 31 1 7 * 1 3 .: 1 :, , ,a , :' t " 1 iij 1. v nuT i; HE u..
-IT -- Mr.
Jrr ^ : 10 !ZV " n 1 .^ ,j 4; 41- 1 t-t f =4T 7.tr +: A A / 7 t+ 1 : 1 1 gin: Ell 'm H, V ..3 7v t ff— g ' fi - R i .
. 7-N HF.", tf'" :^!r
Figure
76. Summary Comparison of Lift Characteristics in Pitch
for Helicopter OMIGEMAL P I I C I I ;N^ V-3 OF POOP, QUAgUTY.
i4o, mi m. , mi N, . , I T im. NI 0 Full $cale Aun : t:: VF ^1 — 1 I t 1 , . i. ::1 4 rf r Ilt :M.
Z.
[I LSWT 550, Run 2 IN I . W -...4 -7 ..... ..... .....
A LiSWT 630 Run i .1 'Wil .. -12 .7 T. 2.
j:: i ! i -n - : 41 :.T—^ 1.
t ;.1", i 0 .
+ 1.
tT iflit i Ij! j i ff^ v:v q I : :t.;, .!I + I I ;I Vt -1 *:: t t. N. pm U.- :[ i t i — NU :4 1 4.
7U j i — ITj 1 II , LT ^ ,Iffltl 4-i -I i -t i L J 1 4 2 --:7 ... ... 1 14. .... .... ...
D q-ft t i N it L :iu 01 '4 E; 'M I M I t - 1 !V V l 7 -7 o r i.; 1 V f it k... N ., 4r1 t it - : i .. . . ....
- 4:7. 41.
I U" * .!
;: .
.... . '.
.. :f I: .... ...
-Itt WI I T1— : r A ♦ .. .... .... .. 11 1 ....... .... ...
I'll * !1 * : 4 : ** -I't . 1 .
Ri6 1.
I -decr 7 -1 1H; 4 H'I A Figure 77.
Summary Comparison of Drag
is Pitch for Helicopter
:j. r^ :ij i; t , 1: Y. 34 11 'Wit 1. -41 4jq 44M ^4 I- , -Itl -, T i , i tt— " ^4 = 1 ttt it;x I.!
; T.
3 J.
M/q-f t
Full Scale Run ; L 1 Tv pi 4. NOW J-I;rN q LS^U 550 Run 22 - i r". I L il t Z
630 123
LSWT Run + 1
It 4Vi ... t J. .1.1 t 120 t il Ttqj -- i l i - ^t-+- 43 - + ] IM + a T' 41 1 -t. Rmi -+t v- 4 4. 4L tv -1 t; fi. in- iia ail :V • * pv. fit: E., Tf n u fit. 3: I 4.; ;.rT v, l l III.
li--- im -;!I M .
.41 t k 7P r .
fi . f q C TT +4 1 .
• *r Lit, I 41^H _ -: : 4 k i7 it r r- 4 I V1 ;1: I iffi iff 4- v.t: 4 1 it -1 1 .! -tq liq- to M k t k •"Lt 1r. , ."
4t . 4 1 - ! i: - :71 W ;g tt.. I I V U I T. 2*1 7!!
ika t1j. 4T.
fn Y " = • U1, ..nrm, t4'.
ME -7F- T7 MF-, U r i i: U 7. V: i.
=7 t
Figure 78. Summary Comparison of Pitching Moment Characteristics
in Pitch for Helicopter
omamiv- QUALITY OF POOR I i t ... ..
4, ;M uv :nI XMM n 5 .. ..
. .."t I + '80 ItU .... .. ... Y.
T 44A 17:1 1 . V"T No ....... ....
. .. ....
....... . .......... ...
g v: t T;tl 1 W :'Ii V.: j.; ni i n . 4 V, n 't v 4. 1 .40 ^^ V; • .: 1 .i ' J I .... I. . ....
.... ......... .... .. .... if ... .... nt - , ....
M, 20 f t v 4i n :It M.i. I—: ... 3V I kI..
^t 7 t.
W. 't
4--'- 4 1 .8
Ri.
-de g 4.
4MV T. I.
. ... .... ...
Ui- 14 -2 0 Full Scale Run 30 V a rt : .:. v 777.
Run 24 q LSWT 550 A LSWT 6301 R= 1.
r T 7'. 1.
. T VI, 47;.
.. .... ...
. ...
... .... . I ....
;14 1 4 1 sr., 8 lyi MIT.
Figure
79.
Summary Comparison of Side Force Characteristics in
Yaw for Helicopter , nr G ^-1 s " 11 • LL ' ' }•' , Run 30 4[4 0 Full Scale } , N : q LSWT 550 Run, 24 { t _ l,.
11.9 0 630 Run •i DSWT i I , ; , - r. 1 :.
t.
?r- t s r ^ . ^• .j J E I c j 1 .'_ t _+ 1 4 t ai , r ;, t w 1r, ' t ,' I r j• ' t I _ , 1 « L + } 1.
, ff+,i l iv r : t .
: +.
"^3 ^c 6 ^T t ^ , tt .J , F ♦ :: ° ilir .1tt tr :^. t .x} _ ` . . t ' t I: t :' T 1)/q—fit .t i t t f ;} i rc^ Ja, :. ti t 31 mr :t 1 f ..
^' 1 Tt r T^ J"' c } t t : { , 1 rl ♦ + C *•t^ t:et 1t t.t :a° :r : 'tt::' i ' . i' f.. I^.^ ' t' t. ! L tt t ri J . r rl t E i , } .
i W , ^^.. t.. at;L l {..I .., }::' •t:• rtT. 't:: . ,t t fiT• i .. t» x { , , , .
l t}. 1 + "° IF,! ,G ','t J ¢ rr.t t r^' 1 eta ^• t ' 1 I ' r1 .
i 7 .
♦ '' J ii ^w28' t :i ci !
tfLfi a J( :, t } t t ' t. i.r ...
! t t I i ft t 1= q« ati :1' 'I• tLL J F f EL 1, rig: `'[.I..}r' T q, il J tr. : "' eI . .t t i -$ •• .»!' Y' r1 x ♦. i t. `2. l I 1 ti Ell t . t :..ate. :I'.: .}.l, L t .; r '.: 7.1.. •i• x.
1 will S t " J ' ' L ,^ 11 1 • i..+ a ' S 1 r ' } 1} .' t t 7"1 . 1:.
.• t" i2 41.
mil J t ^s 'r .}' ^lr t ^.. ri x c. ^^.
^+ t }rU i F'.,, 'r x^ a1+ t J n'i ,.t iii • ts: 'f^Li ic..: • :r^. '.}- c: . 1. +Y_; ,,!, xt„
t
Y• tt r r
t : :IF. t: -^ ♦ ^ •4 . tt: L d i` t .t • :it: • f ' Tr -i 1} t } ` t} * T 2 ' ; t *1 r it '-r r 1.1 .
wN it I +tl' 1 t:• t ;.
IN t• ' • •t. t ` Yt,1 t• t e^ }}+.
•t:' t : r• «xtt I '
ri' l
t.. xt,t tt ' •.. tt~ •+' 1: t1V t' "•-t •,• •tit •• ` i J+ .I r.f t^ i tx 1•r.
i.
,t.: •1^ 'rJ , ' , t t , 1 Y' x '"Y ,t* - '" . 72 1 t;t. 1 + r t... t :t r., . c r , . 1 + t a Y , , , 116N ti r• x ♦ 1 ":Tl. T.i.: • 1 a 1. wi. !,. rt. • ta• .i ..Lt• if ..+r . :1,:La. ;il +..+. .t., 1 r.^ ,•.f Yr iT } a - i.4 _ 4 - • - a wni + ♦ t t -JHI • ' t tt' .4 r : +• t i • t T ^ :' ;^: t.r . t , r z. Y Y t r +t, r :: r ..1 .ttt , 2t r t t . : ,x tt,'s . t.t: ^'s , - zr • +r : _x :sr. i t •r:i it; t1 : ii^ . R ; irk • is .. . ; x.zt .., it t I } + t ':^ 'i `3 .^: i, .St ' t.1 '.i :.`It .2:t .t. +; r • .^ r t ]t i }i,. °i. x«.t Lr+1 is tr rx 3 ' = 2 2^r W32 .+11 r1 ,. i; t ^; i:, ta.
+ 'fir.. t t :a ..., ' :j i; it i' .Ff . f i:'c , H' i 2 i } t ii r} . z it t 'i i rrli t^, r . ^ . • tt: 3. :rt ..., t. ..t . .2i t G V —deg • f ..J...t .z}t t::.. Y,}+ :: r. } g } }^!
, ,` ; 1 :its • r . ` r t: s 'ira tt t , 2 T t it t S t' t 172 r..
^4 tlt..tt12 x 2 , TS l 7 +'1 .it tT+ L,. .11 + i# ri. 2 IF 'r .f, .f +' 3.Y .t. t1: 1 t1t IZ
Pigure 80. Summary Compaxzson of Drag Characteristics in
YAW for Helicopter
OF POOR QUALITY 1.; 17 finii.
IM p lit ':1 .2 40 i f Full sc ale Run 30 J
Fm
P4; * i : ,:;P; R mi * +';;';; H;i I I :t .411.
1 60f Run 24 [3 L$WT 550 - . .... ..
U V A 1 4 V T1 U.
A L$ W T 630 Run 11 9 l;_ WWI 8 0 ff :2 -1 r:I.q eg .... V 44."' 4 1 1 4" nt v.
In.
t 80^ 1.
1.
t V r:: :-, :4 iw ntil .
. ... .... "It LL.
. . . . . . . . . . . . . . ........
v V 3% ...
17. . !iT LV tin it. .... ... :tl 7;!
Tt I t IT .......
r.: H V"! !1i, !7*1 .*"1
of Yawing Moment Characteristics
Figure 81. Summary Comparison
in Yaw for Helicopter
TABLE I. COMPARISON OF REYNOLDS NUMBERS FOR FULL-SCALE AND FIFTH SCALE TESTS Reynolds Number - Millions Horizontal Mounting Run No. Reynolds No/ft Wing Stabilizer Fin Strut Full LSWT Full Full LSWT Full LSWT Full LSWT Ful_. LSWT LSWT 630 Scale 630 630 Scale 630 Scale 630 Scale 630 Scale Scale 6.13 1.52 2.81 .70 2.95 .73 2.25 .56 14 124 1.25 .31 2,.25 .56 .31 6.13 1.52 2.81 .70 2.95 .73 20 123 1.25 2.88 .70 3.02 .73 2.30 .56 120 1.28 .31 6.27 1.52 2.32 .54 .30 6.32 1.47 2.90 .68 3_04 .71 68 109 1.29
N
w 2.90 .68 3.04 .71 2.32 .54 112 1.29 .30 6.32 1.47 .38 _19 .65 .32 1.57 1.46 .72 1.53 .76 30 119 3.19 Qy C Notes: G^ Pitch runs were made at q=62,5 psf full-scale and q = 75 psf fifth-scale corres- 1.
ponding to velocities of approximately 236 fps and 252 fps respectively.
G- Yaw runs (30 and 119) were made at q=16.2 psf and q=83 psf corresponding to 2.
V=118 fps and V=272 fps.
Q Reference lengths used to calculate these Reynolds Numbers: 3.
Full Scale Fifth Scale < L3 1_0 ft .2 ft RN/ft .9 8 ft 4.9 ft Wing chord 2..25 ft .45 ft Horizontal Stabilizer chord 2.36 ft .472 ft Fin chord .36 ft
Mounting strut fairing chord (pitch) 1.8 ft
.5 8 ft .117 ft Mounting Strut diameter (yaw) TABLE II. RUN SCHEDULE FOR LOW SPE33D WIND 'TUNNEL TEST 630 a '^ TEST STATIC T&I RUN CONFIGURATION RANGE RANGE Cl TARE RUN REMARKS NO3 (DEG) (DEG) (PSF) -25/+25 X3 0 83 1 Model Strut Fouling After Data Pt_ 4 1* 8 = 83 psf p . Upper Fwd Support & 2 X3 (TS)1 No.36 Grit o R e ar 3 X3 -10/10 Remove grit and modify front of hor-^ izontal fairing exposing hori.z beam.
4 X3 -6/+6 Increase dia of pitch strut to simu- late telescoping NASA system 5 X3 Simulate`gusseted joint at base of dummy strut.
-25/25 Modify gusseted joint simulation 6 X3 (matches drag of 40x80#) Repeat Run 16 R.q = 75 psf
O O
N -15/15 0 8 Pitch run with same configuration as 8*
a
Runs J6 & #7 s = 75 psf 0 c2 3
O'
•-14/14 9 Add large vert fairing & remove 9* X4 dummy strut (40 x 80 14) 10 r 8 Add dummy strut with fairing 10 X5 (40 x 80 J3)
rn_
Complete A/c smooth 0 75 11 MODEL IMAGE BC-11QO4P3Y1V2W1M1Ii E -51/25 11* INV. OUT i Add 15" fin :cap 0 -30/30 12 12* V Repeat 12 9 q 83 psf 0 -30/30 83 12 = Remove fin 14 -15/25 0 75 11 Remove endplates li Remove horizontal 16* stabilizer 10 11 17 11 Add fin With cap V Remove wing $* I 18 19 H l8 Add horizontal and E endplates 20 l8 Remove fin horiz stab & endplates '.FABLE 11 , CONTINUED.
a STATIC T$I T T EST RUN TARE RUN REMARKS CONFIGURATION RANGE RANGE q (LEG) PSF} (DEG) MODEL 21 BCH1QO.4P3Y1 -15/25 0 75 18 20 IMAGZ Repeat Run 120 INV. r' 22 18 V2 19 Add short fin horiz HIE stab & endplates 23 18 18 Add sbo rt fin horiz stab & endplates 24 11 17 Add: wings with W1?41 retracted gear Remove fin 25 13CN1QO4P3X172W1M1H+E 16 16 0 15 MODEL IMAGE Add horiz stab 26 HCN1Q04P3X1VZW1MIH^E -15/25 75 11 INV in 11 14 Add endplates.
10 m cap 11 11 Add fin with 28 V2 0 83 Add 15" fin cap 29 V1 -30j30 12 13 q = 83 -sf 75 12 12 Repeat 129 with q=75psf tV (n MODEL (ALIGN -15/25 0r 32 28 Add fin 31* V UPRIGHT wj10" Cap RUN) i T+I 32* 32 Repeat -131 w/o BEGIN DATA RUNS image Add fin with 15" Cap 0 -30430 33 12 33* V1' O Repeat #33 with q = t3 psf 83 33 12 Remove fin ^15/25 0 75 32 14 Remove endplates 36 32 15 Remove horizontal stab 37* 37 16 ,4 32 17 Add fin with 10" cap 38 V G 75 39 1'8 Remove wing 39 19 Add horiz stab and endplates 40 H E 20 Remove fin, horizontal stab S 41 39 endplates.
39 20 Add transition strips in configure- (TS)2 tiou of LSWT 550 Run x!20 39 Add fin with 15" Cap & tzansition 43 V V strips to match LSWT 550 Run 119 39 18 Add T/R guard. to ,match configuration 44 G ofl LSWT 550 Run 13.8 Add horizontal stab to match LSWT 45 g 39 19 It 550 Run t17 TABLE 11. CONTINUED.
ix 1k STATIC T&I TEST RUN q CONFIGURATION RANGE RANGE TARE REMARKS NOV RUN (DEG) (DEG) [PSF^ a 75 4b 39 Add endplates with transition strips, (Ts) 19 BCN l Q0 4 P 3 Y P I to match LSWT 550 Run 16 47 32 11 Add wings with =etracted gear with W111111 1 1 1 1 trans strips to matchLSWT 550 115 T/R hub, M/R hub Add & exhaust ejec- 48 -30/30 48 12 JTF 11 1 for :siring to match LSWT 55D #24 39 18 Remove wings horiz stab, endplates 15/25 0 75 V2 14./R grit, T/R guard, change to I 1011 fin cap 39 is modify T/R gearbox fairing to pro- GTFIR60 so BCH C ^' S) _1 2 lQ04P 3 YPV2Wl"l'^ 'E duction configuration (compares to 40x80 Run 168) + E 51 B N QO - V.WIMIH F 0 30/30 83 51 13 Yaw run with configuration of #50 1 4 P3 P2 @ 8 = 83 psf 11 ' ' 1 1 1 1 1 52 M 1 W 1 -15/25 0 75 32 17 Add wing with retracted gear (compares to 40x80 Rim 169) I I 53 YJ r 17 Removes production T/R gearbox fairing I H 32 15
Remove fin, add horiz stab O
R60 55 > 32 15c Add M/R @ 60* ;-;a r- 56 E 32 14 Add end plates 32 14 Remove M/R
>
V 2 32 11 Add fin with lo ll cap 59* R 6 59 11 Add M/R @ 60- <r 60 G 59 11 Add T/R guard antenna 51 11 Add 15" fin cap T, 62 0 -30/30 83 48 13 Yaw run with configuration of Rua #61 @ 9 = 83 psf 63 48 13 Remove exhaust ejector fairing 64 75 48 12 Repeat 63 @ q = 75 psf (compares to 40x80 Run #30) i 65 0 -15/25 59 11 Pitch run with configuration of Runs 63 & 64 I I T I I I I 59 1 11 Add 10" fin cap Y4 I 1 1 67* 67 19 Remove wings (compares to 40x80 Ir Run #31) 68 100 67 19 Repeat 467 L a q = 100 psf T 69 p 4 -15/25 75 59 11 Adel wings and open fuel sump re- 111m1 !
cesses (compares to 40x80 Runs f20 & #21) TABLE 11, CONTINUED.
TEST STATIC T&I RUN CONFIGURATION RANGE RANGE q TARE REMARKS RUN No.
(DEG) (DEG) (PSF) R -15/25 75 60 59 11 Remove T/R hub (compares to 40x80 BCH G QO4P4YPV2W1HlII+E Run #22) M T 59 11 Open main gear door, add T/R hub N 59 11 Open nose gear door 73* 32 11 Remove 2S/R hub {compares to 40x80 Run #14) 74* N1 P 3 M1 X2 -12/12 75 74 10 SIMULATED AMES 40x80 same SUPPORT SYSTEM config as #32) If t Remove fin, same config as #35 0 75* 75 BCH1Q04b3Y1.V2WlMlH+ X2 -12/12 0 Remove endplates, 4 76 75 75 10 Same config as #36 Remove horiz stab. Same config as 77* 77 #37 H REPEAT OF RUN 76. #36 78 75 E 75 REPEAT OF RUN 75 #35 80 V REPEAT OF RUN 74 #32 81* 81 Remove horiz stab. Same config as #38 H 82* 82 Remove wing. Same config as 139 N .83* H E 83 Add horizontal stab & endplates.
Same config as #40 Remove fin, horiz stab & endplates 84 * 84 -4^ Same config as #41 .{ Vj 82 Add fin with 10" cap & T/R hub.
85 V2 T Compare with 40x80 468 LSWT 630 #4g 86 81 Add wings with retracted gear.
'HIM, Compare with 40x80 169 LSWT 630 • #52 i[ I 1 Remove fin add horiz stab. Compare 87 H+ 75 with #54 88 Add M/R hub @ 60 0 . Compare with 155 88* R10 88 .Add en p ates. Compare with 89 E' Remove M/R hub. Compare with #57 Add fin With 10" cap, Compare with 91 V2 74 #58 Compare with 09 R. 92 Add M/R hub @ 60°.
92* G 92 Add T/R guard antenna. Compare with #66 94 V1 Add 15" fin cap. Compare with 165 t J TABLE TI. CONTINUED..
a STATIC T&I TEST RUN REMARKS CONFIGURATION RANGE RANGE q TARE RUN NO, (DEG) (DEG) (PSF) R 60 X 0 -28/28 83 95 6 Yaw run @ q-= 83 psf,. Compare with 95* BCN1Q04P3YPV2W^P4111 E l GT e l 40x80 f30, LSWT 630 #63 96 *REMOVE .BUBBLE WIRES #63 Xi 95 X2 -12/12 0 75 92 10 Patch run @ 1 = 75 ps . Compare Va.
with J65 98 92 Add 10 J9 fin cap. Compare with J66 V2 99 ' 83 Remove wing. Compare With 40x80 31 LSWT 630 J67 BCN11Q04P3YI,V'W1140+E GT R 1 0 X 2 100 100 83 Repeat 99 @ J p q = 100 psf. Compare 11 168 with 40x80 #31 LSWT 630 101 BCN1Q04P3YPV2W1M1H+E R60TGX* -12/12 0 75 92 10 Add wings with retracted gear open sump, Compare 40x80 120 :& 21 LSWT 630 169.
102 92 Remove T/R hub. Compare to 40x80 422 LSWT 630 #70 103 M2 T 92 Add T/R hub @ 60'° open main gear door ( Compare to LSWT 630 #71 1-' N 104 92 Open nose gear. door. Compare to LSWT 105 Remove M/R hub 40x80 t14. Compare r to LS WT 630 173 r R60 106 Nl P3 Vl Ml XA 0 -28/28 83 95 6 Repeat of LSWT 630 196, Compare to 40x80 130 LSWT 630 X63 T 107 V2 -x2 -12/12 0 75 82 10 Repeat of LuSW 630 485- Compare to 40x80 f68 LSWT 630 149 82 ADD No. 50 GRIT TO REAR STRUT :(TO PIPE & HOSE) T6)*2 REMOVED GRIT FROM REAR STRUT. Add grit to fuselage Add wing with gear retracted. Com- Will-, J69 pare to 40x80 Add 80 grit sandpaper wingwalks.
(TS)3 81 Compare to 40x89 469 81 Add 1i0 grit sandpaper wingwalks,.
172 (TS)4 Compare to 40x80 469 Add horizontal w/o slat 113 A 74 74 Add endplates. NO GRIT ON ENDPLATES.
114 E (TS)5 E* = GRIT ON ENDPLATES 115 E* 74 TABLE 11. CONCLUDED a fill TEST STATIC T& I RU N CONFIGURATION RANGE RANGE ^q TARE REMARKS RU RUN {DEG) (DEG) 1PSF) -12/12 0 74 10 116 BCN1QOgP Y P V 2 W 1 1d 1 1I (TS)6-XZ 75 Remove endplates. GRIT ON HORIZ TAIL (lower l..e.)
117 HIE (TS)5 1 74 Remove grit from horiz stab. Add I slat and endplates.
Ila V 1 Rl 0 -28/28 83 95 6 Add 15" fin cap, M/R @ 60°, T/R guard yaw run @ q=83. Compare to 40x80 II3
rL^ l
119 (TS)7 95 Remove grit from l.e. of fin. Compare to 40x80 #30 120 V2 X* -12/_12 75 83 10 Remove wing, add fin with 10" cap Compare to 40x80 431
N
N
100 .83 Repeat 120 @ 1 =100 psf. Compare 121 to Q 122 P W M 75 92 Ad wing, open fuel sumps. Compare to 4 1 1 40x80 #20 & 121 P2 92 Add pitot tubes, windshield wipers, pilot's sliding glass window. Com- pare to 40x80 #20 & #21 124 N2 M2 74 Open main and nose gear doors. Com- pare to 40x80 #14 (} These runs were in error because yaw angle was not zero (actually -.79°) * Static tare measured on this run C) 0 (Lj t a ^^l a+ h^ OF POOR QUALITY, r,E4
TA g IX1; CONFIGURATIO N NOMENCLATURE COMPARI SON
LSWT 630 Scale ESWT 550 Full Test Test 'Best Explanation
tail
B Smooth fuselage and boom
0 4 C
CQ 0 4 CQ Pr ot otype c o'w 'ling wit plugged
h
inlets and eje-ctors (Q) and no screens (04)
E E E Endplates canted 3 0 nose right
F l Fl Fl Exhaust ejector fairing
G G G Tf R guard antenna o zer
H H H NACA 0015 h rizonta l stabi li
rY.ra +.1,T B tab) vot ^7 a inri ti n.+. ^r^.+, a .a..t s at deuce
H +
H+ H+ H plus L.B.11slat
Ml Ml Ml .Main landing gear retracted with doors closed M M2 M2 ,Main landing gear retracted with no doors NI Nl NI Nose gear retracted with doors
cl osed
N 2 N2 N2 Nose gear retracted with no doors
0 4 04 - » All screens closed
F 2 F2 F2 Production protuberances; pitot tubes temp probes, windshield co wipers, rotating bea ns, Steps, jack points,
mist drain lines
-- Fuel sump recesses covered
P 3 P3
..
P4 Fuel sump recesses open P4 Q Q Q Fairings to cover engine inlet and plug exhaust ejectors (cont'd) TABLE 111. CONFIGURATION N OMENCL AT URE COMPARISON Symb ol, LSWT 630 Full Scale LSWT 550 Test Test Test Explanation 81 60 R160 8160 Main rotor hub, mast, controls set at 60° azimuth (fore and aft is 0°) T T T Tail rotor hub, mast, controls set • at 60° azimuth (TS) 1 Transition strap configurations used for 603 test. See Pictoral through Configuration Nomenclature (Figure (TS) 7 20 ) for details.
V1 V1 V Vertical fan with stinger and 15" cap (extends to WL 156) V2 V2.^-- Vertical fin with stinger and 10" cap ( extends to WL 151) W1 W1 W1 Prototype NACA 0035 wing with standard tip X1 X1 - 40 x 80. mount with no fairings on vertical support strut X2 X2 -- 40 x 80 mount with both fairings w X2 - 40 x 80 mount with dummy strut
and no fairings
X3 Modifications to X3 . See Pictoral Configuration Nomenclature (Figure through 20 ) for details.
X3 X4 -- - 40 x 80 mount with dummy strut and no fairings X5 - - 40 x 80 mount with dummy strut and both vertical fairings Y1 Y1 - Original prototype T/R gearbox fairing Y Y Y1 Preliminary "production" tail rotor gearbox fairing APPENDICES A -I APJ?BNDI A - L,SWT 630 Tabulated Data
all tabulated wind axis computer data
This appendix contains
from the LSWT 630 test, It is included the aLnterest of com-
in
pleteness and to give the report a 'stand-alone capability.
There are four blocks of tabulated data. First is a set of
data for all runs with all corrections except wind-on T&S's (pp
A-126). Next is a set of data for Runs 32 through 73 on
A-3 to the single strut mounting with all T&Is applied (pp A-127 to A-168). The third data set contains Runs 75 through, 124 for the model mounted on the three-point system with wind-on support tares removed (pp A-169 to A-218). Finally, a set of data for Runs 74 through 107 is provided from which the "model alone"
data of the appropriate configuration in Runs 32 through 73 is
subtracted yielding T&I values for the three-point system (pp A-219 to A-252).
While most of the designations used on these forms are self- of occurrence, explanatory, the following nomenclature, in order is provided for clarity.
TEMP temperature, OF
y v pre--.i s- lb /i -2
dynamic pressure, lb/ft2 QPSF VFPS velocity, £t/s RNFT Reynolds number per foot of length, l/ft Mach number MACH T0l
thru data reduction code identifiers
T20 PNT data point number
of
ALPHA angle attack (positive nose up), deg PSI yaw angle (positive; nose right), deg L/Q lift/q (positive up), ft2 D/Q drag/q (positive aft), ft2 PM/Q pitching moment/q (positive nose up), ft8 Y/Q side force/q (positive right), ft2 rolling moment/q (positive right), ft2 RM/Q YM/Q yawing moment/q (positive nose right), ft3 A--2 E,3 qunlrl li •-3 UJIUGHT. QjairPtl W T Wn* , - TLLNNF.L--T Low C ST -630 WINO :AXES
i lt41948$ . RLIN
nsol I 94 9 14#4696 TEMP pO L A Q *r% J JbmjQ PSI PNT -ALFHA ' Y/Q RM/Q YM/Q ^ f WrQ V r 7, #, 2 2 3 8 ; * O. • : 6!
l 1 ' 7 0 03 7 1169 0i>1 0 * 3 1 169 P81*04^ 9#•O4 4 0•06 06000 3#38 1.416 7*199 w79 v So m 1#193 5 0006 N 8- t 1 # 325 11«59 7*078 -' L- + m i , #428 4#.25 #81 6 000 -10.01 n i*,q tg2 n 7 0"a C6 , . w t9- , 00 14.68 7f4i8 *661 4*79.^ '02 ' 3 55 . . " A 59.
t o - -72*60 " W Is 86 * ' 9 :7 i7 a 'A.S A4 a6fi,,50 , lit lit e 0 * 06. m 386 , 0* , Z@386 6*295 w 61t65 :-81771 23#61 7#•74 11 Oo,06-2002 25c82 1.506 69265 -61 f;49 -30072 9s,75 i 2 Q-Q6 -22-00 J;OA A a ' 4 5 S 25o67 1 i607 5 5 m!6 2 a 73 ° 2 0 J- . 47 6 3 43 1 3 O iO6 — ; 02 * 05 14 7 As T L*'. 0 9 16 0*06 2 0 9*#.03 1;q596 6*627 ,: 09 ; -54060 *7 2 w1#87 3.:99 17 0oO6 108": 8 7 1*476 6*717 w 7 2 #40 jm5ok5E -1#,85
18 QQ6 6 & , Q * o x;u w6oags *
1,506 6#68 7 s lo a .123 74 1664 - . , -06 04 1 06 10 , 00 1.0536 0 W58 , 6 a 05 61;,43 0 5 42: ' : 117 , -.2 w97 0 * 06 12*02 fill i4 6 v ' -st*22 + 97 , 1 22' 0906 1*#.Q0 144*6 64084 -58 f 03 •-5t18 117•, 32 -3#:54, • 23, 0906 16-03 446 , •5 . 241 122*63 1 9 5*271 -46998 241 •Q.80 26 00 , 06 22a01 1«65.7 7'` •71 1 ^"780t -0-1-81 ^0904 244,00 J, st p 047.
`2 Z - 28 0906 25•, 03 1.3 2 '5 5.633 "54 1,920 -49950 '27'1 02 •)4 5 29 0006 Otoi 10596 -3#,193 49941 0 1 8 -4 78..3?. -1#-63 POOR QUA Lnf y WIND :AXES RUN 44 A 1 9 4 SA 0901 -a- ' pd 14r558Q TEMP 64
.i+ • .t eeuA
DC7 i.^Q hlfl f^ F ^^ i ^4rRr, Y/© pM/ YM /Q PM.
1#536',. 5 ,094 10:7' -0.88
00, 1:20 0 00 -674,36
-0+271
. "
•E102il 00:+56 2 Q4.12 ° -2*111:. 1.3336 '5.934 I's,34 -66 62: .
4 6000 1 +02 0 0, Qt12 1,416 6 -65f8 4 0# 21 4 38 0054 1 5 98 0012 -74- 600 it01 00.7Q
1055 84 m 65r62 -0015i
ODU - 2 23 1 .63
. 0. A I SI . -.
11.99 .
7 E •12 . 3a6 .x•16 as 1 1 2
60175 -1 *83 *6b09 6 -13098. 2«k
0W i2 10355 a ^a0!" *66 55 'wat 1 $i •,t g
9 Q s ^. 2 +w'j r ^ ^ 0 Ip ^ b.
_ ^ 95 ` l04 r 4 ^" 6 , ^ is ^",. 1. ^ ^ s L'^.1.- t 2 r^ ^ _ 1
10 -180 P 00 10265 40,23 6923
0^i2 - 60084 -64617 -Qt27l
1 0 3:35
S1 Q012.^S9r95 265 61024 w63t.04 6w,39 - 0tl81
1 1 ,26S w
1 2 11:12 ' 0 22 24r02 1-0 4A
+_00 Aoi45 13 .`
"- " 9'>
'-23 0 x•235 ` 2005
4^i2 " 61935 ^6Stw p at. aQc^ 00P-3.
0615,97
•1;4 +"12 '^35 ^ p4 ^..^05 w i ^7 ^ 8 ".6^F
0. 6 265 ,. Cl t 03ti^
0012 1099 1,536 16 50783 - -01241 1'F44 m10.•80 64%76 17 40100 10506 l«75 o012 5.843 -00301 -20;72 64*49 lw88 .3r 4
8.00
1.9 -wQt271.- 04i2 1 436 5,364 -65.023 *4%57 20, 10000
53394 ; • .5020'
1-6456 64093 t a12
21 too 6,004 -64.96 1gi
i.3 1%& 6.28
13 0,99 22. Q 012. -65, x 1
1-0355 61084 0 0#0.90 m7 R2 1
;23
Qa12. 15099 10355 60145 48«23 -65#83 -0x120 -0'S-51 ^.
!25 Ca"0000 1.325 ^0.w3 •8.p0 0'-"22 ; 5e843 -600::30 -0tc.41 x .
22.00
126 0o f 12" y •295 ► •8,,31
5^ 873. .59 74 ^at39:;?" 1051 24.12 i.ZOE 51, •n"• 422 a•'^^ 0&32 ." .^.7g
rr' 2 2' 37.3
-60-10"
-600,29
^. 28 0012. 24099 1,0205 2.64
50934 op,48e 09*,24
OCx2 29 0.12 1.0596 5+783 -00229 0371 64057 - io48 F O NT ALPHA PM/Q YM/Q P S X D/Q 'Y/Q RMIG L/Q 4 44 #41 1. NOW28, 1 0*16 0 OR q S12 7 -86 9 wQ , . 00 0 #_5 1 S^ 5 i ; 25 = 4030 '86 7a. ^^ -04361 0 444 A 4 OR!6 -54-99 0 0 422 91.70 2*27 79524 -85427 - 0 9594 o w S *00 6 4i16 0 0 392 -1 q 1*5 114 , 30 3*05 7041,0 "820-04 6 0116 -9 * 59 - a ,gn lRs3Q 04 A ZE 2 . 3 A 0 -1129 45 " w 3 ot53 ti 7 0#16 : O -00 ofta le 7456 0 0-8608!^ Cr 271, -Ow*a - , 2s00 0 5 ; • 3#74 0414 -86 60 Q 4 * 12 7,560, 2^ Ft "0091,
9 balk 41 9 2
o 4 .2ok -8 10 5W99 Q!16 0. !}52 7 . #620 3.:89 -2,77 04 850,78 "0f151' .11- 0,16 Of#52 -0009 -3,45 Oo512 7*590 -84941
Ap 0 # 1 A 90,99 ! 2 4.23
-20 - 69 .
-040: 3*53 00 , 16 0+3 12 M04,13 7 . 5. 6 G ! MCw471:- .
kAll,
0 r", E q ,; I r , ^
A-15 OF p ow, qula-iTy WXND:AXES .
TEMP a 1 4 R5 i4«5580 MACH-0*237^f Q p sF 83*00 'VFPS 271#23 160 RNFT , c "l o t To* Z03 T04 Tos To ul !09 T09 T- 1 0.
0 0 0: 0 0 701 0 1 0 0.
Tit TZQ T12 T13 Ti* T 15 Ti6 T 1. 1 Ti g TIS 01 P., RLIPPff R*rg. iaMt e. I,: Ai r !
4T y m A ' A T PNT - ALPHA -PSI Y/ Q RM/Q YM Irl f - Pm/a 1 6 1, , 6. 8 a 0010 7 ;, 1 x t 0•:00 0#4$2 .481-31 I 0 0-03 , I I 1 .1 W: ..
., 482 8^4 7 -^87 1 a # , 7• 6 a 0#30 1.11 1,3 QmAO 4 1,4 09: w o6i01 4 0, , 10 09964 1 106 3.x73.
04422 7#741 waa *: 93 w 5 O * iQ 0-00 8c62, 0#452 7 , 9801 0 90 * . 1 0 r 0+ 542 1•.4 1, 6 0 m i M 24-00 0 R!P* :1 _2 ca. 71 0 0 6 ,4 *t^ 8 O.V,69 1 0 ".
to 4^ 0 a 0 0 , 23 :10 'f 422 3 4 7 , f 00 1 0 at.
7t , in Q,anl R-Ad _ffsj,!Wj :,O.:Ahg 2r s, : :z a al A-7 WIND :AXES 090!7 .
I TEMP 440-5629 85 Pa.
..&I.12 ;Fci, UA pN( FNT RM/Q YM/Q /0 Y/Q i.
C : q coo..
000 7- 5: 0, 0*09 -6 Woo Ci. 361 a M43 80313 -93089 0 0#693 4,6,08 0+.09 000 04482 4x71 71 1 W69 aq353 -94#51 -0031 W 6 ^j w i g a 048 40,00 - -253 ^ *93 13 a ft2ACk A'^,AA^ it -sQ ,6 cb --,ftt%ft A^ d^ f^k C- TEMP 8510 405 62: P8 1 0P8F 8$00 VFPS P.72#18 t MACH 0*2378
RNFT 159012a
701 1 0 0 0 0
0 0 Q 0 T11 T12 T13 T14 TIS T16 T17 T18 T19 T20 .
PSI Y/W I RMaQ ' YM/Q
PNT ALPHA L/Q D/Q PM / 9
I
O'k 09
00632 8+133 01 , 12u 00'77'
w9a* F3
,^ Z.
^_A I it ft x I ^. r^_ 3.tt7 , 2 3 2 0=0 W 4 0.09 w 6001 464 6 3« 010566 8 1 0 '02 w9 10 •0030 1 1 1 53 10 0.09 N atoZ. , $025 00512 80202 *911010 0 00422 4«59 7 -11 «99 0,05 09 i2 7*882 '4 61 w 0sw61 0 87#1* 5=78 5#34 0006 012«93 vso:392 6$a 0.a 2 70952 *86*28 0 a 09 81640, 1 _^_,^2 #MiR 10 0009 -18100 0 * 753 -0f422 4-1071 7.169 w74#88 6160 11 0.09 "19099 •» 010542 6«40 00783 70289 80'80 n 75v59 .
^.? 0k0 0:{# .
a'1 13 0#213 7#380 m0*SU4 10 +w13
X 77 68 11«09
*2641 1 0*09 1 5 1008 i)%343 710470 ` *0# S 4 It jy2 '*78«26 SS , 16 0009 2001 D 0542 0$7b3 -5 , 0.32 80102 0 9210-41 '00011 17 0009 39-98 810042 00542 00693 ® 4089 -91957 ®0e,73 '7#$w$ i9 Dios •
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p8 .
89 4 1 4, r6464 : 76.00 QPSF 258, .94 CtACH OtZ8
VFPS FtN T' iSQ:185Q^ 54
T01 T02 .703 ,TO* T03_ TQs To U7 0 0 0 '32 0 0 0 1 1 0 0 i 0 T 8 20 T12 T13 Ti* T 15 16 T1 T19 T 14 , T 7 T1 0 Q r 0 0 .;SUPPORT DATA iFULL SCALE QA'TA SINd LE DkT^ ' AT Q.©.
° p sr PNT .ALPHA 'D/Q Y/( RM/Q YM/Q .L / Q PM/Q t M G*01 *0#01 7.093, 41 59.933 1 +'92 7.257 103~22 s 0147087 2 :-360Z .0t01 $8400 6.933 -0124.34 6+200 25 44 v V3*w53 3 t#*3 + * 99 ° - 001 w0e133 ,"6t933- wi 4S * 01 6#500 31151 ai,58.80 __ .. 4 .•5-.99 -0. 01 -3.933 7,1.33 - 7 o 067 37 474 x +161 q,46 1.61 i 0 040 74567 454'17 -11640,38- .10 8,02 1 -79667 % 176#'59 7 ° +240 6 w 9e99 -0s,0 1 wi2,109- 80267 wia9goi 7020 53 h 13 mi120e30 7, -x14*93 s ' -004 74967 59473 •4168426 P,17a1,00 99033 mt96t65 0 .14`402 0 651«05 ,*1580,26 3: 0,001 , i*214620 10*20Q 847, , . • 20507 R 61 , w,i480,10 10° 040V -00-01 ; 59967 19-1374 7f433 71ti33 '+102937 1i 21000, -001 59367 i4v09 •140926 10x800 79433 -82:,88 x659.14 '12 0 0001 9.55 3099' 13o433 71,700 40893 0132.67 X1284.47 1.3 00401 302 164600 8903.3 — 44140 494. 07 6#4 1 113&29 14r 8f0'S ; '..Ot01, 8.433 A, 199733. • 2408 0667 !120*76 •16 10.eM • Oa01. .4t54 ; w 9*77 12067 9tt67 5#967 "119.29 16 , -0+.01 -16.03 1,2401 25.8.33 59200 101 9tQ5.
10v100 16t4i 913 «99 '1.7 -0901 260520 11.9767 344, 72 69100 -27x43 w111e11 w O * 18 15e.`99 01 289667 69633 +*109918 13%167 §0978 15 18#00 • -311,46 •119«17 #0 0a.O1. 60r60 4x633 28.907 •14.840,' 90' 20#Ot, -0401 -304;78 28.973 X61647 4 39967 -12202 " 7035 21.. :22902: -34.55 •128.93 0 001_30#9,40 181407 a *-t6— 4'o997 ..^ r0*01 .22 •24001 44«25 •4131.52 319827 208273 96156 0867 - 25.:00 :23 - 09,01 59587 -48x95 219600 100!'20 A133g21 340073 w 0o02 -0401 7,200 5067 19%48 *148#,26 24 ' 7.133 *104.27 n^C^dGr1^JG p ! ^ C ^ ^ nn g g {; Cq ^ A-41 D W'IN . iTUNNEL N m, SPEE A T — L jVeU ,._._ :AXES WIND OluT liziJlml ! - RVr4 AX I ' R. 14r6464, TEMP 940 T.
: MACH 002254' OPSF °' 75tOO RNFT 14846140 YFP9 260114.
' TAg TQ'4 T1.0
TQf '109 T'03 .To4 Tas TQ6 Tol
1 0 0 0 Q 0 39 0 0 0 0 ' T18 T15 T20 T.ii Ti2 Ti3 %4 T15 T16 T17 d _S?
SCALE LIA-T ♦ Wk'AT C.6 iFULL, OA o r 81NGLL 4uptpoR1" YM/Q PSI 'Y/Q PM/Q PNT ALPHA PM/Q 'L/Q 'D/Q 2 g Y14 X1470.58.
5%567 1 Qo02 0401 5.767 ..
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r 12 '1:2 4001 0.01 3 3 -6 0 t 71 407.13 :,.
7x99: ^i3oe49> 466?
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I ORIGINAL PAGE 15 QUALITY OF ( P OOR A-42
ORMNAL
WIND ;AXES ;_ •.
Y1/^Z9lAY O Sa^ RUN RUN 60• ^Y 14r6N64 pd.
TEMP 94# RM / Q YM/Q.
PM / Q IWO PMT ALPHA P SI ' L /Q ' D/Q 2#1,38 + i5i° 30 5 . 1767 ° ; Q•C7i^ 7#.267 t4xS4 1 «tl#a$ .10.0!33 29459r w152vo2 1Z 90 ,^ ► 1t^,94 0 0 0 ' 7.80Q v13#.767 6'i061: 38«00 '*157*20 3 • ► ¢ Qi01 .17.300 L 9• b0 107.52 1*02 45W05 • ,163 , 0 6.500 98 x6.01 +01 p,21t800 - 9#033 137#.48 51:21 4171#:2.3 0t,01. 7!200 5 '-7094 *23 * 700 104180 144-02 59089 .. C)!; 7-#36 4 17 1s5 6 mi0#01 0#01 m24,20.0- ___.
7.313 b6i^22 f.68«90 1*4p00 7 *t2#0Z 00S -27.267 :12:4667 7r36`m16522 6+9b^ : 1.3967 8 r^t+i0 Q'0i r '^9fi3!67 152x17& F &7i$3r'`159 =6060^k 0101 was3t30' 3rt93 *13 9 - 56 --- 69%36 *150#21 69013 Q901 , 10..15!01, .30#947 149 727 161• 30 220159 mi154a-78 59867 11. 10 06. 02 0401 *i0000 42#49 74467 15.49 *15051 0.01 5#567 :12 2i 02 -6.667 3 $ #'8?
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RUN , ki ..Rum #a TEMP 94 0 P5 . 14 0.61464= rl ► 1`1 . A, MLIA oeT •r a ImIFA. eMiQ •Y/ CJ RM/Q ' YM/Q 1 • i\ 1 .A1dV r1/1 wr N. r 6.( ".
1 0 Q -j Q401 -1i i33 5##6.7 ► 940 8 0: # 2 46 27 'o
.2033 .wQ4$
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i m2#000 50iQ. 0 ^i27.70 ti0^Y6^ -6003 04-01 w 3p867 5*800 Q#JP33 -0x79 m20=78 143030 w 5 09847 -0o,88 '-7099 N 4,700 • 156o,24 =S *,65 0 t0. 60,100 -9099 0401 5.7Q-0 0.57 -00.91 6#433 w 170 * 09 ^* 0«Oi s `Q,367 1 7 •^i g ^01 ,..6.,967. •111 14 "00 109 6033 .Z81 X94 8 da01 o1r,6^ 3, :13.'
-14 0* - 7:433 QROk7 8x100 *^:19 g ^46 #7L67+ ^^0f ,9 6 , 0 '001: s r 3 3019 wi5 wg iifi 67 7 00117 Air 1 67 0 0R01: 33 0•.02 . 50333 m 0 . 00 w i% 20,6E -94*28 0001 mi0,36 it 1099 - 01267 50300 0 1 -00267 0+ 79 4 0907 :i -63 CP -I *.I5 2 4001 0601 00733 00.98 0 0OU0 -.9*300 .
i3 $•0a ' o 00.01 w0+F733 Ov9 0066 1.661 50367 g'x38' 1,4 84Q 0e41: = ^fi^0^ +^ta0£3 . 0 13 -.
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OWCM M r,,r m cM —44 ' IF POOR VOUGHt lflW WIND TUNNEL TrSY -630 SPEED .AXES WIND • PC 1*4 , 6120 TEMP 76o RM/Q - YM/Q FNT ALPHA PSI 'D/Q 'Y/Q PM/Q 'L/Q .
- . •0'«80 0#96 - 0*1 . 67 .
3 ^ wSf SA 0'&01` °2,733 59741 m125r46 n lwoo 4 600 5#98Q 01 -1-k01 0,9E Q 0 w 3#633 -141o +4 Q 0 273 5 '-7# 6013 -0,7t 99 OvOl -0#,19 4t 567 ^157 °95 0000 9#99 0 ^ 9' s 0%58 0401 w 6*55-7• 6.680 -171 @,27 0#Z-00 .
v 1 7 alZo , 02 001 Btso 0 6*800 7*013 0 18 3 t . 29 ' 10 0 *047 *4 3 mi.* aiol -Ot"72 4 m , 4 0 1 ` • 70(00 'X# 44 3 360 50 -19*v7Q •15109 9 O001 6 4,500, 7#880,w200042 0 0#400 10 0 # 65 3*49 IQ 0 * 01 001 0 0#667 5*533 -9303 1; , 46 -0#353 - 006 4 11 2#00 okoi 0 # 233 00#360 n 0%65 , 43 59580 m o 76r,99 1•, 0 to 1 mooss S #^ 5 • 12 41 , 02 16267 s. 8 -0#69 . 0 2 S *5 4Z w6 e 2 -- ,0a63 6.02 Q mo O t5Z 13 #067' 0 1 a•400 5 , 913 -47 k60 lw l 11002 0*01 3067 6 , #Q 7. , , m3 1 * 26 . - i t? . 67 -0*40 0113 -14 ► .
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o: 0001. fol 0 033 6 " 013!) .*.62 I ,!.O q oo a 00 *92R56. ' -x, 1-2.03 Q! 04 .967, 6*233 50433'' w1o ' 5o$5 a . -4 1 t oi 0 `4 01 !-91967 6033a 1 * 19 , 91AA- - i 4 6000 Q9,01 833 3 w1,*O#-42 6000 014$09 6 • W33 40#,59 w140@-59 5 .-840Q OoOl *40833 6o800 - 4 5*913 19 181 43*. 44 wJ28 &5' 6 w10#02 -OtOl -5 933' 71233 544,33 w 1 6 7,x° 9 2 4 * 600 43*93 4 7 w1,t#99 0*01. -7.0.00 0 1,14,*71 7•700 4 1 79#4 8 .
w 10. V^ VM Q#01 m g 4 0 0 00 , 103 300 ^-04$0477 Eitll -4134 0.93.
1,0 O•OQ OtOl w I v000 6.1.60 m 92i67 591 20 -11 2401 OtOl Qq167 14t76 x:127919 69167 *, - 76w43 4#713 49267 1 Ti: 3 i '.1 2 1011 !12 4600 0*01 0.900 66167 m6Q em 5*32. ; 1 !1 . 18 v - 59 642 0 & 01 3# 413 13 A 1#933 6 i 367' 47.06 0115 0120*36 30193 ' ' -1k $0,02 0901 3 - 047 64,590 5-80 ".*290'93 067 68 - t122:' % 03 :001 4 ,033 cosoc '16# 91 3t ' 2 9 933 -t123 00,01 5vi00 -8161 •,39 6 :14 # 0w 7#1,33 1,87 2o567 --12 w 70 mi1,22•,70 !00 0001 5o933 7,9567 15950 '17- •14 32•,3 6 2o233 -16.•33 IS 1.6#00 0# 01 01 6*767 7.833 mi19•01 .
! 114o30 '17.99 - 0 101 7 * 433 8067 49*65 1#460 - 19 , 36- " 1 19099 8#833 0 20 9, 01 3#067 6'5,#12' ;•24 C . I r s - 67, .30 21^ "22 * 0! O,0171 1 90, 367 2..e 98*44 85833* 'o .25 2 stiEG #77 22• 04 QtOl 9#833 109033 39767 '3 97ti* ► 23. 25900 3 t 7. 00 -33915 0 -il7i77 0 10110.100 10P267 102#, 43• i5t4l, *134*.94 .2* , -0*01 0#0 1 -16033 6910 • 92.50 59173 , TEST .•630 V LIGHT Law y-VE- WIN D TUNN9L WIND .'AXES RUIN .44 AWN ^ 9/83 090.7 RG 14#-5973, TBMP 76 ► _ MACH 0•:2258 • Qp F 75vo0 VFRB 28+r'' RNFT 1541668 Tla
T02 jr,03 T04 Taa Tay X99 T05
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LE iSYPPORT .OA LTL 0AT_ _5i ' Q RM/O YM/ Q FNT ALPH ID/-Q QM/Q Y/ A -PSI L/Q • 533.
S 0.01, 04*01 - 59114 93t73.
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5 n 8 # 01 0'.01 40.93 .142•:26
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P. P. 23 143 .106 #78 OZ 0 01 11 f 233 9 '.000 61.,85 1 #x,.80 .
.
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WIND :axes
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.;19,700 9.167 6,080 .x21;.333 10 110 # 38 6t233 45 154 "147 *:00 -8 i 00 00i *333 : 6 •10.05 0 . 5#000 49 o 70 01 "23.200 • , 5 2Q .37 so J* 07 .1 10 .. 1 .
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i9 18 # 0 1 tact? , 67, lC3i01 «116.'75
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•2D.333 •13+ 1322 ml16,v03 41^J^021.
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2^F -0#01 04 01 "896 00 704U 18021
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T i t T12 T13
0 , 0 0 1 Q o $2 . 32 SCALE 0 ATA 81f4aLit ;SUPPORT DAyA c^#a* :i.F-ULL RM/Q YM/Q PNT ALPHA 'D/Q PM/Q PSI L/Q 0 1 00 1 39473 6 07 7.700 :]. 5524,3 F, 32 1 3 " 7 9 . ., 137*6 0401 . 0 13 * 433 41400 4745 5 -t 5 00 24o;90 wi4603^ ' # 9767 a 5 tl q 5 9260 3 -A 4,01, si i 7 .267 4:35 40 m15l07l
4 w 6100 0001• w210500 90433 1330 . 43 61300
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14s400 90033 =lil147
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Y OxOI w 9
25 —0#00 #620 7*767 39*40 20 ' qt*3 TED WINO &IPL, Trq? 430 WIND -AXES YM/Q Rmllpl PNT L./ Q D/Q P3 /0 'Y/Q ALPHA -P S I Oa 0136 6g 93 .
.
3 034" 39•-59 Nq O6 q , 04 OW02 4t827 *22*93 3 10*700 iOV70 W8.9 6026Q 45 014*491 •269653 12020 1194.05 - m 13 8 .67 00,02 *12.00 .04-02 w33 667 J6 167. 12ji55 5 l 4 Is al 90 0.1% 5 6 :"133 *35 *93 4$#073 . 4 , 6 2 K 6 X122,,88 19ii8 otJ605 -09 . 02 - . 8 10 4 900 9*1,87 54127 0 0 32 81 BOOQ O;02 U3 4 800 9*267 5#927 1 2 i *7 m137o77 It 1- 5 #40 40 1 A8 WiV 443 1 6- p o 6.327 3, 0 99 - 0 'coa 0333 9, 4 533 'A14 17 15: Ai*jwO, *132 — 3 W OtOZ, 3 .* 933 , i,133 5 .27 w oz 44 0; 4 2 ' o. k 7 ,67' 1 0, .
iii.367 15: 14x0! ° 0402 i 1 •-90 iZiOi 0: 0 2 P520+6 4.093 16 4 4*367 :iaoW 17 •4i r 01.
0 0 2 17#20 0 -14033 6 6 5 4, 00 3027 - 150,53 0120•,46 -190, 29 * ! 1 14 W59 ox. 1 02_ -7 S * , 6 2 2#9 3 is '1.5499 g 0o107 15*547 11 ____.. I- ^ , - *17 9 ,0s Okoi 13#300 1,7 :F30#0 w8 5 :•30 ,,o29 41 4 oltoa ll t iV 9 4 , 40 Zo 0 1,55' 173 0,#,8 A st 21, 2 a 0 a R02 3i •'X'67 0) e-66 w5l w4S *136t26 25 * 500 w112c28 6x 427 22- 62308 002 38,373 6e860 054,0 -m139 m,51 as .23 •2407 -'Q 0 2 42 000 "27,•893 11 9 • ., 64 19 *9§ M8. 06 0 wOS *69 0 002 0o - 02 o 967 9 1 i l WiGE"ii' l l Fr I -S - . i3 OF POOR QUA L61, A--50 Not)GHT LMW SPE90 WINO ' F UNNEL .TFqT,:630 WIND 'AX8S
fly", 1 1 4 8 fizi!3/8
RUN 769 a4*-5973- TEMP PNT ALPHA RM / Q YM/Q PST PM/Q 'Y/Q 'L/Q 17«24 , 00 0 R 01 . 330 if 4 ,46 76 3 4#
i 33 1 2-7 , 33 48 t a 0 x 093 67
^ i OtOZ -m6 @,Oi 4 167 --4f100 21x'27 -!iZQ o-49 wiOq600 '13 0 52e50 oroa -84 , 00 *18 m106100 13 633 2i * 4 491 , 29 '-74967 100 -,22 6 ' ,A iOo'02 1 9 i87 0102 *2*21 012*767, 'w7l' # ,9 -9s232. -i^1600 I .
7 0002 0 - 0 wS P,0 0 0 15.600 0 0 1 7 #53: ^ 4 I A.fl I CS 47 St A 4^, I L 4 , 0,04 1 9 4 1 '94 Q - =;z I 0.0 • 181, 00 1;4#,60 400189 a8 t333 af 62 N32,633 10 333 20 # 627 oo01 '-204,02 0.
11 , -$q00 0379633 00^00 230133 12 41 72#,76 .12 0600 0 220p0o 104,593 0 91090 W80 6+ 047 *2 *2 02 7 •439100 , 3 3 40 2: .13 0.0Q . . !,R48 06 '60: 1,!
. t3l— 0 5#24,7 w31 70 7 a#00 . 4 * 8 tol 6. 133 a 6 bob 1 vs m -Y. : is x 4 4 g a r 1 6'066, 169 i 7t, 46 0000.-'304-01 40#000 • e 5v;o4 X61 279 . , 02 6.647 0 120 '1 1 7203 17- 000 -0!01 -9000 q 867 5013 i5v1,0 "136 f . , 6 5 :12 404.88 o lzo i 0000 ze, 01 600 -, 13 OOQ 7s433 Og w122v63 - --Is tS 4 02 •8w267 ;. 1 34367 9085, 1 2, 3,607 '410 * t V 1o63 I « 0 C t OZ 1- 7, 2 67 2 9 4 4*1 767 28 +x 340: 13 15543'
' 21 cioo, t j j 6 2Ot87 : 15 , 0
1001 - -697 , 00 : 15#609 19 3 15 #173#51 .22, '000 12 , 00 16 .3 -5#900 16#800 259$00 6 -199*47 11,•46 23. 0j , oQ 14'• Q1 - 4q633 18 * 333 3011'87 16 *53 -!U5 x69 7 21 - 34 •24 0#00 16401 w 3#200 20 #133 mao , go 359367 16033 4255i15 '25 , -00 , 00 11 1 w00 t q, 133 22 1 #400 -2.0 t,5& '359967 ' 28 a * .69 ' 1 & X55 a 46#300' 26 0;00 20401 0#933 X24+ 913 X31 ,'59 1 . 6 4x46.-303x24 2? 00 lo ,r-68 27 0*00 2 -38 t i0 5- 1 0 0 10: •29 01 20 707 9.09 0000 24wol 6«6 4 *t433 31#033 w48t17 56t267 loo 37, x,3 2 OsOO . 26•1 6 t , 86 w - -50 •23 61 5 9 767 3*9600 ^476 , 02 t 0 07 30 osoo. ; 28400 6 * 027 0 38#293 mo 4s^8 :6500 -0;41 *366,44 , 31" 0 4 30,00 wi.5 % 26, . 95 '67 e, sm 366# 4 1.84 7 ^"2 9727 &c W 4^ 7 a j_#', • oa* 933 lat g O x13 7 ; #40 A-51 ^9! ^^Q a' P NAUGHT LMW SPEED WI&D TUNWEL 30 TE ST WIND :AXES +44 RUN RUN Jig 14.6562.
° TEMP 75,.00 MACH O vZ354 6^P5F " ROT X 629067 9 VF 250 + 71 ^ ..
' toit Tag
102 tai roe gas s4^c any Tig
cart 0 0 0 0 0 i} 0 0 0 0 T20 . T12 T13 T14 T,ig TO Tit T15 T16 TO ' 1 32 0 0 Q. O 1 0 ,FULL CA, SCALE DATA, DAtk pAlrA eT SIM - "Y/Q RM/Q YM/0 FNT ALPHA PSI .4/Q 'D/Q PM/Q 2 a16 1 =0.03 x,.0'33 5 0 oll.54y '*'90 1 0001 * ► 5S x34 . 53 6+000 ^ i .
Ii hK KA •A-O=Ati.. . Qa.14 au < 27 1 M .., rre..i.r 2. M *9^ ^^W^ ..#^RZ{J^7 p^IVV ^,i,47Raf ^^. ^ - !-*4
60340 • ^t16tY B6
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3 0**L °-267QQ
'iy02 06 ,,0 , 40.29 ,16'7'* 7 5 61787 _ 4 O9.01 M 3+600 6x400 -i44f67 ..
"8004 47«5Q 172r,76 5 0,,01 70253 - 4 000 6#767 p -157r25 , , of r 53s-59 +r 167 ..
6 p o 0 1 7o227, 41 9. 60 59'wZO -w162A63 .Of 6x853.
7 +eft* : 02 -6-#933' 7.667 1x8 * 33 $ 61263 ; 63.24 m151*95 +.1+x•01' 0*01 •+1S&S, 76r 8.233
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4928.7 "0 9 39 4131.98 i.3#99 -001 54633 6x833 1,5182 -17«79 ai33•.33 0+01 58^ . 16402 6#800 6187 7*5 0 0 29.&99_ 259321+^23'`.i12Js32 19; 01.
''i8^02 11400Q $*204 45^i0 2'8693 .-2 1*jr40. -4i24*i4 20 20*03 004, 8o,833 8*733+ 60020 i,90 .30i 47 .22.01 ^0°41 2 2 91407 76:47 3'*013 21. _ 9. . WIL24 t 3087 -32.39 m^122+i78 :22 0001 87 % 89 •2.4x02 10#467 SO*U67 - 35 *;39 3+x053 X120.86 :23. ;25.02 001 10*467 141v g 00 95f57 -95y32 5.653 21x+05 :154.32 °2.4A •0a0i -i t pOQ 6,000 OQ OF poor'.
Leiw p - PECIIND TUNgNFL TEST' VOUGHT -AXE'S RQN ISO l^Q RUN
16759
MP b Pti X4 MACH ,Q!2252 Q p SF vrps 252000 RNFT 1606 50 40 , 1 0 0 39 0 0. 0 U T13 Ti* T1 5 rib Til US T15 T20 I TIZ Qt 0 4 0 0 X32 1,T d FULL, OCALIj DATA S-MaLk SUP)RCIRT-,D -2AIA RM/Q Y/Q YM/Q FNT ALPHA ^PSX 'D/Q PM/(*, IL/Q 21*01 3 , - 0 1570 , 50 GAOI -1,0100 54900 0 0 00 50933 .,0 98066 !mgwoa "0 0 0j -j 6#000 6 033 ZS*66 qq ^ 64 .91 s ,7 7 - 9,74 6soob 35*t7 71•97 3 0#01 * , -2#gD ' 0 v40 182.0;1,8 U#01 --36933 61433 *1,43 7 0922'1 43 J + w e" 00 .01 - 5 -wa" s 00 01.0 1 *007 QQ mi 153 7, 0 853 5 -ig^ 5 0 , 00 #68 7, o8 0 0 57 . 811 *1 80.3 0 ..•01 06 # JOO 76 200 -1 6S # 4q 6 -9t99 . , - 620,94, - ' 17105 7 OiZtOt O ' l t 0 1 - -7,267 74633 -1-71 08 7,f2 8 O - 611 5 w155*20 6*633 8 ow 0 v 94 0*01, -841467 SoR67 wi g 5-60
A 6-0 3 331 68162 -- * 4 *A—
9 , m , 11,91 - 041 -9^,000 9s5Q w19O#i2 - Q - 0004 wl 207 w11 5 7-8S 10 4 O 51300 1 06 S#aQO - 0 00Q w 97 1 3 .,39 O R 15 0 *^ 8 0 11 0 iOi, 2 . 02 -X011.67 541867 *83 * 49 0001 13 *141 .88 .12 4 s 0 1 0.800 5*867 w6at56 3 -0$4 1 0#01 49533 08 13 6a03 31867 -54*96 141767 kt207 a 0 e , 96 -402e,23 00 0'1 2 , 6*000 •-36o , 05 soot 41667 19 -t ij 4sJ67 m 5w!5O.. w130' 15 10000 6 * 167 Ot i^l, 3 q SQ0, - .2 t S 6 41267 "10v79 Ai310, 83 01x01 641400 1.6 :12 0 0 l, 4.414 00 49333 -1-5*, 23 - 4 134, t ,63 0.0 1 5 1 633 6000 i21i8 17^ 1 . 4#00 w80*56_-s140*,08
Oooi A1 167 7.267 25.9 E 44200
IS 46099 .
29900 .-R4 f , 52 - R 1 ^5 1 , 4 7 01 89100 39si8 19 , 1709 01 4 741900 .3'0 1 61, -1360 ; 93 i 7 0 2Q 20,004 0 900 55 0 16 34121 0 4,0 1 8, 89'7,33 * k_kZ 68,#98 30567 ' m 35.9,, 52 0136417,4, 21, .21-99 09-01 9,700 ?,633 -- 4 04 1 .01 1*, IQ "135e67 .22 -2*41O3 1041533 1.09207 82*'87 . "*3•i5 *133C , 80 8 7 t, 9. 9 31600 .23, *25v00 0*01 1041967 l041467 15x, 2 3 59767 209, 42 41+ -Oqoj 0401, -1 * 067 6*967 - 99t46 •2* L ri M A-53 ..' N OW381 Lcw serEp wyNcl TUK1wFj__TEs1_AU WXND'AXES 0907 AUN Si.
RUN 01 11ii9z91 TEMP 64 pd 1406808 PNT RM/Q -ALPHA P S I D/Q 'Y/Q YVQ L/Q PM/Q 0*01 000. 00 W 01664 . 08 934 5 ► 873 6 64 0 : w01 0 400 0 0.' 6 0 2 So 96 1 k w99 pjl IWO 66* 8*83 35 0P - 7, 0 , 1 + 0 a 0 r 9 6.81. *143,,83 t 5+'9 430 1 6*325 0 100*72 0 3!223 E 5 002- 08*00 0*68 O•e271 6s9Z8 w i07018 0 70018 w12507 6 0.02 9.899 0,R1F3 11 70 r 1 0. S 6 4 5 O0 X1 05.5 2 f l t 7 7 1 7 O ► 0 12eQQ 0 - U 4 34 vo , . to! 5^ 66 : 015t187t . 49s,72 -87,67 901'57 1, 8:^ 6 , 42 , 9.I;e 03 -67#49 0,04 Z* 0 1 0 783 40 f -1.10 0iQ 9 ,-50.•50 0 . 331 A24048 -69 1 s, 94 42 247 12, 419 08 0*02 w 174, 99 136886 0*422 426.566 -109 , 08 '-29*.64 -70s'67 11 0,02 0 1.9499 00482 1, 5.9 07091 - 6 9,53 64 0600, 65 *300663 0*09 . 0 2.1 42 99 OA33 18 * 373 w50 i35- *34#910 1 0 #36, 04 094 U 13 000Z : i *23# , 29.57 0E873 2 10235 : 3R 4 S106 -4t 54 , 0 -1 : 099 Ot i. 02•"' 26 Is 205 24 361 w3 4 4, ^ 494 18 47 . v99 15 6'* ' 07 - 02 ^"28407 1#117 447079 ,, OR '27, 992- ^-2St 1jP 6 •16 OsOZ w, 30 cQ3 0 2*J99 3IP687 1,6v72 11085 s 6'- F o 8 •51.0 898 17 0 ► 02 G O P.Oi 01 * 024 E 5 ,934 - 970-68 , 5*873 18t71 01560: 52 i8 0002 24.01 b i 6 6 jj_4j 240,90 0 8 "404 1 59.13 19 0"02 309'3 6 a 31s, + 15 x» 00' 9 34, 4*6 : a i0i q " 65: . - lo t 816 14161907: 5.•98 350,35 20 0'02 -0i,873 .149938 60498 _1054 1 12 ' Sou i l 72, w0#542 2 9 38 , 0 0i87 21 CoO Z 7*98 wlfl e Si 1 5 0458 4 "152024 :22 9*99 0002 0 80253 - i 1 =17.20.08 0,1:20 8 t, 9 9 19 , 2 1 + 7 47t1O 23 0003 110,98 51086 01 , 211 50217 0 121 "1a9o92 , 87 -289 E 92 0 .03- 1 4 l, 00 _0.33 1 1 1 e 054 w116 ► 86 27*319 55v75 m 25 0003 15,0$ -04030 124620 , 94 31: • 242 55080 v ^ P _ 1 4 9 6 -1Q4* -85* - 84 =35.
26 , 0*04 15*00 -0 v 452 14.x:67 6 5 1 5 4 *43 a l - a 3 2 f51 ZOk01 - C. 753. 16.^j46 .76w3y Q 54s39 27. 01 : _ i39191 `259.31 0100, 21*99 00#988 18,946 -60 * 11 . 440608 63090 8289*05 0*00. 23 •, 98 01041.6 210506 •42023 48-554 51,,09 0311162 30 01 ► . 235 0*00 26 00 5 78 m28 ► . 46 5304, 64 41* - 55 ^326.72 31 0.00 29003 • 2.1,69 53 ► 283 01*75 -233907 28.247 11098 G•CO ► 99 29 •.1 0 :639 32 ,0 000 '57*681 -8*63 wie49*85 21 .02 0+ 01 s 00 -Ij 054 - x9 - 19i87 ' 904 097 ES - 5*813, , -i 1 5 7 ,74 O.
OF POOP,, Quf,^;xnx WIND.TUNNEL TEST 630 VCUGHT Lmw SPFEU WIND AXE$ RUN 52..
ii/i9/ei ^967 RUN :68 po 140-680$ TEMP 661 MA6H 042252 VFPS 253116 ROT 1 587 4 9 50 QRSF 75*00 y T10 T01 T02T03 - TO4 T os-TofiTol Tog To!
0 0 0 0 0 U 0 0 0 g TIS T20 T14 Tic rti Ti Tit Ti4 T13 T15 DATA . I AIA *IT COO& EULL SCALE SINaLE °SUPF - CRT Phal RM/Q I YM/Q Y/Q 1/4 D/Q PM/Q PNT ALPHA PSI .
«02 6.067 01! 5 7084 0 60900• 7.200 1 0003 w iO84 , 76 2.6-26 a I k - 4 ef; 6 5 #.02 2 : 0 2902, 0 3s033 7433 w i2$069 6*333 32 0'84 16i-tA5 4 7.28; 49647 .P4900 QtO2 ! t Q # ?..2 O - . 1 3 $- ^ 401,65 *169403 w163*56 6t80Q 4 w6 01 0--02 m 4#300 7*500 48*67 -^73*,86 - t svoe 4,02 7o3*7 5 0 m8,867 7,900 w177#0 -180 *,x`3 S-467 wJ88#42 Z- - - 9 Q C. — -5 6 — .! S 1 , 6 Lp_o ^O 0 c02 12 o 533 62x97 407*20 7 l - 11#99 OkO2 *170767 9. , 293 -d5690 x 68*21 P166t12 6, 0900 002 022#467 i00600- w205 o, 49 a 014001 w44 v*j60*28 71 , 0r0a 024 1 11*233 *26 t6l s567 9 wi4098 0 19••65 69067 pii57#71 002 6o867 10 *0001 7*233 o10895. 9 A153*51 l*tsz 54900 2400 0o02 7 .500 089*32 S1 10067 8 * 91 , o144o66 00 . 02 13,233 ie 4*02 7- 673 16 - 2-041 *J369 21 2, 917 067 "51,6 - 69 4',q 9 00 0 6001 GOB 16 , SoO67 -3 * , 06 -mi33*67 '59Q,73 7499 0-02 t8 * 900 84633 -32.0 28' .43 15 10oo2 ..,. 0,02 22 4 400 9#433 -i0 * , 59 5@400 - 1 0 0129050 5t*67 16 0367 -1 5966 '! 1 8 5 k 02 4 :12801 0,02 250840 ,10 9022 002 88a*53 5 t 5-00 .-2 0 9.21 -1,191,99 17 .13#99 110 833 28 x , w 33 v85 - i 1 7. 0 0499 0 0.02 29 . # .1j-67- 43 6-ilU 18 387 X3 -20*58 lm ^ I *o 9's 5 7 ofoz 18 a Q'i 26,167 46*580 ' 52927 40533 '03.3609 .
'+135. 13 • 63#33' 4 *381 20 9*99 0s-02 27#440 17.187 37w65 wi43o50 - 21 22 . 00 0o , 02 29.700 18 o 924 75962 447-Q 5*433 0 47*59 -148,,.94 24002 0x02 200993 85t44 2? 32#600 -SSo, 6Q •+147 2 3 -25001 01;02 0 433 433 22 *1:33 8 1 34 8 f71. 60347 •115 5. 42 . 24 0 . 02 7 . 3 33 0*00 02 6, 720 x109. a . 8 200 , 08 A-55 TFST 630 VOUGHT Lmj—,q - gE WIIND TUNNEL WIND :AXES f UN +53 1if15f8i Q907 aUN , 11 3 TEMP 690 Pa 141i6857 RM/Q
L,/Q Uq YM/Q
PNT ALPHA ; P S I v 0 o c 0. 4 2 'wavoo 3, 1 00 00 win . ok Al 79 • (I 31 P5& 158 *06 -3 SSI OvOZ 6i.267 3v, 6#567 37 *.9* 1.59,1.90 79500 • -4 * 133 164 , 082 45 * 96 m165••2* 0,1.02 -841,00 ' 7tQ73 7,833 w 178t24 0 •.02 422 ^ 9167 1 1 44347, w2006 0 17 6oQ33 10 0400 00O2 6#800 7#367 vm105v29 -1,55*75 15#;03 ;151 *06 li -85*-50 59800
10i37 -141*95
4,01, O.oO2 13 8 133 7s8QQ •66#2!; 50453 .12 457- 00,02 33 13 x - a 0 3i, • 00 16,103 3 049 q, 75, '4 30 ' 1 - - !Usis5 l i S*OQ, 0 .02 8.9 667 =2 $1 v4 3 0: 19ot67 ^9:93' ! 1 2 6 15: 3'1.0400 4t02 ' 22.233 9*361 w7t2O t wLt 3 7 -16t46 •123*,09 0e.02 25 0 867 0*51 16 11 99 109433 5*447 3j,30 5i880 -22c90 04.02 28 0 240 '!122t63 17 i3o99 1,1 •633 6 * 553 -33*99 -116e.34 18 16*01 0002 29#367 49 *.ln4 1'0327 11. 300 -280.86 48so0 0'02 js 6 0 G.: X126« 29 26.'367 4 'k .-30t 22 O L30951. 1 0•.,112 11 00 .
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*AX-ES WINO PO ,496857 TCMP' 63.@ .- . MACH Or2251 1580156 QPSF' 7500 VFPS 253+60 RNFT
105 106 101 .108 T 1)9 119
TOr 02 T03 X04 ' 0 0 0 0 32 0 0 0 0 0 `C2 o T18 T15 T11 12 T13 T15 T16 Til x Ti* a o 0 0 0 o 3E ;32 0 FU L SCALE DATA C3ATA AT con ^iNQLE SUPPORT DATA , RM/0 YM/Q Y / Q PSI FNT ALPHA D/Q PM/Q 1,/Q *8*39 0.10p. 2068 0.;02 8o-033 1 0•00 x+ s•+5.33 2.4.29 ^.8xig 2«6^ 0td33 2 0t,02 0 7.10 600 8+300 40 26 m t*99 x•:1.59` d.07 3 8@833 6098 0 4.01 0•02 .i4to i ..
1 163 . 6. x 4 267 w 1 @` 77 04. 02 +600 4 00 0 19 0 833 9 80122 MOC98 X1 @'92 r24o7*0 04700 5 '-7.99 0+:02 10*95 3 83452 . 8 +$4 1+.167 1+00 12.36 7 84@18 6 410.00 0+.02 x29.667 .
46:0,,30 Q*360 7 -12.011 0.02 w364iQ0 134833 98,•44 0«85 3#0 8 0002 1.5 867 10.01 00+2 t}' 014iso1 @@42E1 3 3 !1^^ i r"07 4001 0 ^^ MtA * 600 ' 16.9'81 119 x52.
9 000 9L402 t m2,, 40 3 X05 06.02 8.133 0 4127 10 0, 03 0 1#7 3 $ 24 436 -2425 2«29 04100 11 04:02 3@500 8.100 16@19 1:0 2'4 2 2 51 094 9 G3.^ K 1 2 0 00 04.02 7,800 8. 1 6 7 9 _ -2.16 13 6.0:3 0#402 2 84333 6976 *Q *03a ° 1 4567 . .
wool 14 0 * 6 1 67 1 4 8 , 0$ 00 2 « 8. 833 70, 4 1b 5'67 4
, 3
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.
WXNC):AXES PNT RM/Q ' YM/Q ALPHA PSI 1,/Q D/Q 'Y/Q PM/4 1 '0 6 S x33 ' o J3 4 -6402 00:02 r x I f, 6 8 -2Q9273 139067 09533 79.83 5 -8603 0•03 002 .25.500 10;00 14 0,E00 0033 84*92 6 -9*99 04,,02 -2 2 l- 9 67 i5 o6 OQ 1o,16 m v io- 33 1 61 ,33 83,117 0 0 _ Qr 0a 0 9 . 209,.$ 8, 67 2' • 0 ; a 36 ' 4 9 3 * r 0 o r r 6.r j r^ & ® '038 I WO l g ar i f ol J.n: _ _,44 i I S , ,5 f i 3:: r -4.7' 'r
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4°302 1: #967 X . 9'93 :80•' 0 t4 1 - 1 3 f 1 1 8:, 1 1 .0 51 6!5 49^'' 21. 2-2woo 0. Ac 0 2, 0 , .
'35, 24 . 56: 7 i 8,1' 133` 24000 430 0'5 '22 0 9. 0 Z 633 27 ! •360 09.62 . 2 1 "70961 0 !,k 4A 0 23 ' 2 5900 I i 0•2 46.09$ 28 1967 #. 65 SW' -Z 67 3 t, 79 24 -0001 04,0 2 - 1 9567 1 1 a Ok .A-5 8 OF QUALITY, POOR VaUQHI Lei SPFED wiN -T ^. i I ^TFgT 630 WXND AXES A AUN 56 9/ e^ o9n7 RUN .56 , TEMP 70# PH i4#,6857 t.BSP f 75WOO 9 MACH Or.225i 'VFP3 25490a RNFT 072614 - Tflt .T02 'f03 Tod S Q8 T06 T07 Tog Tog Ts0 ^_, o.
0 32 0 Q 0 0 0 0 Tit ri g T15 T20 g T13 Tik Ti5 T16 Ti7 Ti w SINGLE SURF O ORT DATA DATA AT I pATA ,FULL , CxD._ SCA LE FNT ALPHA P$.I Y/Q • RM/Q ' YM/Q D/Q PM/Q 1,/Q # f89$6 v,4 .a" 4•V1 1J M:V6 361 .. 1 ► aw48.
3 ► 98Q 52 1.3, 167 , , 2 :-O 0A"02 'Oi w9+.567 :1.241153 68.50, 1,173 twi4 -7'oF18 3 > 1 *3r99 0*02 ei6i,M i 92jtQ4^ 1#287 1 70 - •7 ► 83 4 x +6.03 Q1,02 oR22.233 1433 1 ► :59 •5.57 '139267 107.12 .-8000 2053 •4•, 83 "27.633 i4 ► 200 I 220 0 02 iiS•08 n 6 .9099 0 6. 02 2.04 -6,70 .
3 00 1 + i5.^ _Io6*27
3 20 is a 661 J,14 0
7 r7+
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s n 13093 0.:02 .42.687 4,.2i -10,50 1,S•887 108o'S7 1 000 •0r02 0 ,44#400_ P34,31.
9 •0 15000 19+86T 1.06y780 $ Q -^__ • r____ to 1 0000 0 02 *3.400 .867 e 1'67 -001 0-9 4V-99 11 91 67 i o•02
i1 2. 01 woOs
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15 12700 31 ►
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8 ,.._-.
1 16.0 06, 0 2 2.2l3(S ^9W39 i 3^b0 17 ► 547 2:^•8Q 15 p+:02 18«OQ .8,.40 i9 -5.17 33.4 •20'1033' -23..13 1,R 333 6 0° =20 ► "3.22 20 03 0.:02 •48..05 i-#1'67 36.600 22.413: 01002 -10 21.: 22 , 01 00,02 13 -i1_9 , 39.724 2*067 w*65win 0i767 — 22. 24,OQ 0,:02 wto,74 43e673 27.567 1+160 n12.56 0 76.48 23 ',25000 0f.02 -6wi6 46.393 "8402 500 +`9ei$ 29.433 1 .3 o 367 ..9•,53 24 o-00 0'i 0to2 U «04 11.967 1.133 51$27 O F FcGr] i u 9 c A-5 9 ' YOUGHT LOW WIND TUNN EL TEST 63Q SPEED WIND -AXES / Q ' YM/Q 'Y/Q RM D/Q PM / Q FNT ALPHA P SI L / Q 6 0001 4 •. .43P63 *733 S 7, 0i -7. a45 63 *93 ata.
1 „7"096 **I 3 .,w4 * OQ 002 .15.8—'67 .15 1e,39 -7934 1.
0#687 4 -6901 002 " 21 ' 4$2 "1 3 1 1 0+ 22 14,23 w8t , 73 OOS33 UoVS Q 0, 0 1 16 11 5 ,-B *01 -002, m m 1 * 533 2*,58 -11 •.84 OcCz 12069 6 9499 w3iti93 t m6 * 6 9 ej ^3 . , 0 67 a 37 3 13. e 1; 19•.13 7 *12001 0 o."O.2 t' 7,.
It 0 0 5t*,I" 0.02 `137 1 67 9: ' 4 4 5 - 7'_.^ -0 w25 0o633 -7 x90 - 43 * 66 10 -0001 0 •.Q2 .- m 2 s 867 89207 -0 W29 *10#80 09707 2,333 8 . 9167 33 *,94 11 2002 04;02 -0 050 -11.69 00,02 0970' . 1 2. 4006 76100 8v300 24slQ W2: •: "q q.
9 02 G x 63.3 12029 13 6#00 0 1 1 9933 8#567 19*22 .
'' -3*65 •12 . 12 900 . 08 . 33 1 1 F 8fQ'1 0 2 16 * 90000 .1,902- i L _1 -4t19 0:9k15 15. #02 29 # 700 9• '1O90C IL L -St14 --5-35 1 6, 12 0 2 10*733 18940 1 3 00, 02 25*700 -7* ; 03 -4986 00,02 1*667 11948 17 -14100 294807 121067 -3.95 2 .593 1 1 •'07 7*97 593 18 'l.5 *99 0 c02 32@393 '13 • , 700 -:7.58 -5-'22 169607 19 '17099 O's " , 0 2 12#100 - 41.x 0 2' 0 # 787.
Q4253 20#04 15*160 , •64i45.
20 0*02 36*,667 : .
33 93 --83 9- 41 -oe0.13 iv O'%76 -12+,24 3 9 1 8 21 • ' 21. 'S 002: -30,23 0+900 -10• " 11 :22 .23 * 99 OcOZ 449333 24.473 -96*14 -6 *, 74, .-10t - 52 26931.9 t 333 39 0•.02 '47 4 7 -103w42 23 Z4 m0 * 09 0#460 •7 •-50 431 , 95 24 0:00 00:02 _3f100 80300 A ^ i5 a p Op,alN ` Y ^IA^ I POOR Q -60 O TES T '630 VOUGHT LOW SPEEO WIND UNKEL WIND AXES RUN 64 ti/i9/g2 09,07 RUN 58 pa 1496660 T E MP 70• RM/Q ' YM /Q -PSI Y /Q PNT .ALPHA 'L/Q D/p PM/Q "22.87 w161.81 ^O*OQ • 69567 i ;0+000 -39400 8.767 48*35 309,63, L*16$e01_ : -9 4 Q'•00 800 , 67w72 = 6+413 2 :-2.OQ 9#067 36:995 0 164 V 10` 3 '*3.99. 66633 0000 015. 927 91480- '93 64 439.95 6#893 -,167961 0rJ0 4 - 6oOQ .229267 10+333 115.9i 500 1 w171 «75 5 . - 8.01 0w00 117o,48 70433 .,27x033 11•520 61•,95 4.09.97 0.00 89213 6 wiOfOQ .31.433 -120873 12*39 67k y 0,176,32 8 . SlB1.
9? 0 00 .37.3 7 14 1567 i20 9 45 7 •r 11 74'e31 '.169w00 S 0000 . %1695.33 132«35 7^o , 467 . .4•14,00 *043:,400 78697 -169«b4 Q OG .(36993 '79433 9 015000 '(7.673 _.
23w90 "1.62#,05 0900 89760 61527 1Q O•OQ -39500 48*74 16«69 0900 89733 69363 -15702 Root 2.267, 36.72 i1 -153.72 0.00 6.053 9984 :12 4.01 7,Q93 8 .767 27.13 3-08 0 - Ou 0148.73 6.00 9. p:00 9+767 13 11«433 19.82 -3997 *141,80
O't^00 5t76r7'
i5 753 9.3'67 .
14 7 9 99 E `21 44 .
- . 94 10 0 3y'•0 0.00 204,400 1G.167 29127 6tiOU 15 I<Qt01' -16.75 •133.57 16 :12.41 0.00 1,18100 21#23 6!00U 25•( 3 3 •23980 n .128e12 0+00 g 13966 6(•287 ` 17 •14. 00 299280 12 487 1234166 -31-90 v r @78 7!1 67 1.8 :i5•98 0.00 14.03 3' 10 31.437 -30045 vc131.31 -41«29 !01607 19 - 170 99 000 32 **07 . 407 '1.7 -33161 .1.35.40 O•OQ 66*38 49800: 20.20.00 36.120 19.547 • 495OO -38096 •1484'02 21: 122,0.1: 0.00 22-100 -849;16 39,893 5.963 - 9*-34 99.00 4 im150e37 22 24901 43.780 25.033 M101p,,,83 6 0 767 - 561, 35 0153,:18 23 25.00 26.800 -1Q9917 0.00 46.927 69333 23017 ++ 161 .01 .24 0.00 0.00 -3.667 898-00 47' • 39 caEmAL^aC 6 (OF POIG71, QPSF : 75.00 t r MACH YFPS; 854 25 7x5b x'.253 RNFT T01 TQ- To? , TOS T.05 t 02 t'03 T04 f05 T 0 „ 0 0 0 59 0 0 0, 0 0 x'13 711 T12 T14 TS5 T16 'f18 T15 T20 Ti7 0 '32 '32 0 0 i 0 0 0 9IN61 E :SUPPORT ,DA: , rA rlA1A 'AT C .h :,FLiLL SOAC_S OA.rA: RM/Q FBI Y/Q YM/Q FM/Q FNT ALPHA d/4 L/Q 1:'S ► 63 •.135k99 56 ^ 6 ► 0:3:x; 2 +r2+01' t ► 36-#36 3 .x4,02 Er 3.47 # m 14,4 66 4 -6,01 0o, 00 "22.367 13o833 11 61433 37c,86 -1489-20 ► 46 s25 ,~ 151 5 - 8.03 0 100 m28 # 233 14#800 6#787 ► 139 j2i 1,94 6 -i0.02 0 # 00 132,167 1.6.067 1 l 6.'77 7 •^ 12 .•' 0 3 7 13"27': 60•"67 X55.4*gib 6(a 73.
8' +•1.^F^0^ ^4i,7'33 't3 ► 327 ' 6195,1;:: S,: 7b 9 45447 '6 ► 767`:.` xQ"•76 `,.151'•9( 18«75 10 0002 0#0'0 ++34333 599U0 124400 54#73 ► +141,07 00,00 11 2,17 2.300 45•.86 5#767 12:74 -1369-63 124467 12 4.03 0.00 5 953 3 Si21 WI 5.46 6.733 120509_ 38.44 13' 6 , 07 40 ='32199Sr7tiG 2.r2$' 6133°41^F 1113'00 12#733 14 B.Q' R<OG. *3165; ::1513` n 53.19 100. 23133 :316:7' ' m^j0, Q3" K5.340,96 S5 " ":.9.97 13: 00 ► .6126:'7 1.S.l 67 43 800 34s:55 ,16 250133 .t133e,28 .12001 00.00 '140800 69247 -15«75 34,04 "14 0,00 17 #01 29+473 15 ► 900 27033 60433 - ' 6 7 2 20 , -129071 18 15.98 0#00 0 31009 0 525.67 32.027 17,42.7 26."14 7!333 ► 0'+Ott S9 i8 Ctt? . Ei+2^?E) -31"t41;'^i3(3...93 32 ► ^E60 '20t2€?0. «6139' 19.99 0',04 1490'3 -3487 20 . 35 ► 822 S: •L67!' "^37 22 ► 553 SC1 ik 92 +* IFS;.
'22. ► a Q,+-OA. 2+4o 5 # 8,33: 4.0 21F . 33 x9 ' 93 6 93 -66 IS 4 •x, ( yk :22 •24403 0,00 43.853 6#933 -51w39 0159007 27#933 N 80969 23. •25.00 , 00 -58*66 011 29,500 -88,50 71833 ,161*,45 46.353 24 -0401 0.00 5,873 19.09 -4.067 12,533 56+97 •i39.97 tirj r.Y ud OR 0,UALITY OF Fo, A-62 _ y YQUGHT Low SPEED WIND TUNNEL TEST 630 WIND .AXES RM/Q YM/Q -PSI Y /W ' PNT .ALPHA 'D/Q PM/Q L+/Q 3;8.714 •ti36a59 •• 12.667 53.3$ 5433 ^QiO'2 0x00 3.!633 ^1 0 2:5•.21 W,1..19' ^*•0!1 64073 2 : •• 0.00' 46 5,.833 ' 00 70488 is#8 _.
3Oo73: n142^60 3 0 0.00' _ 93.83 if a3 3 016.267 '131267 37••90 92 4 -6.01 0.00. 109x09 6!267 -143 0' m22.333 ? 13.840 ..
x150 co$ .8, O # 0 60767 46.,63 5 a 0 .27.867 8 00 14.833 1,0 # 7 53#,46 .. 7,5 -158.31 6 0 -9#97 0#00 M32,040 16.167 1, 60*73 X 1:59 59 ` 79513 +.12•00 0*0fl 0'37 420 1797.80 10^bctl5 6.853 67R0r_ X1.51.81_ 0•fl0 19.3'60 ' Si4^0:Y ,.42.133 `. i0^`+.°E7 a147 8i70^ 70477 9 '01.15#i}0 0 009 500 $Q.553 SQ5*^4 ••44 ► «zk _..,_, 19x19 59867 -137.64 . 10 0.00 0 * 0 0 -3#900 .12.667 53#57 12092 wgi32•,85 00 , 1.767 54707 11 16 9 9 00 .12#667 44691 130..58 0900 35.98 7x72' .12 4.00 6,800 12.667 5+600 3.••48 0.00 3Q :99 al 6. ++139.72 13 3.99 11,033 32.,0 , 83.3.
-3«6.9 ^ w 67 0.00 *I 5,,!S * , 5•800 13l.
14 B.OQ 13.280 3IN87 ' 1.3 .9099 OwOo 19.593 .'13.9" 0 32:67' 15 6- ar l , 8 ; • •15F54 691J0 129 38 :12.02 O o OO 25.300 14033 31#97 6#367 -22 #.42 o 0.00 294493 # 1'27 25,,28 i127 •,59 17 1:4.01, 16 0 299: 22 --q 12 2 o 43 7 • h 7 18 16 01 OOi 0.00 32 .1.73 '17 .767 23.56 r,126.°62 X30.:1.8 '5 # 887 19 18.00 0 • '00 ' 32 * P-67 20.• °. 27 2r 39 x: 5.567314 &3 413(J•8$ .•46w39 20 -20.01 Q•OQ 35,833 '.22x567 ,_ -38•,75 .1. 41 • 0 *00 5.733 0 21. ;22 4.01 40.273 25 #300 so4 r2 -48 #,69 6#7oo •+151#'!,3 22. •240102 O.00 43P820 28.233 -87+97 -560-34 0155+41 7 25x01 0•, 00 29.780 m96.2Q 74500 23 46.307 18«83 ^00136.60 5.733 24 "0.02 0.00 w3.733 12.700 520. 24 A-63 .- ^^,—,_VJUGHT Lew _Sng g,_W WXND:AXES R.
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T9MP 70# MACH Ov2253 QPSF 75*00 WPS 554025 RNFT 1570 6 t q ► 09 Tug-TIC 10i rO2 T,03 T0 TQS Tag TO 0 0 Q 59 0 0 0 0 0 3 T14 T15 T16 Til Tla T15 TZO TIT T12 T i 0 0 0 4 a - -32-.'.32 0 E DAT&-- DATA I "I IN . aLf,'SUPPORT I , . DATA 'Al C a G a 'Y/Q RM/Q YM/Q PNT A!,-PHA D/Q FM/Q PSI I •148 «76 I -Ooot 0#00 .12 * 667 53*73 6*267 21 r5* •30600 2 :02:•01 , 29o,31 12#933 71,t14 6 520 ^1.w65 QsOO 10 riO ...
6*760 35-69 " U4 *64 3 4 .00 OwOO "16. 467 S&ZA 69867 4 2+5 1 wt$G is,24
* *5459 0a00. #967
-2 1:36833 1080,86 5 85 0r :,,46 0,18 5 00001 79233 Q s OO m27#800 i4 800 119939 59•,36 iqi69972 6 wiOaOO OaOO m 3 . 2 4 . 2 6 7 16*200 1 13.33 8•ioo 0,64 . 890 00 67•34 7 12 0 0 0 -170 0 00 w37k . 347 0*867 4Q5072 73*5i -159.70 S "11099 0.00. * 42. 233 1.06 7x 4 61 0 # 533 «Q9 7 6 * 8 k. , x i 158 15 is,00, 0000 20#600 10 6 -* 4- q - 7*167 3 •44 * 66 0 Zi o.'62 0000 12;667 53954 &a2 0 n 147991.
10 000 - o 3%600 OOOQ 6.167 11 2402 eo167 1.2e633 1 50 - 1 9 w145v24 4 1 , , 47 •: #93 1,0 +'22 0140 5.967 12 4*01 0'#00 6#900 _-LZ— o 3 5 **,39 ial 40;# 80 3.1 6 , 0000 13 6#01 0,00 11, ,233 .12•833 954 final 0000 15.867 13 * 333 32 6 4 267 •,32 wi40967 14 io 048 1014 fia 6. 533 VS L0 6 00 0 a , 'O 0 2 0 - a V 6 7 1 4 940: 33,42 -15928 *137t , 6*600 04 16 124O2 0*00 e5o367 15*000 311;63 61633 -22#87 -133.18 17 14#01 29*7 7 16-193 25075 00 00 00,00 3 2#040 17*633 6 , 3 2•267 -31*00 ^l 2 8 *. i iS 16#03 22±.
-30 io,,03 W133 .62 32 # 633 20*333 6 1 113 19 17 9.9 0-00 -25 *19 6oC67 w 3416* w144*29 20 20402 0*00 36.667 22#907 P52s41 $.o -39i57 , ' 4 ;22,_ 0s, 00 150 1 7 21 02 409213 2t a 1 67 o l i t 34 6 i x2 60880 -49 4 *16 ZZ ^ 24 f 0 1 0#00 J +4,000 28#233 -88#43 I't71 -58-64 :79 25 01 0900 46 #1667 74960 - 1 61 9 es 29.933 -9509 6' * 233 21 9 , 56 -m148,36 24 0#00 0o-00 -8sS33 6 6 6 7 53. 12, 12 .
[12
YPUGHT Law SP.E.E.D - . - kl N.EL- -T-E-S T.
WXNO AXE$ 1 PC 1**6660 T E MP 74# QPSF 33v00 VFPS 268 # *7 MACH Osk2370 RNFT 1637 5 8$ t T02 T , 03 T04, TOS ,- TO 12 T13 Ti4 Tl$ Til Tl$ Tl$ TZO T T16 T PATH T A 'k t COC A 31NOLL S OP OR FNT ALPHA RM/Q PSI PM/Q Y/w yfl1`4 4/Q O/Q i o p ot 0+.02 - 3 0645 1.8 .620 20080 01*7979 $4*33 6#235 2 0*0': -241 2 .1°39 22•2 4354, 15 -3,o675 x:2 0470' 56 x02 - -4*00 -2 105 095 - W igo!J^- 3 , 0.0 1 A2#530 5609t, 20,04 8 4 # Q78 Z5 00 5 *101*04 U 49 w7 21%.42 -76.#03 44167 q 11#747 04434 ,.4Z 6 0461 -10#00 wii687 17 * 06, -- * 3
7' n7 #.A-S wi6i5Q6 3 5
_1 4 "1 #928 12*60 W1;9#18 7 000, + x. -124,02 0 , 1 8 1 003i 26#27 -21 8 Q * Qt 0 13 * 99 "Z6 #323 10 *79 0 1 26 10325 460$88 . 18 f , 74 9 0 * 01 -16 * 00 lo A4 lOwSO 2.361 18.976 146 4 5#71 _ 0 ' 0 18 00 x3&•386 0001 702 10 0 .52 77 3 0$4, 21*23$ 0,72 I Oot 0 19*99 9*71 91151 23 4$61 *4*95 *41105* -220,03 .
i h L 0461 _7e36 _i_a 3 4 7#440 27 048 - w2i#)AI .Q- l- # i n so 13 0 9 0 1, -j? 3 * 9 9 3v10 'AJ66#03 9-608 30. m 38f49 - . . 0873 - 0 26900 1# 0 1 #01 11#4 1 + 6 33*706 -45f87 w 55 v, 41 ,6 601 '17$444 1,5 0.01 -28#00 13 # 3 , 98 5^ 9 9 50^03 37 4 0 1 8 as 5 f 5A- a - t '1 *53t Ictle I sp- 16 Q # 01 03 00 , 00 140.066 40#313 6 1 *63#^Sl 0400 *3470 0#01 17 6 51 53;67 6 18 , 6 ^ 4 36 5 200,49 W i494,19 0 *0 1 8 1 • 5 18 5 4 7, r 7.9 w 1 ; + 3 i, ,7 6 201 0 1 w 3saSS Il 771 o 8 50 5 I 1 9 0*01 4401 -3 * 886 1,3 -@ t, 33 9932 47 q 23 `,12 190.9 - A15 , 6*70 20 0001 5 •, 99 -3,0253 434675 - 370 , 1 t 633 27*,23 w19154,49 23 7 21 0.01, 8*01 02 0 *40 , 2 , #x•42 6 0 ', , 3 9 - 2 1 1 0 4 14.3iq t88 . 5 a3 , 3 3 , 22 Q4 0,1. 10 0. 0 -i x.386 J$#21.j 25 q $34 t2.1 *230, 6 44#'#32 2$ 0 4, 01 izo . 00 3 4 it3a 'R Z4 9 X3 "00331 16#265 otei :$o 0 ial 24 04 14*00 01 06994 17(,651 -iioaS 33,3,74 350,07 199398 .25. 24 391$10 , 25 O*01 16 0 02 2 * 681 34, 0 2 w2,99e k 7 96 0601 18000 3 30,765 -34#09 44080 66.4 w320 2.1 #476 k76 1 27 0 * 01 20+,02' 0 1 2 0 240020 -49 SQq564_,39*13 36 _ 5''' 2 8 000 . 2240 1, 5tx v'4 6 b 43• , 09 . *398.05 3 7 27 w $3i$i 6#8 #036 240, 00, 2- 4 0601 43 !17 8#7 05 30*181 -66#05 605 , 94 l4al ,79 so 0.01 26*00 912il w _ 4 8 #, 5 1 34 • 669 " 31 O-Oj 28 * 00 10,.343 -49 t j2 7-66 *38 , ,Jo , 64 38#402 66017 30q01• 69v675 0 3#115 0001, i001.8 49a380 -43*69, -73$2* J,2 33 OoOl , Oo, , 00 .
-3 * 645 I2,590 S#Z,! 5 3 22,t 63 t - J ,4 I w 3 ^2 53. 81 A-65 vaUQHT Lmw appE q wiND TuNpjrL Tp-ovt,68o WIND .AXES PO. 1*t6709 TEMP ' 75, /Q RM/Q YM/Q KIT ALPHA PSI D/Q PM/0 'Y/Q Qlkot v o 3 s o 1,4 4. V. 45 1 0.0Q 7*4 -2 ,02 -3 1524 12.r620 58.#13, 867 *1 , 34#37 A 0 i0o 2 4 *-Q2 0*36404 ' 20 i 163 1 1#31, 12.6 56. 15 &VIA068 4 0 # 0 5* 9. 9 1;93 12o$61 200,97 -1020,5.1, -3 , 52 0, 26 -64747 0*01 "7#97 -2o68i mvi 1 * 77 19901 ' Rd 7 5.30 13 6 I f 5 2 464, 74 7 6 0#0i -10401 WiA476 •14o367 37vJ2 w16#837 15*94 —46o27 .
i - 12, *03 1;20 lsl l i 1,1 +86 1 0, 602 25.6 w42 q 289 - 16t - 24 .
aJ^ 51 91 , 7* 6 22# #01 0.27 # Olt 9 9 1 7 v , 22 U9247 A k St, w32', v Iff 9 51 47.1i LO 0#03 -iS000 8#99 7q61 80•36 34,976 21#524 "36071 4#516 9o46 .il 0o07-020,04 2ko217 109t1E -Oo87 0441#560 12, " -0401 M ae 03 •f i Q^ 37#259 wl9o94 04 0 5#67 1 + 13 O.OQ 24002 9+3!01 3O#502 -340 2 0401 .
-2s«98 11 175. 33 * 916 45 19 P, 55 1 873 39 , 94. A82#79 7 ., 91 V22 12 1.93 37 337 *5 4 3', 159. 0 49 21 16 1OW25 1 ,50 OsOl m 2909 -14*337 40o81.3 m53*98 m 463 q 361 59 6., 17 0 . 01 - 19*75 - 14 1 :i2 M831 6129' 6 Q# - O l -3o72 3 831 54988 18 0#01 2001 -3.765 0- 9 5 52.57' 3*639 7 .:12 -148•x8 19, 00. 01 155 9 - 05 **03, 0 3 * 494 13t253 45#65 13 #44S 19i37 20, 0 * 01 5499 17, .00 7`,74 .,", 1 # 133. 15: #6 2 X 19' i' v 91 - 33 37 4.
8 «02' #:08'
21, Q#Qi ag 2 4 7u 31 - 2 w60
02-2i :22 0f01. 10000 -11054 154,21.1 320,03 -221*87 109,53 •250402 .23 0-01 12# , 00 0.120 16#30 33t8l -2.45042 -1#89 29070 24 OaOj 14t00 34,53 271,15 1#6 7 '17 * a31 -12w2O 34 4 .79 ,E .
25 01.01 35.:56, 2 96 * ji 6 t 0 102. 1 , 91518 ' - 026 # 71. 35- .898 26. 17 o 99, sS tj * 365 0 0 -44:1x48 374,12 *!3 17 •,38 4.295 -3.4w70 '27 OoQZ 19*99 5,663 6, 6 3 -4iq97 1 4 0 - q,'O 7, ; m, 356* 1 26 50*S3 A• 4 28 0802. 22t00 264,988 -52#96 559873 43-25 -3944,76 70018 29 0402. 2, ; " 99 8P825 30 * 030 -67t,64 60Y723 44t;aS 0416928 30 0s02 26#01 9o337 34 a sBj 6.1 12*99 6a,s_ w* 6 • • 958 -361 w08 8o , 66: •43810 52 11 O&OZ 28 0,02 4.0-51Z, 38.,524 49. 0g 66 f *!$4, "39 0 * 02 30002 10- 4 , 139 -2940 -379..03 42, P 2'65 -42v-50 69,789 '33 -0, 01 x4 -9S 0*00 -2#926- 1Ei771 *,75 5v6 , 93 219,, 66, w l OF POOR QUALffy.
-- VegjHLLmw 3P 2nwIND TUNNEL Tr-rT_Aao WXND AXES ji/,19/81 0907 RUN .64 ^,."u .
I?d. l*t6955 Temp 50 4 QPSF' 7 MACH 0v2251 5# 00 VFPS 245•1.6 RNFT I65025 q T01 T02 T0, :4 104- TOE YQ& T01 TQS TIG a 0 48 0 0 0, 0 0 0 1`I8 T15 T20 Tit Ti2 T13 Ti* TIS T16 III 0 . 0 32 '32 0 0 1- 0 0 SINGLE iSUPPORT QAyA BAT A -Am FU co G is, 0 A T A PNT ALPHA RM/Q YM/Q PSI Q/Q Pm/Q Y/Q I./Q n 1 0*00 041 , 4a033 '12#767 55#,72 6 1 2U Q F100:82 -1*6*49 129600 57 39 1tS'-6,7 22x71 0135813 2 0 , 00 02 *04 -4906 1 7 3 0900 - 0 4*0* - 4 , r , 33 22 # 45 -!IJ8* , 26- , 12#600 57st0 *i m 2*361 44 0. 00 0050, 99 -3,600 12#900 SifO2 -+ 79100 228,80 - R i0i *,13 5 167 wq 11 4 600 0o00 --7,-98 13#400 45828 20*^ 3 3 '-74 #63 -3#167 6 16#,26 0f00- --9099 w2 * 163 14*36Z 36138 w16*667 -47673 W 9 ,8 99 7 0#00 0 11 ; ' 06767 15 o 533. t 021093: 3 120 , -19. 11.
1 7 2 G1 7 li&68 0000 0 1,3099 j9 s 51 4 8 0*609 17oi67 27t067 14.05 2 , 4661, - x,94 1;00 15098 031 , , 10•,36 ! AAAA-^-- -17 19 -0#Qi, •,99 34533 21#353 9v79 1,0 •;13 ss36 q 700 79#03 4*367 11 lo odoe W 20 0, 03 w103 m4it%3 9oQl -iio,7l, . 20 , 100 '12 "0#02. -21 . 99 64,40 :134040 6..67 '27 + 267 *17 o , 82 -46 #600 13 .'- 23v99 - -,14:q 59• *51 q *,*o 2m,73 -OPOZ 8,60O 30.640 , 1. 61 & 8 6 qo o c t96 a *83 .183 1* -0*02 '-26 r00 1+ , m o 56 9 093 'l 10,767 :;-28t01 4 A-96. 1153*68 15 -0002 -13 4, 67 37*709 -56 .-49 •60*263, .
109,56 Z03045 9 16 w ovoz "30401, *6398163 14#227 *1@093 w 5it-75 0@02 0801 '17 w -4o167 90 0 6#567 19*3* "147464 . 12# 56#. 03 -0-02 17#19 m K I 43 i, 1 5 is 2*03 -4,200 1g#967 6'3@9'2 ' 39867 19 -0902 4*00 w3 * 933 1 9#17 26T' 4508 , 13 66Q -160*50 1 13 # 0002. 6'.,01 20 ► -30233 '17 933 27#'65 •196,56 43-767 36# 54 21. -0-0 1 0 2 8000 -14*467 . 45 45 2 1 800, 3 1 43 -2.1.1464 62. 243 321+83 - ^ 22 "0902 10# , 00 -i t 233 9%26 259933 15O280 226*,25 23 "0002, ilo,98 33.89 09067' 16o*00 30t267 *247o63 w205 •24 -0402 13#.98 1o460 17,800 m15#37 34*913 36917 02738,98 --0402 16401 40#26 36* , 58 "302*42 2*900 19*600 o 27r89 7 26 -0*02 18*01 4.167 21*667 -36#8 !4 '451 1,;0:0 38s67 *324w65 V -0902 2090I 'W363 F83 5.400 240267 - 4 39,02 5 G #, 8: OU 41*21- 28 -0002 21999 56 , 6067 '27 t2'0 0 -54#64 1267 438.81 -400-66 29 0 0902 2*000 9903 309300 m - 68 * 43 61v100 45*08 -418-31 30 ► 3002 2680,1 j0o633 339567 -81 si s o 66 q-3oo 47037 -*43952 31 -0*02 27 s 99 10 & 1+33 38*6153 -49, 1 35 674080 8 v 37, 4 379 •.6 4.
29999 32 -0#02 10 8 087 69tS - 00 0#85` 0375,51 + 42 # 107 a *1452 33 0*01 0*00 . -3.467 12,787 204k56 -146092 614097 '55-133 A-67 YOUGHT Lt)d -- SeFEQ Wlha TUNNEL WINO 'AXES -1.2 R U N IS RUN 65 Pd. 1*o6955 TEMP 62, OP MACH 0•.2251 F: 75*00 RNFT 'VFPS 25Z 07 1603 6914, T104 T TIQ Toi T02 T0 1 3 To, TIOS.... ' Tag 0 0 0 0 0 59 0 0 0 0 T29 %7 Tia TIV Tit T14 TIS T16 T12 T i S 0 3 2 !32 0 0 SCALF, PATA.
EYA-TA 'AT C FL LL - suppakr CA T.
Rm/Q YM/Q Y/Q PNT D/Q PM/`Q ALPHA P S1 L/Q 1 12:0 . tot o ♦ loo 540,68 i 0"•01 , "3 4 700 12 0 8 3 3, 6 2 .
" 0*00 "10.:033 7Vij 73 28 w63 0146465 2 . - 4 20 - 00 '13#033 .
9 , 5 * , 26 6*520 34 •:92. 0 151:67 `"3 w98J 0 0 6 367 2*400 : 43cQ3 •x,15'3 •-53 6t62 , 0 0 •: 00 0 mae 533 . 149067 4 -6*01 111,02 6 # 853 50#61 •4157•,49 5 "8601 1427.633 OvOO 14#833 119#•74 71600 58 .w39 wJ68@76 OsOO w32m067 16s313 - 114#73 6 010601 7,.: t. 5 1 4 , 0, 143 66 * '^ 5 m79 413;, 17.367 08 #74.
7 *12%01- 0 : 00, *37• .
i l . 57W73 71;«'76 71063 1^ 667 41 96 67 : i9 s *67 - . 101 Sk, hg 5 . 7' 11 7 J049 t33 19. 539 i 1 , 0 0 r 0 ai #,66 -144-.23 6#053 0.00 120867 54t1B 10 0 lo ' O 0 -3#767 1 x,56 ft14i,,08 5053 1 0.00 1 1833 12,733 45t58 11 2002 *;60 w 13 8 s, 8 . 9.
5i,647 4002 0000 6 1- 9^0 _ 12 - v 7 1 7 - 3 6 s i q .
3493, "1,40*;38 r5 7 Z7, , 13 6,03 0,9 1 1 00 10*967 i2w933 30*1,89 *65 00.00 J. ff , 30 - 0 13.367 : a • ot '300 80 6 1 1.
.
75 wL4 2 ci ^ Q 6, 4^2L w 9 i5 0 woo 3Z460 10* 149967 6#267 *15*46 *135,89 1.1#99 owoo 250100 32t31 6#893 0 2*0, 26 m134#51 16#367 , 04 44,01 259 17 OoOO 29#740 -329,66 t ! i28s93 18 i6co1 0,00 32 . 9 4 7 '17P68 ? 4 3-7- 3 -- 3, o o : ,-3 -132 #9S .18•01 33 9 J40 ^w23 ,t 0-'V00 10 g 153 67 0173 *138*97 ' ;22#700 4 20 1 10 '03- 0 *0-0- 366207: -40&:99 •j48c64 5,853 0000 '39 * 900 25.333 - '-73#38 zi :21,•199 1452,,58 28 t 400 . 43 6053 m , 157o73 a90 # '22 -2*401 0,00 43#653 -!59o; 95 o•161937 1438o,*9 70687' 25o01 46 * 660 30,000 , 23 0400 -6#029 21.68 -145«64 55 * 66 24 0600 0#00 -3v8OO 12-833
FooR
OF VaUGHT LBW SREED WIND TUNNEL TFqT,-klO_ WIND AXES 66 -- RUN RON . 66 F5 146,6955 TEMP 64# PM/Q ` YM/Q Y 3 Q FNfi .ALPHA -PSI D/Q PMIQ L/O 189,85 -135.59 1 0000 ^ 597 .0.00 ,.3.733 12#867 55168 13
E5 9 , 66 *13'717'7
O.tOQ , = 54880
2 .-2oC O wt0000 13#060 73* o* W14 0.,9- 31.96 A3. 6.1do 31 0 * 00 mi6*733 96t -4*00 38#65 6f193 -142.91 O#.00 4 - 6 400 K22#467 1441-33 111#81
^._
5 •.145, 03
.448 , OQ 6t- r-13 46. p8
"27,800 14.967 119 # 94
, vi155.95 53147 6 -9499 0400 -32#273 16+333 113456 7 # 242 .
._ - k 611k8i -154+23 O^O
' 7 12^^^^ q .37.567 1T•967 1;08#24 7^fiO47
^i , 66 #58 -14 8 #67 6#
• . 63 •'87 68E7
8 ► 1.3.99 0*00 *42*097' 19 3 Q3 70w 14476 6#313 0#OQ - 44. _93 200400 105'#a .15#Q1 18«76 5#680 X135#159
10 0001 0 0, 00 - 3#900 .12.900 54189
, 90
5#4V 129 n 132.75
1499 olloo
.11 1»567 .12#780 469 27
5.347 7«84 -X129.41 .12 4 401 6.567 12#767 36#62 1.*.56 *131.71
; . 31 .5 4
6, , 00 Oe00 413
13 11#OOQ.'' 13.033 #8 2
Se 04 -:4«b3 . -Oe00 5.7y? •9130.6:9 1.4 139313 3227 15#500 .- X 11.20 X134422 Oo,00 32#87 .8Q' !15 '10#4O 19.90 44.120 -169.46 6*igO -131429 0.00 25#033 15#067 32#.38 16 :i2#01 -224,98 X1.27#'83 000 64327 '17 ;1,3#99 23,627 16#333 25#:22 -32#:42 wi24#11 0#.00 17.673 7#113 18 16#00 314900 23#1©
• 33#57^ ±127F3.4
0.00 ;20#547 24,70 '6rt0.0
.19. 17.99 33#180 w
-34x14 -131:-88
20 ^19r.9$ 0*.00' 35 5 -224713 A5345. _ 5 4 680
#873 T -39*42
-141 .61
0:00 25,440 5.780
2t X 22#00 39,920 -72ro2
-48,65 :150439 - .23#99 0900 28.080 -86#:65 6.247 .22 43#460
*153#02
#00 7#280 "57 . 1,1
23 24#99 0 29#980 -9504
46#673 60613 l8o77 -136.10 0#00 55.72 24 0401 -3.800 12-867 a i e
c c.'rw1CaL`u?
A-69 L& 1REED NO TUNNEL TEST _`63o -YOUGiHT.
S
WINO .AXE TEMP 654 Pb 1?M+,6955 RM/Q YM/Q PSI L/Q p/Q PM/Q Y/Q PNT ALPHA 18,94* '> 5x i oti35o64 1 Q•01. t8•7 0.00 *x10.400 114367 50t;78 26i57 , *+138:• 41, * t14 X 900 5 0'* G, 1 76x.20 . r 747 1.1, # 767 3:(b' 33 ► 04fa1 .18 433 ' 12°^5'3 14^6r^f^ ^e. ko 0 3 6 4 5,13 41 *.21, "149:89 :"5.99 0:01 m22.000 x,.3. 000 132 •:55 48«64 "153 23 5 0401 64763 ' -8.01 P24:700 134767 1$6.63 55.24 6.527 "156*i5 6 r10*02 0.01 w25s207 15.033 133.E 60••.52 vil2061 **26.767 b•1r33 "*152466 7 02 0 01 47 `132V.49 . r 64%58- -147•:52 0401' .28*233 17x' 67 6:247 8 •i4 *00 129*82 '131 a4 1 6.067 67 *99 *143*,58
9 •l4.99 . 0.01 x29 r . o73 17v233
8 7 18• • -0.01 0.01 54367 -mi34*52 10 w10+433 4333 50 :28 75 4si32416 11. 2.02 0*01 "6.700 25*,38 54333 12 « 11.009 7*61 wA13Qc28 12 - 4 4 04 0401 x+ 3.233 i0 -zoo 4 •,'3 8_ 5.133 1.90 01301.21 5s0t30.
13 6.02 0.io1, 0'.000 10 567 "15 97 "13$ 85 2x94 401 : 5:1;.33 14 8.00.' : 0 3.&00 10+567 -39. 74 ;: •8.06 a(, !
15 10000 0.O 2*6t O 10.567 ^68956 5.4070 "1.2x.92 ++1,35#:95 16. , 5!367 -- :12400 0•.01 1,1.233 .11.100 "940 42 -17497 "1354% •14401, 04L01 5.467 '17. 14:233 -12+000 w 107+14 w 7 -23 *81 38*22
p 0401 16,200 l2o967 w109 9, 0 3 54 46
18 16 0 , ; X28*d5 ► 4401 5.580 -141 63 19 S!!•02 14+167 w109f10 18.133 .
.. .
"314:8& 'Ki34*86 20. 0401 •15*267 4.6!73 20.x,03 1,9#567 ^108x32
X36.55
4.547 "132 0 40
21` 21 *99' 0#,O1 243.800 16.467 •i t 77
22. 02 0•.01 mi0ic95 44340 •!125x07 •24 ► 22*033 17.767 0401 44567 X126040 23 :254432 1.8.840 =105.74 23x167 io 34*38 0401 wJ0,367 J1940Q 50,47 5067 2.4 0.00 i A-•o .
PC 14t6955 TEMP RM/Q ' YM/Q Y/W FNT -ALPHA L/Q PM/Q P S I vg134lk.34, 0 02 11#205 w o ..Oot wia* 500. :: 5 56Q 260'..
OR - 3 . , , Oooa Zit I - 4 9.02 UiIZ5 :4^a54.
61260 42050 -148 4 w 5o99 0•-02 w21,975 12s800 133.,63 +•45 5 0 800Q 13o.02 w246200 13*675 143619 6- 5 20 4 9t1 * "154418 55 *66 -1 5 3o gi 6 -9699 0t. ' 02 o2 5, 0 80 14 o 8Z 5 i27 o,3 .6 6451 5
1 5 0 *50
77. , 9'145 5 01 6 5 ' 1 X13508 1?133r0a " 5 0 1 a 12.:30 j a L '# . :2 6L g 5L 4:9 00 0 l k o! _ , -64600 7* , 48 i m! 1296,34 10 4900 06.02 -3o325 10@625 6,07 4 0525 08,02 0#125 46776 w130697 it 50- 9 9 10*450 -16611 mKI 33. 7 8 00102 5.0 -2 il, 76 12 7*97 3.425 1 0 * 475 1 0 m 37 ,, 1 3 •7 +1136415* *J;a6 l. 2. 8 3, 0±02 21.4Q0 X91 11.00 : S., jg t , : 0 : 40 I t 0jop- 1 2: 3^ Q 0, m4i.35 15 . 50 t as J6 30 • r A U A-71 OF pC'M -.1iHb TLl NoEI_ _ YiOUGHT Lmw sEo LL WXND.AX5$ RUN 69 Fm 14#6955 TEMP 75#
1554637• MACH 04225I
aiiol q QPSF' 75P , 00 VFPS RNFT -l os 106 T01 log Tio IPA^ T 04 .-ToaL.7 3 0 0 0. 0 59 0 0 0 0 T11 'tie TO 7 . 18 T15 T20 ' T . 14 T16 T16 T o o P?fJR,T $-';ALE QATA Rm/Q I Ym/Q Y/6 ALPHA PSX Fm/Q FNT L/Q D/Q 1.8w80 0132*34 I i-0001 0 9; 00 w3 * 700 12 * 833 56s 86 5*380 5 0 6 , 47 ' 26 wOO o'134*75 2 :-2.09 , 00 -9#661 13#033 74 ► 24 0s Z0733-- , ' @,17 *113806 3 — 4*01 9*00 m16 s 067.. 67 g kikQ 5,747 4 -46000 0*00 " 21#867 i 4s000 110867 5o993 44t70 -8140- P ,36 5 *8 * 00 O c OO wZ76467 14o867 119.25 01 _ 614,93 53 6 01 -m192+ 6 w10sO2 0000 v3i#733 16 * 247 1i$s70 58i67 6o333 44148,173 7 *12#01 -0*00 w369 g33 'Y7.993 101s53 ^i5.37r 5 687 X142.53 w4io253 19 * 493 ' 1 03994 13. -1*0,32 103o74 1016002 99100 445,627 21 52 133495 19*86 o q 56o50 5073 1.0 w0-002. m 3o633 12.800 13 q,22 5t193 .,04 2067 47.68 * 131 ji ZOOR ocoo .12#767 w 806 8 29418 01 13,
0, 1 00
.12 4-01 .
3w65 o i? - 9 q 74 b+ 34•37 0:1, 04, 00 1,1 , o*67 2 2*900 5 * ' ?- Q 0 -3 p 08 6.0 8 *75 1* 8602 0.00 l5o633 ' , 13o300 34,13 &1IZ 35.59 61 9967,-- _^_ -09#40 I O U1,58- 10,400 "i3. 3 3 15 io- l Qi 0«00 *1281.85 5 t 68U to "A; 4 o 13 16 i2i 3 O2 0*,00 25 4 333 14#833 35tae 6f5*7 w 2* 6 0 5, 'Ni23006 *0 1*# , 01 16.660 13429 0 0 0 0 27*920 *30 . 16
13259 7 , 1 *27
18 1610 Q OtOO 8 3O6q7 i a
t 9aa m30-35 -127.39 19 18#01 0*00 334313 20*467 -21*io *5 1, * 56, 5;, 5*7 " : 5 3 1 6 *132142 20 20601. 0*00 36 * *40 22 .633 360 •72057 to 1 -3 Z-, -t A- 0 21 22#03 2a * e06-_ -, 0*00 39a6L 9.:32 2 s,89o-o5 6*7UQ 1 %150 423.
.az 24402 0*00 43t207 28,213 7434c' o 56 # 10 ml-95#82 0100 46,467 23 25,00 30*200 w 96t!57 00-00 24 0400 m3o533 12 # 8 62_ 5 1 t 0 4 So A-72 PC , 14*,6857' TEMP I YM/Q ly/w RM/Q ^/Q ID/Q PM/Q PNT ALPHA P S I 1.8407• 128-66 woo 514 0 ^ 67 -1 * 99 67 ,, 0 1 ' 0 9; , 700 12 *660 30 *84 - q 134: w02 00-00 g16t633 Ut.
3 o-4,01 37w79 "138902 54733 4 ;0 5*98 09.00 *22 2000 13e767 5#867 444, 46 m1*0003 "6 7099 0#00 mi27m633 -14#633 i2io14 5209• a 1 50 •' 03 x10 00 0#00 - $ 1 - # E 47 16 0 , Q 67 0 60^12 59 * 96 1 * 1, 4 5 o;63 6 J '1746 " 180 7 wia * 01 0600 P - 37 100 ; 1.3 . 106 01 .
6 74 -w I 42 0.6 2 '51713 1 9 1 ^44o66
& m0 0 i 4 OWOO 441 400" 0187
68-i , 66 x,138.88 :367 015*91 - "43*6 — 9 0600 W129611 18913 10 0400 04'00 129467 5891*3 1 9 9200 030767 12*25 50903 5060 1!126441 2#1,00 121500 ii 1099 0#00 8%33 ! !_12,4 42 * ;;1 540 00 4000 0000 6#4 67 A2 *4 67 35. 3g 20,06 -^124V76, S33 A^a 0,63it r i: 0 ii q -4*20 3 6 4, A ^ - ;5 14 slog : 04,00 158900 , - 130000 .
W$ 0 10*54 0 128".4 - ^OwOQ 19#933 42t 3^ - Z A 45, lo t 00 9567 50567 V+ 23 w125k ^ 80 .16 :12902 O0 ' 00 25*300 1 4 36c?.3 61633 -2*091 milS•Ol 0900 289187 161293 169-64 '17 -1401 -1"7@61 70000 -31 015 7 18 - 15*99 0*00 3i0iV '17s 8 73 16047 ' n -31t5l -6W*A o, u 2:'67 r66 553 19 18#02 -G*QQ 33*360 •2Q• w20 ` 6±130 *IS 20z 20oGj 000 36 * 567 : "22*113 ' i -470'89 : 50567 ' W34 06 - 4 1, 74 wi36 *-39 39,373 g4 i: 4 60 1 * 65 i 71 -6 - wiU0 21 !22*GZ .,0*00 m 48w*5 "150907 23099 w 83#91 694780 :22 09,00 43#440 279867 7#133 6;53 194 6,152*62 . 24698 000 46 9100 291533 -92437 129467 5 90 2 24 0000 00010 w3#767 6 z'^» 13 - is p x--73 QUA1. T poo p
Or
TUNNEL_ Lmi SPFED WIND T aT '630 VlltlOH'Y WXND :AXES 19/Al QAQ'7 RUN RUN .71 14.,685' TEMP si t P5 MACH Ov2251.
QPSF` 75*00 * 70 RNFT 2532185 YFPS, 256 Ti'0 T05 Too; TO!Z T02 T0-j TOt T03 T T.S?2 - - 0 0 59 0 0 0 0 0 0 T20 Tit T12 T13 %4 %5 -TiG %7 T15 T1 g p .AT ^3CA^L^ t?AT,A^_ 31 Ra L E$tIPPORr .DATA DATA C.4,e; ^^t S= RMIG YMI PM/Q Y/Q PNT .ALPHA -PSI ^/Q 'D/Q 17.85 •13.2.5Q -0.Q1 00010 ••34633 62# 06 = '9#7oQ 1 <43 . 567 r 25 *90 5 w X133.62: 2 .2.02 O sOG .g ,g33 13.933 78 91 8 0.1 14.'Ar:n 29 * 90 101.96 $e: 487' 80131t$Q 0«00' in I 4' ► <306 3 1_3x99 35"06 w1319,96 5#467 0#00 .201000 15.733 4 1,16972 ^ y 41*-54 •?1294t25 5 -8602 0#00 59 313 ` 24o547 16067 124959 48.09 w 13 1 #, 7 4 6 w2Z g 649 .940 109,.70 5#173 ..1040 0000 z 52.47 1 -0133.26 . OU " 40900 7 '•12.01 201.500 11, 0 2, 8, 31.533 60 66 -m132P46 .011 8 b1+^^0a ..95#560 22 . 95x3 67 4 #g 27 1,10 f,ta :fir 64s41 Mi3 28 A#86^ 9 .ISv01 0 ► CO' w37'.50f3 .23*233 18h24 0132.71 0.•00 5#667 10 -0.01 -3.#567 1.3«'333 60*,65 5.667 11«45 04,00 2. # 1;67 miw63 "132.05 11 2.05 13#267 6•!i9 a 31.,46 5,667 :12 4.Oi 0.OG 7.067 1 2 .200 42#36 131.78 S?.•00: 13.467 3 700 43 60i 12 * 400: 35.#92 : .
e, •1* 0'«0d. 16 35'x02 $#Q^ #967 S3#900 10.62 X1 3:86 91 L I L 37e74' ;:'6#133 r 0*00 C i4•°600 9 75 K130.39 0#.00 733 38#61 502p w 13 16 11.99 26 # 15#467 -^Zt88 6*467 m121#•86 0400 17#0133 19#29 17 1308 29x1,40 0.00 31sg87 17.60 7.137 "SI V 57' ! 1 8w99 _ 18 16.00 18.667 -34#0* 4127#86 Oc0(; f.+4 6 . 233 19 18.01 ^b.60Q' 2id000 di.i ' : , X33 86. -+132 «g5 P. F.0 G1 4«00 37153 23.060 4 *«4,9 T ''S a 567 .
0 41 -gI36.88 im6gogh, 690,73 0«00 __390913 25 .64.7 21= 21 99 ..,46.,28 0.00 6 * 467 -.147 * 75 22 . 439240 28.500 - 87 #118 • 24 02 .:155#91 6#833 -52#67 25.02 0o00 = 97#-17 23, 46027 30* 467 1,8.•74 0400 5+667 w132.2l 24 0.010 mat 67 13.533 61.55
p p, Co k 3 A L i 7Y A-74
CA P 630— SPF90 WIND TUAhM TFqY VOUGHT Lmw *AXES WIND RUN -72, RUN -7 1 2^ F0 1**656E TEMP 84 4 RM/Q YM/Q Y/Q FNT ALPHA PSI D/Q PM/Q L/Q 1,$:•,08 : .
0*00 : 7-07 0 00 0 -3o 13 *13 0 * 9 6 , 700 41fss^ w ; , W ' 92 ^o 1$4 * w00 59 0#:00 -9#467 -14# 067 ' 87 i .7K, 98 6! 6 : 5 29 x 4 6 M 1132 i 9 3 0&00.'' ^ ov iA # Z O O: -140 M, . 253 35 0' 87 l g 130037 4 , 0 6. 1 03 0s00 w1,9067 15.967 5 116031 q , 85 410,20 I J260' .
• 16 00:00 5.020 5 0 8001 w24o567 17o060 124 6 w 9#96 0000 • 2 1 3 10., *31 3 7.1 1 89880 1 Z . a 0 1, 9*00 20 066Q 2 '' 7 41 c6*0 1. 07x5 a 22-4 0 1^sO.Q o ' O.C . a.38.g00 J4611.- 4 7: 31,3^:-: 0 0. O'G , i,3 o..
7 - 64 ► 02 , , j 3 01 3 3 1 is 000 i 467 5q687 171P69 -1131,-28 60@59 10 0*00 0400 -3o467 13.520 11s17, o130o91 00'. 00 1#933 13o*00 5005 59547 11 240Q 6*,39 .
OsOO 414,39 5#460' 6 "'130 6 9
12 4000 7.133 13o300 59: 5 : 6. 1. x J,.,2 9 6 4 33 5 3 L3 5#99, 0 : 00 12.067 '13! .3,4 32: $a7 .: w4 l.
4 ,^ 5 a 7 #53 34x51!
8#00 - 17 6 71' . 43 9 67 vA.0 i , 9 6 pt i . 3, 1 '#,J+8 15- 10 .80 . 0 00 22,667 -14' 700 36. 4 2"" 6 : 063 54663 w13h66 *130t06 15o567 16. 1109 0000 26#633 37••59 6*613 .-240+3 -118*81 '17 16*43 14 . 02 0900 29#220 '17#267 --50o, 85 21-o1l 70320 =118#56 18 15699 oo0C 32•o00 18o533 192.0o:': 12 sz0 . -350388 .1 ^ 6•53 00 , 00 18.x01 350200 1 :-,OWO, 0.13 13 - l-'s. 64 20^ 16402 000 37 .8^00 : '23 9 ZOO 7$- 6 f S 8 7.
: 00, .•04 0 + 33 - 1 41.'x 21., :2200Z : 04, 00 41. v eoG, 25o800 i* 66s. 06 5, k s -47#, 32 041,529.44 69120 .22 -24902' 70 86,15 0000 43*740 284600 w540,20 ,23. -2409 09100 30#300 6020 -164974 450733 -98047 1708l p wi31613 -24 -0001 0600 -3 * 467 60023 50533 13.600 ORIGINAL R m lcl - is 'A-75 OF POOR QUAL•x M Y TERT
UNNS .630
NeUaHT LBW SPEED W L ND
S
WIND -AXE /Q RM YM/Q ALPHA PSI PM/Q Y/Q PNT [./Q D/Q 03#100- 20 *,93 1".
153109 1 Cf+00 ^5 483$ 60,23$ 0+00 53430- 299r04 *4153x.19 -1# 0+00 t. 691133 99 -8+93.3 10#333 72 37 ^1gg.& 34:^r4 _6400- Q•Op • _ 3 w 3+99 +14x633 ti 1^ • 39+76 "148#04 0.00 59667 4 w 6MOp 12.313 121.1,1 x!194.707 ..
45996 5 4 567 -143961 5 ' w 0 # , 00 7 * 99 •+23 # 220 14 #033 120 4 77 0400 -148.7 6 w10#00 w26#340 1Be767.1. 6 5 51233 5`2.25 , • 594112' w14so*7 17#513 5.020 -.11x#9'$ O.Ot^ .431rbi^O t224k7 04•.71: -444,162 4 4. 0 0 t3b431 ##760
a -1 4.09 036,4700 19+467
7'0x4.% #460 9 of V53# 9_ . w15-pQj 0600 'w 80 2141 , 60 wi152153 0400 64167 10 0.00 9+800 51491 "3.167 64033 14#:422 0150.61 2#01 391.45 11 0900 2#633 94567 5.9-33 "1470.04 12 4100 041OO 7.900 30 woo 9• 00' 0- _'. 13 6.01 12zt0..' 9+200 23P05 0 t 0 0 ^5.b6 a-40 23s4, 5`•147 . 1. 361, 14' 0 +00 ' 104233 17.733
10r9g
X4 33 "135044' 15. 1,19 ca 000 2240500 11#060 2.6i I 7 7 "16#:52 54733 `!129407 16 0*-00 264500 11•967 23121 37 , 14 22# v 84 0#00 5093 !124 '17 •14* 0 1 304567 13.400 13t7?.
6 # 173 "314.58 ^^21 •-^,7 -, 18 16.01 04 , 00 3 ,? o 567 15.327 96 I1 _ . 1 , 09. 0127.:59 .
4 4186.0 19. ;-1.8 0:00 ^35,t200 7+873 +x26+16 G0 4+300 "32+.1,6 "131 +•89 X20 # 43 0 #00 41.63 2Q. 38,'020 «24 -57 x:80 "38 7`8' ► -".41367 w137+Q8 21r99 0 +.00 41#333' 22.66'7 41.83.0 ci ` -4404 On1,43r82 .22 -24400 444533 25.893 -105#•23 58100 i 5.500 -48,27 "1.44#38 •23< •24499 0.OQ 46#460 27`#327 w 1124,34 20 •'97- 0 400 167 6.100 -.1:,52.51 •24 0.00 ' -3 # 9.873 53147 e' __ __4444__ !,.
,UnL6`uV Q
A-76
TcsT ^. ..VeUQHT.
Law SPFgD.. WIND TUNNEL ; h 630.
WIND :AXES ^1 ^ N . 74 RUN .74 ,; ia9/8i ' 14x6464 TEMP 64# P5.
1ACH 0 ,x2864
Q PS F 75 # 00 'VFPS :252t97 1593290
FtNFT TOk T10 .
T0?` T03 TOFF TOS '106 T07 1.08 T09 0' 702 0 0 0 0 •74 0 0 0 Tit T12 T13 T1* T15 T1 g T24 T16 T17 %5 0 1 0 1 0 G ; TYPS 8URP0RTB SCALS DATA AMEs. y e n E L DKIA :'AT C tFULL RM/Q PNT ALPHA PSIS L/Q 'D/Q 'Y/W YM/Q PM/Q 'r Q7b :r.(jrOQ 221`70
1 : ` 81113 115$.20
"210.3::.- jk 1 4' 300 2<.s x 2'. '* 6 `. ,: 26'tin8 ^168k55.
^2r05 4 r-O +$. 16-x'' 733 46.110 6^3! bl 33, ► 4b 3 ' 44 02 Oel .14'.700. 6. - J 3159 ,12' a. 701425 47 lA, `•-.
4 -6.05 m 0'r.76. 39.4 50 w201400 13+333 89137 50867 IN145^9"r '-7192 5 w 01, 76 m251467 5t6u0 470, 40 *1361.-68 14+333 1001. 50 6 •10.04 0:76 6.167 5601 n .28.453 15.900 75491 -144.96 ..1'5'3 W.
7`^,11 98 7 .mg o 76. . n 3 74"k 1.5 33.1"33: 17# 6O0 61,5; 73x16 ^00,7b 23:2.'7 a: • G•00 fi 867 * 57x:0'2 v+1:x833 11x34'7 26x75 ^0«76 X153.52 9 2•'o ' 3+333' i5 3 _7_58657 15.:57 it '100 - 10 4003 -0k76 7.900 50533 7•,69 8#32 111000 7 1'69 - 14 i*$8 It 5.98 w O-76 121033 11.000 3490 51507 w140}70 -01,76 .12 8 1 0 690334 -7130 "J36678 i 16 .333 11 1300 6.55 • x.3 .;58 13 9.09 w0#16 1 6401-3 : 20.667 11.1:767 9r 27 1. 13114 76 1933.12i156 i4 2410'93 X3'.48 ." 5'0r67 S24913 15 zo001 -4 0«74 Si 4'"790 22. 6. X25:7159 -42.033` i1•433 `1.5 a I i OF V^"- r, TEST 9PQ1aLND TUN EL V6.UQHT LffW ,.424 WIND AXeS RUN 75 f1112181 134,6 RUN .^76 ^.._ P0. 1#,646* TEMP 739 MACH O v2254 QP^3 15'S932O v '. 75 r OO YPPe , 55 14 RNFT T 'C,10 TOt T02 T)3 TQ* . ;'05 10f'' 107. T''08 9 1 0 702 0 75 0 0 0 0 0 0 %6 T17 T19 T19 T20 ° Tit Tit TO T'14 T15 0 0 0 0 0 1 0 0 .SCALE 11.G DATA AMMS TYPE. $UPP9RT i^ ^^ _ d,^T^'AT C.O.
CAM/4 PM/Q IY/W ' YM/W FNT ALPHA P SI L/W .n/0 13.50.
..x.767 67 3,1`^OQO> 2054 Oc R r 0.1 ^Q+'77 r s «64 O.ii 09 .0077 33.a5. 0467
2 a-2:03 .84047 *400 `
t, .
04`133 •6927 a '40i7 7 11+933 62.75 '2 * 48 309 = *14 000 r 3%28 820,00 •5*39 mo "Oliuu 4 6e06 0977 v20v2 12.967 b1r32 7+33 5 '- e873 ::13#980 93#51 -0347 7 !90 "0477 o24 . 3 13#, 04 .93 -00167 6. -1.0!05 ' w Qr77 P:27.880 15#753 69438 ,7 14#.61 •3.',1 7.487: 95'' 0,e133 mt1a p 01 w 0. 77 w33*333 1 71.# ., Oo00 x 8 1 36 11 69 0 100 n • 0#77 • 1'#5.67 10.967'' 20+r,56 -w15 50 O i 133 O K1.b 5 -00 , 17 10 0833 JO «03 1'E°9 3.367 : w 21 w 17 10 4 , 02 09 0s77 8 o 133 10 733 01487 -19.71 5;87 -3«06 0x767 :w24*14 .11 5.96 -0+77 129300 '110.733 1*78 -7«34 +27.30 5«00 ilsou ' 12 -0.77 16.G67 10 933 4+78 .
.., .p t;;77 ^S r bS aw25 e'77 Y.0:,,.03 f 431 6 i F 567 1: 3 a 967` 1 +'.72 .94^t13^.^i1 747 lg 33 121.', 1.t"^'^ 1.'u^r :z 2#,34 .Ii"k+81, .
0t000 15, -, 0 00 ° 0.'77, 'w1r567 111004 ` 2?+^^ r "
A-7 8
NOUGHT EST Law sec- D WIN fiUNN ,L °b3.0 WIND 'AXES RUN 76 176 _ 1 j/^19/81 f34& ftUN • p®. 14x6464 TEMP 75• PST L,/o p/Q ' YM/Q ' PM/Q 'Y/W HM/Q FNT .ALPHA
0O•77 x ^2ti48
0.75
-6273'
10«9'24 1E07'
1 ^ Q,*Oj -Qx633
J
.41«59 wifli
w Oo77 1. Zv 167'
2 -2.03 -6.667 iii , 300 6.10
. , -0*29 , 1*07 3 _ -4x03 ' -OoM '*12.633 12.033 33 «65 • rQe 0 7 a, 05 .
.6 + 1 «65 3: 87 - 0. -0 # 460 4 7; .±18.367 .12#800 51.21
6,,42
64,35
5 -0#77 # 600 14#033 53 F39 "O t 580
-7 * 91 *122
90,016
0 0#77 1*, ik
6 wiO#04 r26r467 15 * 633 42,o 4 7 - 0 02
1;.1422
00+,94
7 •eiI SS -0.77 .'31x933 50.79 0.10a
Oo.400 0w2f -2r.
-O:OQ - 100#433 333 *4
8 0 #77 10.900 1006 F N G0
'0I(sz .4'•66 9 -Oi77 iQ#!633 x0.453 2.01 4,433 .0 *25 -84-64 ,w0 # 167 • 1.0 4 * 04 m Q M 9.067 10.567 m8, ° 77
-0%48 *9.78
**0#'77 9600 -10 09047
11 5*98 1341,00 10 957
03960 00733 wi2*.12 42 8.01 x+0.77 -7.37 17.367 1,0.967 X6.3(.
01967 X12.68
13' 909 O,e77' P1.233 51•4'00 00,94
44 6.«70 493 w8r87
14 11 a.99 -0:77 "'.2.4 .12 433
11#77 ;: "0061 1'84 +2 .89.
15 -0e77 -0.!S33 11.0'67 -b';«56 {^902 ° OF pooR QUALUY YOUGHT Lew 3PEE AXES WXND UN 77 I 90; PO 1*4607l T4MP 14963 , 164 MACH 0x22:57 QP5F 75#00 VFP S 259o52 0, RNFT 0 = 702 0 0 0= 0 Q 0 77 5 T16 T17 I!$ TIO T20 Tit 112 T13 Ti# T 1 0 " 0 , I 1 0 0 L Q SCALE' DATA AMESO*TY!g SUPPORTS*MCDEL , DAT A 'At C1•89 'Y1W RM/Q I ym/q FNT ALPHA PSI D/Q PM/Q 4/ Q Q. 1 2 *45 1 8126'7 9o167 "136*66 tA Q 0,587 2011' 2 ' -2 , 003 0..02. 3 • * * 361 9#200 o5$$#97 *Vt767
-2x 9
, 2 3605 3 *4s 01 09..02 0s, 7 33 -w loan - - 90933 - - 2 40!69 61 , ,69 4 533 ' 9 4 3*0 4 *6 ♦04 00,04 4833 WZ0006Z 0 1 13056 002 w6o267 8#47 5 ' 749t 10#300 *216#45 w i g 967 133, b 0602 " 106J33 6 Wi0#04 + 553 .*222683
9 ! . ,1 z 16 o, 6 t
7 ai2#02 0K02 *1 1 5 ,200 ' 12. 067 *1 5 41.o *9 .-6 20467
*•04 12, a 0005 0 02 , R * 233 -, 139 * 14 -istOO 3.
9 •'16'7 .
►
3 •b 1
9 1,99 04 ' ,2 # 2 0 0 1 16 i of s -16400— 02 11 # 500. 1 lo- 00019 14,93 - 0 024 t 4 t 5 Z 3 - ' z 10 J + 0 0 7 'V 903$ *93491 0 0033 2- 25 wo v 93 17o267 9.4 57 11 5097 0 02 *-714.73 -Q # 6 33 A w2
-1 o 69 6 V5
96. 900 00007 .12 8*00 00,02 200^00 ^
13 9 0 93 23. , 567 10.5Q7 . 19 04500 ; - 4o
002 -26 -6, 427 19, 4 6 14 04,02 26 .2'73 11. 0433 -$0 , 63 0f 487 : 12 .03 3.64 - . 9t200 wJ36 * 9 3_ -0, 067..
15 o 0602 - 89,200, -?-. 92 OF POZQ QUALITY - 6 30 q VOUGHI -1 ,fjw SPFED WIN TUNNEL TFT WXND'AXES U& fi,/19/gi RUN 73 PC . 14*6071 T6MP 94• 'Y/Q RM/Q yM/Q PNT ALPHA PM/Q PSI L/Q 3x'47 3 63 1 — 1 -0400, 09:02 NO 60 •*41 X09733.
1.0o*33 2— 2 1 04 1, 72.
0 *0:4 .- 6 633 0t467 180 0 10.861 .
- 3 44 IS J-36 3 *12.333 11:o -30taf :, 0•1g 3**,59 59,76 49 iaS -0 9833 4 -6#05 00-04 o q i 8 9 333 .120400 l 7*93 10*79 0 • -19460 5 -7 9 91 •04 - g 22,640 .13*467 53.9 4 7•;68 -19987 i 4 'e , 8 2 6 •10003 00, 04 •26, 6867 15e133 46s9M 9,* '110,59 7 '•12001 O's-04 : 102. BOO 16:500 6 0 * 3 4 <-1x7.67 .3 38.
cig 0 * 04 W 0:6300— 10. 06.7
5 2*00 04,04'' *533 3 0 §0, 1'-72'
100 *40:96: -t o i's 62- 1w-*5 . 04 1o37 10 4003 0• m 0t767 9e167 10*167 w 8e57 1'9:43 0 tlO 0 li. 5498 Ot04 13 * 367 10#133 -89-94 -00500 o5o75 09O33 =1*36 0o'37 12 8400 09-04 179633 40o433 u 0 0 -0 #;:': 56 43 .$ *99 QW04: 2 Va 6 00 1. 033+1 .
48.1 *,453: 14 , t 13*85- - t 4 1,,3 58- WO 633 w09,R33 2,0-9 : 1.5-, 100361 , Owo: oilok O i l POOR, QUALITY a K YOU4HT LaW SPEED WIND JUNNE[. T, T .63 WIND AXES _. I RUN --71 RUN 1 1 it/:;, / ai 1346 19 TEMP PC 1406071 34# 75#00 QPSF MACH Ot2257 VFPS 260.47 RNFT 14826239, PNT ALPHA 4/Q 'D/Q . HM/Q ' YM/Q PSI PM/Q Y/W :_
'
: 6 .45
1 0.ia Q ^F Q 1 ^^ •• 4 3 190 3 1^ 3 r3+ 7 5
1• 3 lOtS 3 3 i^ t^ 1 3.
/ ^y / ^ , 0 / ^ / j ^ ^ j j FM 1040
p r y f r y y/ ^ j ^ a;..2 -.2 # 03
^ <OtO a 6'**&:.. wgo,32 M ,' 38*19.
$^'06 ali 9 : 6.65..
3 • 3:99 0.01 i 0603 w14t267 11.600 __60.75 "Is *14 4 -6#06 -0o.01 w2Q A 267 7,44 12 # 533 3 +•54 80 # 81 1 ^0 t 533 5 '-7#90 w 00 , ,03 00900 w24.#967 13#567 91098 0 2w,79 6 r.i0#04 - 0 0#03 6.35 -R38.480 15.300 111 " 11 533 _10 4*82::_..
7 •F12#02 0#^O;i 84 0 :33. 67 16. 567 ii g t033 1.L. 3.2 6 4' t^0 .,6
• 0«0 6038 .8#.i3
0#O2' 3 0 ico600`' , *0.333;
O it80 18 #•95
-0`..03
9 '...1 # 99 3*400 10,333 . - 12#AA 5'^9Q a 0#97
Ut420':...
OU w03 mjZw93 10 4#01 8#167 -0t 167 1+69 100333 6960 5.98 *•00.3 i1 12.600 109333 3 0+033 1134 408 -13e4.7
x ' 0•.03 M12
12 $ 101 17woOO 100633 -4#.93 04633 owl i77 #78
9099 '0 0R03 0#000 X3..' 72' o, 45 13 210,433. 6#.53 1.i#167 ' .
#.71: 32.02' *0*03 . ^^ 46 14 25 0433 1a IV' 31 0 16 78 7 ..
^O: Oi . 5'x91 o3e 15: 0r02 t633 #.0+5. 4.0 ,, 61 - i 19 .-01473 mr, 1 1 0, & 8;4 oF P03 'R C^UAUTY VOUGHT SPEED TEST .630 Lmw WIND—TUNNEL 'AXES WIND PNT L,/@ ALPHA PSI O/Q 'Y/Q RM/Q ' YM/Q PM/Q i 0#04 gsO*Ql #700 ,110:033 e , 2 5w1;33 --2*03 *001 .,A-a 5.367 34'02* M R 1511*55.
067 110433 41 0,}8
3, *3 .99 x '- w O l iOi l o 1 4 5093, 41w50 •s 1 , 5 8 w 5 z
400, ''12 .027 65x1 Q Ol 4 — 6*07 0 0 - m 2os40o 85 0 .08 501*o 48*10 *158051 12#987 56*,65 5 ' ,m 7*94 ow O 01 •25a120 140033 95133 4f6SO 94 15 5'0• T^ 6 w10*04- -OtOi u286300 15oaog 640°80 w1*5m25 74a,55 4tiUQ 7 , 0280 ':, 17 129 4s827 1 30 001 244 - 0,00 1 14 33o 200 17 .
00 2802 0 t *1#567 1110'67 1$32 *iss*86 r 210.4l' *153's92L^ 3,567 10 933', i2 o7& 0640.- *OOZ -Of t ol Bo967 loo733 40600 12c 6 2 m 147 42 6o , 76 59'97' il -01.01 12 * 500 10 * 833 40 633 6.34 wi421.70 '12
8*00 -0901 160200_ 11ol67 5*97 59233 -2• , 80 w141*,49
-33 Sfoa .7 ; 14 '1 21 03 -4*01' 44 667 *12 s,28 *13*-53 25 . 4027 1205.71 4*0
15 04, 02 0 0101 6 If -156:301
? 11 0000 22; 7 F *1667
0f w 0R;G:NAL Rl T., 2 tlS' A-83 OF POOR Qt9AL1 a Y VQUGHT -.MW SPEED WINO TUNNEL_ TF9T (' 3Q WIND :AXES RUN Ai 3i/i318i ^ RUN at ' 1 4A TEMpp so, PO #4x5973 75,00 QPSF 863 Of 2a58.
VPP9 25'9 ! MACH
61 RNF'T 4495' " Tut_ 1 02 tQ3 T04- 7.02 Q 81, 0_ 0. 0 0 0 0, 0
Tit T12 %6 TI y TZo
TO 'T14 T15 T18 T1 y AME$-MPE 8UP00RTS+MaDEl. DATA 'AT C t G o FULL SCALE DATA PSI PNT ALPHA RM/Q L,/Q D/Q PM/Q 'Y/W YM/Q
4 1 70 . 0
1 0102 W 7#900 26w30 P150..83 QWQI 9.6.00 -1;30-8..5 -2•a^ -Q^ p ^.00^ 5:0^7 ^i'•^^a ^^,S:^^S^ ^.^33: ^^54F4^ f 3 ' M 3 q , 99 M0 # 01 Qg433 goa33r • ^j 38.05 •^ 53 a 4 '06 05 0+01e J 4t967 4329 *1,53^1+^ 2^967 1.0+113 ^-191«86 '-7*92 o-04 01 06.300 10#633 a209v% 40500 524<00 *144s49 e, 6 -m10 s0 4 0 0,01 *10.300 11.400 « 3 33 59 68_w*43s77 -228•Q7 4 7, •11098 ' 4+533 680o a ► 44469.
x•16.100 .12.267 w234 96 00e0 1 •p • pp "0001 26't20 ^152 «8.9 7.e00 9' b7 .334 8.3 4+6'S3 t1^ 6.^^s': 9 "', ' Z 6 0 Q "600' _.1t.QnO 20ab1_ 9• 33 •i14.00 Z9a_ ^.
io 4 6 02 -04.01 4tQ67 1402 mi396 140000 $#700 4 91183 iw - 5.98 -0#01 1,6,867 7,080 413205 1 k933 *+69.54 40033 .128401 0 0401 191967 10+332 -129,70 4 4^3 4 ' 7 9 .
9998 ' n 13 !09,01 23* 8 10.933: )+23'.71 7 viz$-4 le002 , wocol 25 4^5.Qp p
1k 9 533 i i" k833 1le#97 R12^+~47
4 01 28 • 0s00 0-0x0:1 ► 6, 6 26.17. "151*32: '/*SOO! 98.567 .*+133+ . 664 ?
a"M c C ()e4" c C'UN d V ' cF F m A-84 VAUGHT L.nW -SP_F99 WIND JLNN Erl ^ TFS^ JS3 0 WIND .AXES PN7 ALPHA -PSI L/Q RM /4 YM/0 'D/Q PM/Q 'Y/Q •+ ^®•C:1 ^' 27w7Ct i, Qs03 s1^Qv7' 8.100 ;•^i23^3ff 41sc^0 *148.72 . 1 1x800; 33x05 ► 9.67 : -155*8t 8+267 R139 96 0 : . *4 ..• 3 •0s0 { 62 4 -6x05 -0.01 5x5u0 509 , 041659,35 -3+200 80700 172r52 a 5 -00i 62.;15 '-7+91 m 3x967 x185.59 59673 - 174+17 9+067 .10.03 0 0401 .i^4•E6 5*887 739.85 x183'•41 - 5600 2 . 5Q0 ? X12«00 w 4t0i 51633 S1t7w ^i78.32 » 6.033 10'•100 •205+5(s a o oto l -0.00 • .1.6000 8•i33 .•120'x93 4x433 27'i it •,1150*76 "0.$0 ^i!r2!
9 1.99 • h ook . -106.7q ; . 4`0133 • a•o67 7.967 15 -0401 10 4 +02 0.833 79900 3.900 12x24 sKI35r56 -92920 11 508 , -001 14700 7x;02 7.700 76.30 3.667 K1.34130.
:e 12 -0.01 0..21 3u 8•02 2o667 —57—i a 8 3 3 , 13 9 498 -0801 443U0 `6r79 *136X05 3.600 7 ► 700 x39•.36 • *i3:.'70 4* ..1599. , 0+D1 4.500 78833 }21120 4t 6 67 *L142.40 ; 55 ^C.^Oi :' 266 193 0.01 -0.567 8'•200 ~122.21 4 4 4 533 "15043
Q[w! nuJ^aQ t' 1 a F S
—^ OF FOOR QUAL17Y Vf1UGHT L w SP En WT1 , ruwNrML T 'BES ^_.
WIND AXES RUIN g3 ,
i'ieis ia t 346
R 11?4 i3 pQ. 11495973 T MP 779 E MACH UtZZ5:8 75.00 QPSF VF' PS 2 RNFT 15420191 56062 .
TO 0 0 702 0 83 0 0 0 , 0 Tit T12 T13 T14 T15 716 Til T18 TO T20 ♦ FULL SCALE DST's,
pMES.TYPE S(P ORTg. I IlEL 0AT 'A, C.f-
RM/'0 Y/Q YM/Q PNT ALPHA PM/Q P SI L/Q .D/Q ► 18 ^1,'S3,^k6 0 ^' ^ .. ,: 1^7'c^C ,r 48:29 ; .25 ► 0 * • Q•01:9.567 9•:553 35•,2 r^+toj 157.31 2 : 4 2.03 •QR01 113,033 10'1 33 42s1.1 - 62 a28.
► 6- 444 5:313 3 -4001 " -0 Q1, W166 00` 1o r 52«38 ,164.1.5 w 0•.01 M20+733 11.480 5 4.73 4 — 6 v 05 994-42 63.,58 "167915 59460 5 w 7+92 •+09.01 P4 22#433 129607 105987 75c23 w173#.Z 5 ► 667 6 w1005 00.01, n 23.600 13• oi.gQ 0 S 81196 5x933 "i81.27 Q•c}1 n230.733 '15R 0t0 109f, 28`!44 miiS 61 8 o4O0 O't0 1 .93,433` 10e:45 _ 417 . 00 9t50Q' 4463 3 20«98 a' 0'96 P's 0.0.01 9 6 00 5# :0_ ^, * 1,3«25 4144.88 10 8+833 -37«66 49367 4003 0:.01 -296001 44367 5+73 -145.17 0401 09 600 89567 "57+97 11 5+98 00.01 4.467 014.08 "144.12 :12 8•01 3+800 8+353 -78,022 5^0c^7 ^$Z9 X147.37 lr3 999 0001 7,.5Q0 $•333_ w 100'«^S 5.e300 .*509 P4152r63 44 ^12.09 0 •'QCr II *1 67 8.667 ''op ie4o,33 28'rbQ 0_ 3,. ' o 15 40.0 0}00 -9 @ S67 ^i•7 0 0 c A-86 630— VOUG T LMW SPFED WIND TTtiNNE - S ft L — TE WIND AXES ALPHA RM/Q PSI ^L/Q D/Q 'Y/Q YM/9 ONT PM/0 I "' ."
I , w-j 6*14 waq r 68 0 0 01. 0#00 : 6, o0o. 9 33 74667-:-w Ap 2 , '-2 0 , 04 00 , 0 0 33 ; 1 *'a w 6 -1 00 3 *4 C2 Q 00 '.2 -Joo i Q 2 7 -I ' • 8 , 00 -2 # 967 -3•.52 4 0 6905 0• 84433 w178973 -1,*220 jjao 0# , 61 5 '-7991, 0#00 -36633 wls 8#833 wi93,00 67 13:.41 2D S 5^ A & ;-2 *033 3:•09 6 .+16.05 0 + *00 -4@573 . 232 : S Ot)O 14'05 7 •:02 7: M1,260 , t 0400 ow$,467 - :: 4 8.00 watlo, 40, ': w a 6e54 M3*82'.
, • . 0. 02 00833 7*667 p 23.58 a -a
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k oo - M 2 v 52 10 4 * 02 0. 0q867 7 , 400 -92918 -1-9400 3w wlv32
li 5,56 X067 79267 -74996 • 19 5 0U
-V;35 000-134 9, 00 .12 8800 0 2 0 0 7 8 21'' 1 3 t. , 7 6 7, 7 4 ZOO, . 3 0 00 x2 .71 olroo 73 a 441 1 .1 2 , 900 '0 367 2 3 W09 t •
6 R>4© w4 + w0a
wi 15' 0601 0' «00 e E67 - o c ()RIC , .jN'f\ L!
(3F -c-o- iz QUALITY r A-87 WXND'AXES RUN Rog RUN 45 fj'^19/-Rj 13k6 TEMP PO 14*5973 73, QPSF '1500 055*57 MACH VFPS. RNFT -155670** 0,2258 T01 T02 " ' g 0 g . 109 TO*, Tos, To 'r , a:z i r TIO T'0 3 702 0 82 0 ^ 0 0 0 , 0 0 Tit T12 T13 T14 TiS Ti6 Til fi g 715 TZO 0 0 1 1 0 0 AME%-,TYPE BUPPOATg ' *mel:)EL DATA 'Al C-(1. FULL: SCALE GrATA.
PNT ALPHA 'Y/W Rm/Q YM/Q PSI D/Q Pm/Q L/Q .0 4 0' 4 90Q 0002, .647 1, 4! 91 76, 8 P467 -+123.86 4 21 1 03 8IP600. 59 • x33 "A 60 t3s' -14101 : 3 .-2
w 4i0l 0*00 , 633 i l isatal -,5q467 4244l " N i6$0 - 24
4 - , 6*06 Oa-00 -31067 9si67 w 176#80 5033 - z 170'9.15 15 52* 0 4 0#00 5 '-7o9O w3,833 54580 634 , 36 5.433 m189416 4084 , 25 0000 74*,36 oi86o.03 6 alO*Q* W^#R^3 9s860 6.1(2Z wi9 L66
6 -
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•1 1 #98 2 07 5 o.: 6 33, *180••7*
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9 g•OZ, q ► 00 0 - ^33 9g290 wl. , n9rbl5 4 . t4 20t3', -141s76 otoo 10 4 + 03 0 0 900 8# 1 67 3.887 13'M20 "139o*6 -9204 it 5#99 1,o800 34700 7&46 w138s2i 7*933 -77#,08 .12 sool 2o662 7 * 933 -59o17 0-914 oi39ev 3*900 13 9x9 0,00 3 * 667 6W96:: -1 7*967 *40487 4 f300 .
'0*00 + 67 t 14 i3+ 00 4.5 8;4 033 4.t633 6 ' 2 3 -13o ao -1*8 1 *00: '- 2 4455 :O000' 00,933 15, 0, {l:1 $Go 4 * i euo :" 21 - 4,80 • *i25.37, .
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Al ALPHA P$l RM/Q PNT 'D/Q PM/Q Y/Q ym/w L/Q 0*00 80 5'33 1 , 4 t5 a 26W30 0 0 03 v933 *33.
0 1 3 3 7 * 9 67 . `1:0 °000 3 0*00 4, t400 i l 1,,100 it 9-200 1764bg 3), ii i - 6005 0000 - 2q633 wj 60 . 460 , 16 *i5008* 10*567 7? 44 5 00 5 '-7992 0#00 -5 0 833 52059 100880 -21,3o2 4fon 0144411 410#04 6 14 : 78 w143#70 04,00 -5s532 116753 w230*12 4 6. U8 0 wo, $ 240t.
0#00 11 0767. iot000 21 wok, •1,1444i 4 0 033 4004 1*h28 100167 3#80U *133405 0000 14,70 0 -93447 ii 5097 3080 7*-5* 0 , 00 170200 1.0a173 w 71#97 8001 0000 206367 mat-09 "j$. 4. q 08 *m 47#18 4 q 6,i3 1p ,,#567
13 .9098 0:1
00 23,667 5 0 ila. 011 0 56: "1331,03 1 1 0 3 0-0 -25*70 14. 20:0 p 4 3 X000 05 - % -40 . 6 . 3-3 m-^2 - 6 0 - *1 2547 6 0 12.2'87 4. 9 7.::, 6 167
-w0000 t00 8 + 1 0w 025 wi38,7, q • 4 # 40a., p- I. s 0 #49
u Ca
op'lairM
OF Poor, quALVT TEMp PC 1*9 RM/4 YM/Q NNT ALPHA PM/p Y/w PSI L/Q D/W 5v3*7 R2ua6.
P-0002 o oa 4 0.100 .'.1Q R723 _ w1 1 w1 •;64 r 4. .27 2 :Wawo wo 33. 53..
X2 25 -6 • as2 e 3 0'0 s.08 *0 4 92D. ^ a87 ^. I >RP39'$5 _ .11 733 25i72 12 67 7,4$ 3 ► 4 "605 -0+02 w17,300 12.607 4705 *11120 -0.02 w 49 7.•53 5 '-7.90 13«800 49#72 -1.853 11 •22.333 , . 0 3.1,20 ^.p5 6 -2.12Q r10 *05 •:02 m266733 15 *393 45..35 10#83' x Al2,*QQ •Q•02 17'e;^2.0 53^6^ :..29253 j*o,76 X132.353 !`1 4.59 0 a wZ 83.
1, 002 , •02 -4.033 *1 s, 3i A$:7 1,09-747 .
..i^c^g' S^ ': 2r`Q.1Or;t72; ?F.900 1(1«500 *70:781 X367 4+064 -08.02 -14120 *4011 10 4003 90300 10*400 10+09 W WI+r•.94 39-04 5.98 -0x.02 0 04767 11 134467 10.467 51.1#81 - 1.45 8.01 - 0o.02 17.900 10.767 - 647 12 08. ,7 - 0 0 120 -3,87 x3.72 O+s24.7 13 9.:3$ X002 2.1..30Q 0000 ^iv400 .7, .00.(32 0994 -24 9 7' = -'1+ 26 14 ::12.'0 25.060 12 233 !3't : .15 • " .
w0e.02 0,000 040'1 1.0 *'o 67 * k2^32 *1#48:7.
()r poop, A_9Q LJQ PNT ALPHA -PSI D/Q RMIG YM/Q PM/Q 'Y/Q
O p Q2 - 1 : - w QtGl wO 5s-, W f w3
` * s 0o787.
' : 2 "-2003 vM1 0 , 01 • 64600 833.
18*,,3 3 isz, .:' 3 « *124200 15.273 31o3l *Q OF6 7 79 5w98 4 0 6405 "0601 81S6200 161100 14,24 47.37 N04833 116,18 5 ' w 7#91- -0-02 022ti667 46673 6 14413 91.78 17.F213 6 w10604 11887 14931 0 0 6 03. x , 27,653 18,633 45•.94 .-240 A 7 7 *UoO4, s RO# , 03 v :^ 3- # a3 3, Z, 0 # P..
3 4.6 5 i 047 ^_l 0,9 4 2 Via . q l 3 -0000 01 03 o*O * 500^ x 4 t44533 7 U 7'.'
9: 2#01 x 090 3, 4•267 so(): 5K4 2 ° *2196 4.+ 67 000;03 10 4403 3.4t167 004*1 "0#633 9*067 4$,*8 -5o,70 . 13o100 6000 -04,03 34,86 05,00 ' 11 -04267 •14 0 200 -3*;79 840 1 0 5 -0- 1, 03 17,:67 14*600 1 6 05 4 00 -00'80 -5o,74, 9. 99 X 0; 03 21 * 733 0 .c25 Q, , W59 65:, 9s.29 12.00 66 ^O i 244800 46 4 1 03 a 63 7 *P V8 I 151 0*02 w Ook 0 3 -0 a A31 . v60 b k 0, w 8 b a. 408 t A 7.
OF poojv^ QUAL64Y A-9, I YOUGHT L.S 6P950 M IND WXNO • AX^S RWN 49 I 1346 OUN :89 _1i l!g/m Tem p 634 PO 14#6071 QPSF 7 159*9979 5 * 00 VFPS 253#07 RNPT MACH 0o4257 T01 T02 T04 T04 T05 T06.1 I TO$ TO 110 Q, 702 0 88 0 Q 0 0 Q Tit TIE TO Tl# T13 T16 TIY T19 TIS T20 I 1 0 Q Q o- 5 AMES-iTYPS SUPPORTS+MaDEL DATA 'AT CoGo __ULL SCALE DATA PNT -ALPHA 'D/Q *Y/Q RM/Q I YM/Q PS I '4/Q . Pm/Q : 1 - -0905 -0*, 03 -1:.933 - 4 -700 26k12'. .6267 70,34 - 1 2 &23 140700 2 -no 6.29 «g9 as 0 000. 454000 o p iuo 1.
*0f83 •1 3 w 3099 w 0v , 03 w140367 iS•533 62j,93 1 442 I •9wag 0 0 03 IUV25 pg3q 4 0 607 N O 03 w2og300 1,60333 . *3 741.43 N 01600 11 V85 5 '*7 0 90 - 09)0 3 lo?,S o 200 17#327 83051 160 3 q - 02
wio' 1 03 wom03
6 * 2 ' 1o567 13081 8 186907 65,24 .6, 16 0 0 0 ..1,, .487 7 •oi2*00 "003 33 # 333 824 2.O t 340. 14 61-096 *1 340. 59#,10 0 t 000: 1 7*01 -00, 03 w i#600 . 14 o 7 0 0, 2077 . 160 9 2o04 *003 14 # o0#133
3 # 533 4 A 17# 81 6.00
. m. i o I '40#.03 mJ89,34 14067 Of1,33 *v39 1 0 4 00 1 8#00 i4t,65 il 5*93 "0*03 12 # 500 14o*33 ?,C82 018980 0q633 110.42 ..12 80o1 X 00.03 16a967 146733 10233 wi • ,73 - m 18 # 71 ,, 13#88 13 9,99 - Q # , 0.3 21,o-Boo %. 5 # 3;O Q
1400 1- # 4^3 -*,^,46 - 0 14-9 8
14 1. 1,2402 X0.03 2 -2r14' 2'5.91 7' 169240 12 0f8ou p m 8*70 «66 1 4 ' •1 , 6w1a 1 2 0 a ol -0,*03 •900 4 k* 633, 2 5 6, 25 MRO t 1 ; l 3 r15
0916mm
of pooln,, QUAL"" YOUGHT ► mw WIND AX2s : RUN 90 RUN-- 0 0 fl141918i 13 !46 TEMP P6. !**6071 68# QPSF 10000 'YPPS a54028 1575923t RNFT MACH 0^2257 ; TOi TOZ . T03 TQ*,TO a TQfi TO '7 .09 TQ , $ TIC - T 0 0 0 75 0 0 0 0 0 Tit T14 T13 Tl$ T1.9 T20 %4 T15 %6 T17 0 0 1 0 0 1 0 0 0 +M=F L AMESaTYPE QWPPCRTa - - - a AT C.G. FULL,SCALE 0 P SI I im r)./ Q3 pm-In Y-/ 13 P.M/ Q - ym.1i3 FNT ALPHA I 1 000$ POW03 "J**OQ 10933 ' 10 01533 7t34 -10*60 6*46 : 2# 03 0 # ^ Oa 9 it «367 3,,4 4 W OR321 -11 •'47 2 - - *7#633- f 45 3 w*,,03 w0s,93 wj4 # oOg :j2s000 58s3a -0 t 3,12 1, e'21 =8*72 * 0#;60 * 6*06 -2t 6o w0O03 m i,9 q , 9 33 12 0 - 9 00 7706 - 4 0033 *7 9Q P * O , #,03 1 1 #, 76 1 , 961 ~24 #680 -3 83#67 100 "1O 6 7 6 w28#833, •+i0 +05 o0 c03 62 7, --- ,68# — #? - 0 - w f 087 5 * 8 6 i15 *04,0'3 7 U11094 433 9 , QO0 X 67 13492 17 s 73#20 -104UQ 0.48 a W OPOO - 0 .x3 7t2i J 6 ? J •967 % —0#567 •j0• 1 # J + 47 i917 9 2#00 a p 0 w 0 3 700 6 ,0 14 0 ^ 19*709 7956 -0 1 53. t5i io 4 . 0 09-03 8#413 104633 3* - 5oI5 " 1 6 t, 34 63 -09433 It 509 w 01,03 12#600 10*567 01033 3kll *16*60 01 c, 018 t2 8o01 *0#03 10 * 333 17. 133 ao,6E;. 0o561 - 0,156 .
13 909 w 0&Q3 29 8633 #733 6#733 w3 *7 9 P13*03 1J e647 2 s'L 2 4 14 -12#00 - 0 w03 25.467 . -4 92 0 x2#400 019,71 . 0 533 , =6•82 35 000& 7% 2 & w , 9s * 6 0 03 a 10967 i b. 3i w oi600 L , 2 C0' — I 4 A- 9 3
Or^ P052 QmLru 7
P15 ^*#,607t T E MP' 72o PNT ALPHA P S I Q/Q 'Y/Q : PM/9 . YM/Q I./Q PM/Q . 1. 0001 awl, 29t , 16 v3 : OQ V^#360 :2 1 tog 54173 01590,7 6 7 0 4 i p * 4.7 .,.4„ 02 w0:, 03' : - 4130500 :12*267 64 r4g 55Si3 41. 2 ' 6 6 3 *43 4 w 6o05 i m 13o333 - 0 f, 03 20q000 1 socis wl - 82 0.05 4t267 63 # 13 5 ' - 70,30 55'0;35 i 1 0 0 & 03 Lm24 1, 8 87 . 140333 n 5 4 tj 9 5.
940,45 - 419o0 6 wiQ o 05 -00.03 Pm28020o 67#49 - R 1 52 «6. 9 1 6s18O 71,30 066 7 w i 1 9 a 0 * 3 033 • 7, 0: 3 33 17 500 . 40 ,8 67. 7 5,45 so 15 4 -, 70 .
0 . 4 wo ok 03: 0. 0, 99'*56, w1 5845 4 9 , 0 , 5 10, 43 :9, 1 2 0 0, 2 2 .0Rp3 00 - 11 167 22*43-lil5bwoo 9 1092 ' 3# 8 'JA I 4902 W 00O3 80400 110067 14,02 8150920 40-89 '!-587 li 5098 0 0003 12 4 500 10@873 04-90 .,S00 8*34 m1450-02 .12 8001 -0#03 '17,000 9*36 7 -1*93 *144w19 110400 *#37 43 5499 w o o , 03 21 ,o1, 6 7 46'a147P26 11 #967 - 5#57 : 51 0 3 20 Aav W Q i3O3 00 ` ' ;333. 121 4067 -140 2 t"4 6 : .
0*01 0k03 67:: 11+ # 1r 4 362 20*92 547 95-61 415 9e11 Quiff fY of: VaUQHT Low ,SPEED krTND TUNNEL: Il_si"f : 630 . — TEMP 744 PO 1446071 75*00 QPSF VFPS 255 , , MACH 0.2257 OZ, PNFT 15535'3.58 .
TOl T 2 .'CO3 T • 04 TOM 'T06 yoT TOR 10S T10 702 0 0 0 O 0 52 0 0 Tlt T1,2 T13 T14 Tl5 T16 TO T18 T19 T20 AMES: PF4. SUFPORTS,6M5n9L ;. MAT A _ • 1r C FULL_ SCA 9 DATA rt Al'T ^ nun 17CY - nu ^ . ^ 'V 1 UM-/M I vMin
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4 6+04 -0401 wZOo 200 44*58 00 16F700 78431 44747 -1444.68 5 w ' 7494 *'0401 r25067 54471 x'1394.84 '174433 85471 41400 6 w10.04 0 04.01 614.01• ^+284^47 _ 194267 3497 K131+.98 .
644,87 _ x ., -411 #98 ' • 0x01, 69 02 .43340'47 2.0450) 4 R 1340,a0 64x22 4087 .
: 01 0 a — *0 24«i0 02 -1#533 1501 67 '28!42 040' -0139&84 , g • Oe.01 lg*16 2 • O9._ 3.300 1 1 49933 20.78 4 213 , •;i34^83 to "Or01 841,33 12x35 wi131*65 4+00 •144833 1,6421 40333 SkS4 li 5499 0 0+01 124500 1 ,1 0867 14x35 44747 x+134420 1, 4 , 12. 8901 04.01 90 16 4680 1 .5.447.. "2 6 134 * 9. ^-
15 + 151170
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1.5 0401 • 04.01 v1 x567 r :0361 , 24 `52 1 4100 27478 ^131,:70 rte, L -j __ j - P)r'c ^" b\^' ^u p QUr&Fj"J' A-95 •D/Q RM/G ' YM/Q lY/Q FNT ALPHA PSI z PM/Q 'L/Q 40*0 a -0, 0 00, Imo 0 1 2;4;47 w 135*48 1 . , Io s 67 15 a 347. , 27W .
2 : *-9 # 05 91, 4 •Q 01 ' ,i ► '15~633 42.
7#7 00 91 -Otol mi4v 133 69's a a 109 16, ZU AA 72, 3 4 #5b0 43w66 -1421 4 -6o06 0 0401 "0033 16o853 0 60 77*20 51#70,1, *137*94 5 '-7#91 '178767 841 1 41 1 4 4200 w000 1 -w 2417 67 60 *35 p w i33sQ7
6 wi0*03 w 0s01 w28oA40 19 * 400 78a5q I 3t9O(3
0 00 033, ^ 6 . 8 +, 29: 133 1 e, 3 6 * , 01 3 . a 0 . 9 5: 3 7 ' Ala, 2. 0 9 - 960 t 60+'877 p 0 q) V O 24. 33 1. 3.$ o^ 5 6- a Ol 2 wi t SO 15*4010 ^^ : -PTo! 22 41 Ul ," Q 1 w 0 ga
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"1329 . 58 10 03 w Q 01 $8233 4!167 1. 1+.81 4. 09 149947 1 5 9-- 4 9 5#71 *130#,01 .11 5#97 w0*01 '12 # 500 15#067 12024 41540 w3o.01, 2 1 0, 8"OQ -0401 i F oi 6 3 32 l4t2p- 5633 3 -(133.
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QPSF 75 *00 0
'YFP9 258 r i . RNPT
• T i0 TOi T02 703 -TQ*.T05 T06 707 706 Ti:^ 702 0 0 0 0 .92 • 0 0 0' 0 T19 T20 T11 ri g TO %4 TIE T16 Ti g p " Ti
0 0 1
1 0 1_ 0 - .AY.
SCA LE- DATA 0AfiA C LLL AMES-+TYPE 6UPPCRTS+t0b9L RMIG 'Y/W YM/Q PNT ALPHA PSI L/Q 'D/Q PM/Q 4.567 26005 X146.26.
0#14 00001 151333 1 25#57' 't1^1P,`^B 310 64 ^1,47o55 00k.01 47, asb7 4^9`^3 -gs. 04, 00_ 15 ^.J*351 '^ c'3 ,,
49s 58 a.ti
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3 4
,4,7,,76 49.,58 0 ^.0 000 # 6.04 P209000 @ 933 16 74e ' iO 4 573 ^ cIB mi47«37 5 ° 0 91 0•.01 y 24• g k$7 800 -7#90 '17 o 2i+51 ► 65••74 w142 4i -0001 4«220 6 wi0 05 028.33 1 3 19.487 62.07 72x96 4'30Q *141t2.8 rQ.01 20.833.
I .i12 i 00 •13219 3 3 61 *28 44067 .:, 2'S 92 mi,45.12 8 0-02 X0.001 250139 t600 1501433 .'• 4.73 2G *48 . 59.97' 0'142 tU 9 2.02 0 *0t0'1 .1.68.x# 166167 9wVs 13+•04 * 0101 $•267 15.000 141-39 4++433 10 4902 6«75 -4138e-23 % 4t807 5.99 0901 129467 15ti00 12025 i1 -1*85 -1410152 5o667 8.01 -0001 14.92 12 16.900 15.333 r 6tC10 -144950 9'•98 2'1.367 16#033. '1 05 7 13 41 0101 14*95
13181
5!567 1'42gS1i
ORO 11.78
14 12,02 251.373 i6r:900
.*. W 45 *05
0.02 24..93 4 ^ 5^8'
13 *O t 01: 15t433 264"8
-1 a 633
is TEMP $6# R0. 14#5973 •V lrl dwi 0 • ym/n ; PNT ALPHA 9T 0 If Ix .3.01 Or00 *• 0 9 994 411.3.9467 j^^o•o 21.335 5+369 26OZ ^f9 o•o -0,9 4 2 .z ^128ios #2 47 : : .
''1 0.02 4s02 24•Y6 iav =1.1 1 15 21_355 * 4 •'27 • 3 9. 69 ._ 3 -6.00 C 4 0#02 *0.512 '-71669 21•;82 :,094.17 219620 *9147 5 0#02 -7•'99 19049 0#608 21#898 +X131307 •-63.61.
-18942 0902 -109.02 1.446 22.964 -1 9 018.766 21w09 ;#35.•54
7 0.02 -142:00 up ..-=3.,21
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16 0 # 02 0#00 230.82
-x•934 2.1 . s 416 5092 -39,60 *139«24 *33 17 0.02 2.01 9 •ft(138 -1.114 21.572 -4100 9 157 21 9, 49 18 23•,83 0002 309 -0.813 21.554 -9182 :13#1;99 *1531,49 ._ 19 0.02 - 28035,' •198.12; 6401 0:.331 :22.2:33 7'9,99 -20 0#04, 3*4--08 •213'99 ar663 22 578, vw 339.9p ;22.38.0 0.02 10.01. ► 239560 3'2.,19 •+229..36 1 837 *48.34 , ?7±.146 .22 0002. 1,2100 837 319.89 •253.78 3.042 •24.608 -58.20 319837 14101 23 0402 !68 9 , '37!265. 30•,06 -9282963 49337 26.114 52 2.4 0.02 16.00__ 26 426 5.392 - 27,169 -67.44 . 4 19, 849 *309.:83 - 2 0.02 1841,01 23036 6f02it 299,367 '-75!74 -466, 37 -3379,59 1.99,99 26 0 . 02. 6.:898. 31,•>95$, 201 19* 6 4370.5 6, ..
: 2'2.091.
27 0.02. 7.952 34.940 -92.38 71289 20.:56 *403.72 28 0.02. 244.02 9.066 1804 384102 -108.81 629 7 428 ,64 0.02. 26.01 8.705 :621355 19..21 42.440 n 86x72 0 -360128 0.02. 2F1•00 9+464 459934 -88.38 66#6U8 -4380,01 -26916 -,0.
0.
Oo'c: fF36 9 04 214'536 41392 2 *ia9^75 X4. 34 U R 10 1 NA L P [^ A-9 8 OF P002 aVOUQHT LOW SPEED WIND 630 TUNNEL' TEST WIND -AXES RUN 96 RUN .96 11/19181 1346 .
TEMP 856 Pd 1*0'5678 QPSF 8340 VFPS 272f14 15903969 MACH 0*2378 RNFT 10.1 702 T03 lQ* TOS T06 TOY, YOS >U9 T14 702 0 0 95 0 0 0 0 U Tit Tit T13 T14 TiS T16 7`17 T18 T115 T20 0 0 1 1 0 1 0 Q AKESviTtPE 3UPP0RTff+M0DEL SCALE DATA DATA 'AT Coat FELL CO N T Al PWAL PC T I n T i in r*, O M J Q y I f. 1 0 m I r _ l l vmn , .,. , l I __ ► Vr 14 r 'm & Ir — I lif NR I.r — r- f 1 0601, . 26059 229470 "133 1 0000 m Q#873 4 0 95 40.307 .
1 P R t. 4 2: 0 01 02 0t 723 :22 199 0 68 O St 24*26 : 7 a oiot - 4 x00 0 0#331 22 38d Z!oa 22,9.82 99.,62 4 w 6901 0901 20 x20 OR392 :22 .530 -6988 w iO080 f 14 '-7 7' 5 0001 , -86, 00 1,386 239l63 6!i59%5 47i62 -13*70 22%.32 6 0 o 01 -iOiOO 2,072 24*006 w w209873 229-00 =23*.12 18 * 13 7 .
0401 0 12400 29892 22. 73 25.181 6259572 2 24046 0 0401 0 14400 584 , 2643 i9l 251x7 4 3 9 584 W 1 71 94. 27696 m t - 3 0#0 12 - 16 9 0601 , ' 191 3 0: 97 4.639_' 28x430 -27,t 7S %35IC66 97 Oloi - 0 1 a c 0 2 5 * 633 31,#066 33&05 890,36 w 37611 i s 39 v 8- 8 0 ii 0601. 0 206,02 36 * .13 118f;36 6,867 33.319 -49900 *4 4 9639 12 ofol "22801 60o16 4691 5 66 31&74 jp , 7cj5 86042 35. 1 470 n 13 06Ol .-24901 '38#964 at '.52 #ISQ427 4,675 '-78140 015 i-0 0 101 6. 01 O t .4026 12 , J ++O 4 2 61 99 ' 092195 *5515u4 40 92 . '170x56 15 0901 1.4,934 45.663 m106v,90 0609-OUO 3*#-30 181*,32 0001 49458 0 0 0 1 -09843 220440 6940 27-r5*.,m1349*1 1,7 9 0901 21928 4138o,,23 2 00 -iti45 291660 7*12 B9825 18 0601 402 226819 21•2 wi52614 06904 00 - 83 131313 19 OSOL 600 w0 * 181 239193 1 81 5:30 - 1,93621 "9974 E9 0 - 90 20 ofok 8600 0 9 783 ;23•.6.1 31197 : 4 o217wo0 -21,1,78 2 3 073 21 0 x 01. 1 0 0, 00 2 9 d48 24#648 w 38*65 27#9;52 '29 ol 9 u 423 2 *:33 .22 0001 letol 28*;70 3@373 *255610 2 50 331 -51175 3 2, 3 80 23 0101 i4o02 . 4 9 295 -62#.24 269416 36t639 26*. 53 0279942 24 0 * 01 161Oi 266,16 54289 27,922 -71924 409504 m304•08 25 0904. 1 1 01 6 # .639 25x 299518 ' -70#73 . 46025 OR 331 l , 92 26 OtOj 20101 ► 7 * 651 329.289 -76997 51*717 2 S . 5 2 4368,35 27 0001 22tO2 86705 '359392 25 0+6 00 9004 '57#223 223 0400- 1 -68 28 0.01. 24100 10.265 38*620 miOPa88 :629031 2.3 c 4 0 X426922 29 0901 26900 .62 i 633 101723 m84917 "991 15 "362617 4 , ,91127 -84,88 0 001 28 900 116205 46#819 66917b -16 9-72 -377o^66 0001 0601 -0 1 8*3 28 9. 04 221440 3o73b- 7c69' -4134 , *17 A-9 9 OF I 'Y/Q KM/Q YM/Q D/Q PM/Q PNT ALPHA PSI L/Q 06 0.0 1,5 °# 1. 19 145 6 7 067: 27r53^: .
Z 2: 0.05 Q4,01 *7 # 867 2: 15 #7Z0
o:L -L-
. b:3 5940 .3 4*ol 0*01 w13 . ' 8Q0 16o267 6 1 49#;23 164500 6@0 1+7 815$#41 4 w 6v05 0#01 78#65 -q19&767 569,49 64080 mi58#64 85q.58 5 ' om 7 s 92 0 4 0 1 w24t7 3 3 17o820 65#, 92 "161*28- 0'qo1 028 * 533 74418 6*4 , 5: 6 w1OiO4 19a367 3 , X32.8.3 613 7 0. Q -2-07087 3 0.: 29 :, 8 0o'?. 1.42':6 .'15#4.00 a 26«83. :c 5 .
8.01 1 5 20i551 78 2 2 IR - 0 9 Gtoi 4033 : 4 13 5 14t03 oi36+34 0*01 8 9 367 4#713 10 4001 15#133 13o57 7#90 X133*97 li 5i95 Qo01 12#633 15*087 1is - 55 1 +48 1 *7 a i t 6 1 1 0 139 wti+ 0001 150400 I a ^ -Lt- 50547 ; iE 8001 17sQ33 .
40% 00 .9 01 2 1 5..33 150967
0.1 ' 16 t 60 5 42 6.7 - : -0*61- W 4.3 9 2'
0 25490 G 16. 7 0,0 1 .
- 43 &4 ^ 1 0.01 x• 1#66? -15. 4 !^O 6 . 3 30 104 15 0#01 .
t Xa QUAUTY OF POOP, A - 100 J- VeUGHT Lffik - SO TUNNEALIV%1-630 AXES WIND RUN RUN 99 1 13" , ,- 140 , 653L p d TeMp , 739 t 2262 1 MACH GPSF 75#00 . VFPS 454-vo 95 TO TO?, T03 T04; ' T 06 106 107 T' 8 TO 110 702 0 .92 0 0 0 0 1 0 T15 T20 Ti* T15 T16 Til Ti8 Tit Ti2 T13 'F'l LL SCALS QATA DATA AME-$^TYPE SUFP0RT9+M§ -pEL 'At C#G*; RM/Q YM/Q D/Q 'Y/Q PN N T ALPHA P S I L/Q FM/Q ^!134^2b q.1 0.01 2 8.: 0 9$0 :7 27037 O 67 4567 0 , 2 i f 5 5'e-00 E7 ."86 o 'I S 2 7- i36" * 'R6 404-, , 0 4 01 07 *467' -, 2 0,09 6 ► 39139 " ' 1 - 4 4 5 - . 78 - 1 4 5 9 4 W 6006 Qtoi vi9 * 900 16*96 - 77 ^ 2!5 33 52o , 15 "146#31 5 '-7 * 90 0#01 "24#667 : 8404o 5o767 17 o 8 r 10, 45 m i 1 5 0 6 U 6 w10o04 0001 028 * 600 4 1 6 1 _6 o 067 9 a3 i 66'%45 6#2Q0 - i lSl s 27 0 1 o*01 12- $94700 20+.980.
27 75 .
0.02 0.01 4, 1707 8 1 3 4 74 »x.304° 15.467: 27 s2 5, j^ 333 ZO'P6 127 09 9 2#00 0 0 2,667.' A * i 2o 096 13*89 4e467 12637 !128«33 10 4601 0001 8 * 333 15#013 5•,66 ^127P00 j9733 11 507 Q101 12 ► 667 154067 11o51 -3..06 1 . 55 .12 50273 +#13 8000 0001 1 7. 1503-7 1 00 0 *56 I R 13 6 w +' Q 9 13 9,99 Oo,01, Zi 633. 15 1 . 7 5 7 d^ ik *SO 0. 1b05 5x !;33 26 w,70 -13501 w -0i . . 4%.433 , .0 0 w00 16067 7*^i jL7, .. . ...... .
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R UN T99 g L82 .-Z3
._^rY-3 .^"r: 14x5531 TEMP 73# Pa.
MACH Dr,2262 75.00 OFT "1554345• QP9F VFPS 255.95 TIO Tng 705 1 ug Tor TO T03 T04 T O& , 0 R T :$3 70-Z 0 0 0 0 0 0 0 0 718 Tl$ T20 Tit Tit T13 Ti* Ti5 T16 T17 0 Q 1 1 0 cam.-.^. 0 ^. i _DA TA SCALE
0ATA `AT tag, ^Ufj
9iJRRORTg' ♦ M^ k E3:T1lPG F^.
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(136v93 3e607
09,,0 i 4 11.4 933 '4075
-2.09 1 3•:300
. sy ► 435 •1*_4
- *Ql . 65.1 i0b 40
3 O•0 1 .1'7. H7
145 ._1k 61767 4789 1.87 4 x+6•.05 0001 d20e967 97x89 15*667 55 x 3 1 w i60x4 9 5 0#01 16x5 87 7e073 (.- ' m 7.90 ,22.993 i01 44 671,40 -169'482 QsQi 9801{7 7°433 6 m10t03 wa4 t!P67 '17%567 - - 73490 4172.70 97.24 79too 7 ,12,00 0.01 M25:467 :18.833 .
36.20` ^ic9«33 ; p.p 8 0 01 •9 680 13^^6'l 15.85 W^ g 67 :: < 18 x'55 nl29.39 0 of ' • 2 .1306 al 06 9 1499 6.067 ^ 4t 7°80 , 10"455 4.633 -^129r42 0#01 29.66 10 4.02 -21667 12e933 "132.63 41667 4«374 5.96 0.01 0,567 12x667 w 47e•48 1 -2a93 +e1370-53_ OtOl '12i5 t70 w6a *, Q498o57.
12 8.01 ;+6067 yi36.16 •13 0' 01' 9.93 7* 400. '12.700 -90494 .; 38:•60.
11.133 :23x200 14 Al 09% Q001, wi15004 •41$.1"e16 7#206 2:5«35 t$ G•'OZ =001' * 10.'367 , 13 22. 1k C.^^ Yrt^ G^^ ^^y^L pJ 4L•M^A VdUGHT L-MW ' S P EED WIND TUNNEL Tq_630,__—; WIND :AY25 _^' RU14 iQ f / 4/$1 Z34K RUN p 144,5482 TEMP 84 9 PST , DIG 'Y/w RM / Q ' YM/W PNT .ALPHA PM / Q . L, / Q 22,x39 ,- 1 280 2 4 4* 085 99,04a
1 ' :0001 otQl plo*750 23 4 78
31*36 1l^Rr^l25 . 109,118 4;136"vb4 . 0 2s0.3 09,01 +.14.500 509,51 38'.6349.96 001, 8'3'0 540 73s^ 11+?7th
3. ; • 3.99 jil7. i t
41639,57 45,71 4 w64Q4 09,01, 5 1b4430 934.10 '121480 !•209, 91 54«84 -+190 *65 5 'r7v90 179,01 " 23 # 245 17+460 1039,36 13127,5 759,16 m.496.,32 6 09,01 .25.780 1 6550 118•.35 13*765 w:10.05 <.
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-t1^86:26 7 •r11s g 8 { 102 *27v 680 19s7^25 k 13r':69G ' 9,2*o91 23^$a6:,r:1,28^9i.
0 ► 01 OtQ2 w104625 * 075 ' ' g i7'«35 n x .24.> 9 2 * OQ 0.02 0 7 2' 0 00 13.600 0.76 7^ 1 0 5 9« x!1249,.13 4#03 09,.:02 w 39,450 13*350 m 26«04 79lib 1.96 -!226 42 6.950 11 5.98 0 02 -0#150 .130120 -48 9, 04 6*900 375 '13e625 x 68970 -5w38 ?1251 89 12 8-Ol O *w O2 .. ± 97' 6369f1 :.*1.Q +x'.L30•r58 13 00(3 13 - 10.00:; 0t0P- 6075 ^91• g 5 .'.^' 18 6r t266 0'7' 40135 825 04:Q2 139,.40n.^+115^.5b - .4 12400 109,.600 : 23' ^55 ^^" 129.98 (1r 0'2 •14.1'75 24s,16: 90.2i ' , 9,:5 t1.RQ1 : i0 .875 u , A-1,03.
. YOUGHT Lmw SPFEQ WIND tLINNS 1 TEST 630 - WXND-AXES RUN :i05 gut 1*t$875 TEMP 63 * Po QPSF 7500 ,,RNFT .159392 5 0 MA.CK, Q 'VFPS .453t : 24, , A TiA lic TOt T62 Y03 , T . CJ 4 ro F L- ~06 'I 0 92 0 0 702 0 1 0 0 0 TIT T61 '5 T16 %7 li8 TI9 T20 T12 T13 Ti*
-TA -t fU -r SCALe l Wi
I YPE SUPPORTS4M &MESI^T kf r Al CLIA YM/Q 'Y/W RM/Q PM/P JgJ35 : I K 31 0 26*45 94aou - Q 01; G Q-1 ' ,32x3?
0 , 14 GiOl a 667 -142 1 47 - ; *Z67 : 4 ko 9 3 40 p,*331 k o:*+Ol * 14 * A 0 S' Z igl 1 271 4, 0 t 8l -U51 i 0 j 3 t- 3 479 , 76 "164t-8* .12#433 4 "6005 0001 w20#03 17*667 72485 56&98 -4184,92 5 '-7#92 18#867 13 q 500 7'7.!60 0 0 0 1 "24,793
w194* . 06
00 96o2g 13s233 71i47
6 v o lQOQ 0001 = . 30vI33 204
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, 6 .11... 60 67 2 94 Ol k, 0 1 , was 8 g o *e,* 14 9 8 0 46 .
8. 0 13. 20 iSD +!127•63 01 - 0 2.94 0 i5.33 11c72 -!121t,82 Otol 70-33 io 4003 13#71 747 0 0 - 1E 5 6 400 4,45 15OE00 7.840 - ! 120-16 il 5#97 0#01 110800 10009 -30, 95 -i2l.20+
67 151 , 720 1o§50
12 SoOO - OeOl 16. 3 8 , 053 20. 740 1 , 6 * 353 ;' 8 X 200 '12:7,.06 .: 13 10#00 04 . 13 , 404 80 :0. woo. ^ 3 44, +iz 9: o 00^ 1207 7 *233. 1 51K, Ot I88' 65 z V5 OtQ.0 - ; & 3 24 ^a 13 4w,76, 0# 02 2 #633 1 5. 99— : c p D^' olu OF pocsp, QUALITY.- YJUGH Lmw SPEED WIND TUNNr-L TrS W1Na :AX'2S RUN 102 i /'1.'9/81 RUN 002 ia4g TEMP 674 Pe 14w5875 Q SF .. 750VO 'YF:PS 254+21 MACH , L X2'259 RhlFT, 1578645t :.
TQr T' T"03 I T ' 05 T06 T07 .'DOE 1" 0 5 'f ilk 702 0 .92 0 0 0 0 0 u 0 T11 T20 T12. T13 T14 %5 T16 TO T19 T15 1 0 0 1 a 0 0 A'MES-4TYPE. SUPPORTR +MODEL 5CA E ; ^ UAIA. sT` °C.G * FUj.1,` PNT ALPHA PST 'L/Q FPM/ 47 ' YM/o D/Q PM/Q Y/Q 31...
1 tlOR 0.00 2x533: 25x20 ^+1^^1 ^E•$67 400 3605: .°1 5.
x 2 0x070 ^"'.2«0Q: ^8rb 3 s.83'S 48..86 9%96l' 320*6 ^+2?$r.32 1. r ...4 0 flrOQ 3}ai064 w148678 02 w14•b01 . :16.433 4 -6x06 459,56 m41620,33 00209313 170320 75.74 :129293 5 0 09 , 00 530,98 7090 "24.740 18«547 77081 i2tEUQ *175o,58 6 w10+03 0000 *29 * 200 i g086 68184 120973, 86.,66 M391•-15 l % 00.00 035,.:^_nn...
7 X1.2 0, M 37 a1o473 : 9,507, ii5t2.33 8. 0 O'4QQ 00 2 15 4 36 6 R4«970:1;129` jf6 7 6 8 8 ► 14 9 1099' 8x0.60' 19 i 57.
990 00 2.967 15•zt7'0 '23x,64 =224•f.3 10 4.02 0 00 7.600 15*067 16033 74733 10%28 ®1i8x44 11 ' 0.00 11,x.967 2ti$ 15x100 130 . 56 7#067 -!116v87 12 8101 16, -5%98 0000 33 8 .013 •Al20•-62 15.433 13.81* ; "12-i4.7 c3«OQ 13 "' 9x99 20,733 1,b r.067 '&tCbl; r1200P7 1409'3 1^ p 0:foQ .!16 11099' %G:iO4QQ. e5t33 :-g6t 0^} 14 68 71200- 1$3x82 ' i5 E7.02: C^'!QQ ': 1+2.70Q 15 y 433 34 49 S±r5,93 24'A5L 13:1:x99 '."
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* • 0 # 42,7 .129 1
0400 18f767 77 .68 { '07, q91 53.,05 dl73.-69 a o 0 00 0023,307 X1, 073 80, 55 :12o700 66.85 f ^ 96 0018b.,62 b ,w1 0f05 0.00 0 33 7 X27 8 w `12 •_ _ 719,85 01.82 sl12 iQQ +78 Os.OQ w31.773 23.+473 88 13- t 407 962: 23. • .13500`1 o t of 0.00 S OU0' 53 - 2033 16.2.67 36.00 16161 8#63: 9' 2002 00 , 00 2 .a67 1 5,e8 ,129048 u X3..28 X125,•23 0,00 14,.73 8.333 10 4e04 2#200 15,867 .0N69 80307 0?1,23f,24 it 5198 04 , 00 13 f 1.00 15.900 0012 2"349 00 igvo4 8f5UU *-*6 *75 .12 8 0-00 0f i8rQ33 16+367 - *13.75 _1G* 00' 0.00 8+=433. 2.7.87 13 .2:2.60Q 161,833 16899 ! -17•b7 w1.29A33 14, _00.00 1.74 , is0 79533 .51#9,9' 27.033 17.867 23 s'67 9 e^2 00 i 131.91 0.02 0 *00 67' 16 +233 - 34:.• 75 -2.9 : 'Or PG55.' QUAL87Y A-10 sPEQ VOUCIHT LAW WXNO.AXZ$ C R IWI RUN 104 po • 1;+*5875 TEMP 7$v ^256^ ^ MACH Qv2259 IjP^ SF ^ 7$•0^ 0 ^ VFPS - RNFT iSWIll* t13 I , TQS 1099 Tot .. TQ2 T 03 T04 ' Tot Tag 'to?
7,02 . 0 0 0 0 9 2 0 0 0 T14 TIS Ti6 Til Tl$ T19 TZO TIt TiZ TI S O.
SCALE Q#TA Y/W RM/Q ' YM/Q FNT.ALPHA ? 'Of PM/Q $ I ^ /Q 21 *86 i , OsioR, 0 v QQ 6 24067 16 4 100 2509 5f5 O -1134630 41 # .76 5 613 27+:7 - t 1 3 4 9,4 0 0 wOO' -8-033 46o660 a '-2003 3 5 - 33*36 3 0 2 13 6 6 7 9-227 6 4 , !^L_ _p 6 6 6 0 #,,,0 0 . 11 , $ p -q t - 4.1* 39 . 09 *6x 07 0.00. 76 t93 5x 467 wl.9 OQQ 18067 L.
5.9 412$908 43 .
4-0oo 6 1 0 1 0 -# ol^ OoOO * 26ij13 2i +513 x.7,5 .
56f10 vqi26623 * 233 23 7 mil2s . 01 0'.0 , 00 o 30 4O ' 72 , 27 SPOUQ *134%32 '21x89 0W00 "1 ' 933 a 0 0#00 16#060 26,06 A V 6 3 15828 1 3 2 •d0 9 0.00 0200 - 4 5 0 4 4,^ - 2 00 $ #' 08 **31 93 Q000 61 07 to 4 16#687 10#90 61 $#747 0 6 t 05: 3 *6*76 *i32o,42 0#00 13#633 1$*633 9.90 ii 5098 ,13 2. 5"4 *6 +,28 54 0 # DO 18 * 600 16#, 067 6*433 :ie 8000 10620 -lio6S 0, 04 i t 97 ' 17 6. • C 1 3 13, 909S 23#e00 16 , 700 O • OQ 1,28 t 4.
, "I E 5# 6^ a 1,3 1 a , 20 000 27 # 460 15 v 6# 067 14 1202 17o$00 , . 21 ^ 75 1 004 (-.34 0«00 11 +l 24 0 51 15 000 wal 1 33 6«0 J rq A-1 07 -- "JA I Qv P3 ^ ^1 1 1 1 -1 . 1 6 YIVGMT LdW SPFEQ TUNNEL TEST : 630 WrWD- 12PSF 75000 YFPS 256,37 RNFT 4 5461-4490 , MA C H 00'2259 ' TOt t TO& . 70 1 1 Too TG9 TIO 02 T03 124 — UZ 0 0 0 0 0 0 7 0 0 .
T14 TIS T16 Til T18 T15 TZO Tit TU T13
1 i 0 0 . 0
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$7-60 . 6 007' 37 , *63 0150"92 Jl 673 6 041 0 0 00 *13 # 447 6 2'@34 429 . 06 . 0 6 o 05 0000 0533 •140867 9 50887 1-147000 P418 824,09 OiGO 5!733 47 4 r 2a a 1 44 9;38 5 '-7+ 90 m g 2* 2 p 867 86o 16o267 . 84 000 .2s.753 -g 5*240 56w83 1 c66
6 •10 * 04 1$v307 " *1.4
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6 1 v , 38. - 1 43 * Ot w3o * 033 20 4 080 '!$*2 0 7 •412000 0*00 5000 3.3 atfi67 - i t52-•s0 a 002. 0.00 'iZ o 200 1 6^ -m io,367 5.: 0 : $ • - $ $ 00 m i 15 3 w4l- 2*00 0000 — - 3 67 11 o967 14,65 1 i 9, . 6 1 3 90,01 2 -+1 4 8.58 10 4#03 0#00 1 #. 6. 9 5#827 9fiQo 11 , 833 00100 a1038 5097 116933 50967 100 m1459-47 11 14 0 000
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i2 80833 12#200
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43 4*99 O'i 0 C ^ 23 # 200 120833 3@53 • - « , •4 :1? 0,100 5.29 6, v 767 150 77 *137'*23" ► 0O 27.600 13. «733 5qa33 2,6e57 oo15.3s I t 7 15 0 , 002 otoo 400 "1,* .
or l MlIMM is OF POOR QUALITY VCUGHT L SEFEa w ItVD L^, +VEL T^ ^T' :634 WIND :AXES RUN 106-11119 : /81. f,34b FAUN 106 TEMP 88s P5. Iift.58'7ti GPSF; 83,00 VFPS 272+70 q MASH 0+2376 RNFT i58Q4C0 _ TOX T02 T03 T04 T05 T06 T07 TO$ 10 9 T10 0 95 0 0 0 0 0 0 Cl Tit T12 T13 T14' T15 T16 g T 15 TZQ X17 Ti
0 0 1
1 - 0_ Q- A.MES:TY.PE SUPPORTS+MCpEL SCA'LFo QATA [BATA 'dT C.C. -PLLL, FNT ALPHA PSI L/Q D/Q ''Y/Q R'M/Q . YM/Q PM/Q 1 , '0000 27.33 0-o p •00,904. ^ 5430 41410.93 210837 4 7+.04 .
-2*02 . 2'7x59 X1.24088 2 ` 0.02:' - O 21#705 013u7 w 7o 95 -1 # 79 _-27*13 ^_. 3 0•02 1+4*00 -1.024 21.669 4'707'3 M 1tl5*48 45099- . X910,24 .4 0 . 02 0.633 .22,018 7u922 25121 4 13971 n 0#02 4 79 , 99 0s090 22*64 22#440 419,22 12t590 lu64s29 6 0.02 410101 1,506 23,072 -29 # •18 / 2x23 1 8&80 .-33.91 - .
w9*60 7 0*02. -1109 *2.3 f 2 63r 0 4.21 20259 _ 24 9 187 =34,27" 8 , 99 40x57 0s09 =130 *26t8'ol 1408 2x651 240880 -25 53 42411 9 0*02. -15*99 2 6,,8 67 s31s4:76 v35 3.633 -12 t 36 10. 0., 02. -18,01 4,277 m36t512 2!707 75499 29. 1 10 4 41041 11 0002 ' 4 200,05 30+*4 51693 .320434 0o41t687 107s37 -Si 0, 16 12 X8.,48 0,02 . 4 21699 7,892 35.560 oo `128+23 71#6.2_ 0r46s5U6 29438 °152.,73 1.3 0.02 . • 230.98 10.422 ,_ -88t9t 051x75,9 391187 14,. 0,02 ,•250,99 31 64 '172*10 i2,, 669 .<*a*-892 *100040• *^56t657 0.02 "wZ7,#97 5. "1.76,17 44.k64 46.620 059004 38*66 •i'i06*14 21 v*9 •0140..1, 6 16, 0.02 O x,00 , 6 0295 0 0.843 E1.693 -64,74 20-03 17+80 '17 0402 .22001.8 109169 41'41,,08 4 0.994 47.31 18 0.02 3.98 20«74 m160'* 33 4 0.452 '22,349 •14 t669 4 16.9 _ 0,02 19 6000 2901 X020.3099 OtO60 22.801 4 25 .44 . 49,089 P. 0902 °8401 1.s295 23s422 312168 -219.1.7 X39.:41. "24!2 +17 5W99 301.83 21 0.02 2'4.434 -53.Og . !29 1: 57 01239 *22 P.- s 6 2 0 :22 000"2. 4,066 3319117 30,-I1 -m265058 11 ,08 25.602 ^61t87 25,;90 13 " 98 .23 0.02 . "18 t 86$ 029?-976 5#301 '27 ,133 ' 4 70 0 73 24 0 16100 43#02 24 *74 ,02 6.386 28*223 472..58 4 r310'*60 25 S.8w00' 70,139 0002 30#4k22. -81120 '47*0912 26*'10 -341X16 0002. Z04.02 ,52.074i 27o,20 4377000 26 33113 .3 ;, -87.37 7,892 27 21099_ 27.97 0002 8,602: 57#35;; 350843 •10i•35 W4980,29 28 0002, 230 , 99 240.55 042.9.59 94970 39.114 m i14.58 .62!4:22 ° 29 0.02 26 000 10,482 7 63 t 133 *16 *0,9 0358 *45 43.81,3 4 89 c29 ° 30 27*99 0.o2 66,898 .-27.:92 -373.37 10 6217 47771 % 87.31 31 .0,693 2*•27 0*04 210783 46f04 5t633 4140,35 00 0 ^ urn ^'+ '' f r" YHUaHT. LdW SPF ILNNEL 7 Fs r 630 EO 'W INN PSI PNT .ALPHA L/4 D/a PM/4 'Y/W RM/0 YM/q p •t^1, Q-k00 :., 25.2.x' S. •1.033 8•6:60 + 123#,62 4#333° -147.52..
: *.00 1 567 161 ..^9 2..9 22 =i42.k59 9#U67' t` 0 10 8f"1b 3. 1 • *4.02 ;' .
+"2x567 9.313: +193 w7% a fQ61,, 1#.22- 129•&2 4 0.00 -3#367 203$0 33.711 Alit«64 " -6 . 07 3#813 -172#07 0.00 37#40
5 -7.92 *+3.80'0 10#167 20380 +103#46
w i88#20 6 .i0#04 0#00 10x500 02.6 7 00 44,81: -107wi4 -4«500 -203.72
aa.7r53 VfQQ a':3f 3uQ__ fl#,lb,•! 11^^18
-5#467 1.10067 o m2i6*64 .
0'x00 "o, ki 16.7 0 f 03 8 • f ► 73 •+1 24 *0* -146"999 0 3,+ 12 9 1#99 Oai"30 '• 'E7 . 15 3 18, 37' w ; 7#:03- •4' y ^ 00,00 10«65 10 4.04 0,767 4 05 S#167 -94087 •• 1*00 -1439, ^.i1 04•00 1.700 4#367 4-h26 5.97 7.967 -80#Sp rti37#42 -3w23 '12 8@01 0#00 2.67 4#544 K136.66 89000 - 62.47 $,_45 9..15' 0+ ► 00 4.+8t3t.' *i38'.p6 13. $ # '0G 8 it i;40 .6 415468 t7: +00 .R t ± -is.w2S^' m141's^4 14 :12.03 8#. b7 5.
4• . 504 X27."77 M i5 •0.00' p"iQd 24:1:4 -14r8w53 -1.1~00 $•733 ad 24x53 4x.20(1'
A-IIQ
OF UAQTY NOUGHT Lew..SPjEQ_WTijtl TUNsIEL T'p5. 630 ;AXES WIN D !RUN :' _1.08 RUN 108 lilislA 1346 = - TEMP 88 p5 14.•5875 IOCT T ALDum PN I Q Drj 0 i/Q rNrl TM/G TM/ Q ' L QR01. 20,*93 .14807 1 coot 9 000 8 0833 31847 p 1 i+. 12jfh8 9 :. 24.05 ..:140.75 QROii 3p500 . 3.44 !M 1+^939! 9'^L13 :w3.99 ;. 26 «29 3 0 o 0i m2,s 633 9,427 .1,55, i R I 2t362 00120#169 •%10*#:65 4 w 6#04 0101 1#54Q 27t90 m 3, 1}00 9.933 w 170#90 30*76 5 ' 0 7,94 0#01 10#3010 i;#367 w96o-4* w 2#800 K188.43 0101 10800 37#-44 r1ni4si 6 •+10,05 w 4,533 10067 w 205j22, 7 -Pl i; R 98. 0 4.01 w5.433 .11 .333 •219, 02 2@633 4.2 o-83 Im!i i2 C95 8 0*01 3693$ 2i., 1 0.03; ' X0.967" 8.,767 w123#'$2 •.141045 :.
+ 3#967 ,. 4 7*6b
9*533` ri69tA Vs 5 9' a l
U .QtL 6 7 00 49060 9#06 mi,4it-05 10 4.00 1 8.233 m 94w,43 04833 5096 0+.01 JR800 3*26 x+137#38 11 8 000 N 79t29 40000 Ot01 4#167 137v89 12 8. 01 2,767 $,0300 ,..
a 62r 5Z_ s 4 R 347 X7!.79 ,x f'S.o-2* X1.39177 1$ 9'o-99 0R01 3.700 80067 s13`iv97 •1.44,06 14' 0^ 49467 .1.5.99 4i 933 $6 167 - 0 26x 78.
4,• - r — 2 15 Q Oi otol 01 2 000 172-7—ow 12 4 71 3oUl $.•Qi.
1!
`1 1, VQUQHT L81i SPEED WTND T U NK FI ST 630; _T E WIND -AXES RUN l o g 1,1119 /i R l ' 13/ k A RUN TEMP 149,5580 88# ALPHA Psi PM/4 PNT D/9 YM/Q PM/Q 8#867 2f9*0 21 • *7 m t I27*46- .3o,16: g x3 4 60 . 6 ^- w 3 1-3o99 04 01 24667 ^ : i ^^ S o87 7 o167 , I w 93
01r33 _
4 •6008 .
OtOl -3,467 90967 i m 16 8 4 1 93 09827 2 8 # 13 ' 88*23.
5 ' w 7#94 300;50 -82911 0 6 01 -3#900 10 * 367 -w4,88*,53 09667 w10#05 OtOl -4e633 38v19 m84 * 5 1 10*733 -205o10 ,1, +027 ll 7 •!12#00 001 it 1 6 . 7. x 2.1 6 1 #27: 40, t2l X 87'.
W 5 400i I 33 OQ $ 1, oi:^ 9. 1 24 8 6 0 . : 2:1 t7i i Z7' 9 ,.
140.0 0 0t867 : : m '12l '' 260 1 64. 53 ^i 2 2# -67
2 0•'q .-0 # i 00
io *903 0101 7*96 Oo867 8*500 -10%53 -0 921, 78 3#247 otol 11 5#57 io833 3*86 x1209,66 80100 -75*65 39427
'12 810 0 .05 asJ33 s o 5 a !E 9 4 x2178 - 12 2o 77
00 3+8 4"1 9.99:
9 0 13011
#•66 " 7+16
1 3 5'. %, 0 a.
O r,* 4 .7 5 r 003 _0 1' 4.9 *'jgS !
, j 7 2" 83«J& 8,76'7 'R O 121 i4 g 'S OF POOR QUAUTY.
1 > VQUQHT 455 SPEED WIND , TUNNEL" TEsT .630 WIND :AXES
RUN 110 ih19/' 81 134 6 _ RUN 110
l TEMP o PQ J*cs3s3 g o QPSP 756,00 S4Q:t VFPS 260.014 M KACH 0.:2263 RNF'T 1A T10 'T0i T02 T03 704 T05 T06 T.01 'TO$ 109 - 70'8 0 81 0 0 Q 0 0 0 0 Tit 'TIE T13 T14 Ti5 T16 Ti7 T18 T 15 T20 0 1 0 d o 0 Q 1 1 AMESo T PE 8UP'PORY64MC0E oATA.'AT CoG. F . =F LL SCALE DATA FNT ALPHA RM/Q PSI R/Q Y/Q ' YM/4 'L/Q Phi/Q • 0o0c. 0001 1 8,40:0 1.0 *40G -132 $0 2':i7U0. fi1•05 ^11$^55 Z .
; 3004
0,01 40767 1.0o46.7, 39; 29533 *110.;1.8
1,5 E30-9*
3 apt ;- a.67 io,.767 7«53 27-, 66 -ss
2iQO0
K6 g 04 00 1 29«26
"20733 1#493 -92•.75 11+267 - i92,56 '-7890 Oo01 330,10 "6#133 110767 i'R533 -91091 w 2i3e68 6- _alioA05 .
r w2P--^90 I 108 426 1 4 '99 0001 1..g.,0i33 3 -94r , 12043 - •11.2002' 0 01 z.-SS:9g7_ "l.4 w 667 1.3015553. *23'6.91 20a7 43+37 0v0d 001, ,' So56.7 ' 03 21ail 100433' 0133,28 2t . v!1.1s'o32 197 .. 0it01 110533 1.0.533: .12.401(1 E9740 17 74 X121 X70 : .
00.01 -' 10 4902 3033 1Ut4l 14+600 100433 w9ae62 .1118 +193 11 5098 001 0, 10*533 1€463 7 80 171400 ~'69064 '!120~73 -47* 12 7099 0001 20+933 100767 4'x173 -118+.63.
.
9o9It 0 r 01 23 * 800 - 33: ^L0*63 1:1#333 4'!'0 -12I'm!07 14 1 11000;, 0`401 i2o.200 -03c6* -16.',77, 27,^2Q0 4t!a,3 o^i2i017 15 -0o02: 00:01 .: 80433 r133047 2a ► 2(j.22:
10#407 5 7:U'0' *11815
' s rC^`^eL r4^ t ^t:u ^r^ ^^L l^.r • '^^UJ llu)' ^J 'ua^_,^^^ U CST F1Vi^^uo TEST • L 630 VOUQHT Lehr SPFED WIND T LUJt' WIND 'AXES HUN IS Y1/1918 _134b RUN 3t1 —, P E 14 •,5383` TEMP 88o MACH U12263 A:PSF': 75+00. VFPS 259.66 14997750 PNF°T too 7'119 T10 T01. T02 T'03 TO* TOO _24'CT R7 0 0 0
702 0 8 1 0 0 0 0
T11. T13 %5 T16 T17 718 T15 T20 T12 Ti* 0 O.' O O 1 1 0 0 ^^.
IULL SCALE DATA AMEa.; Y 'E SUPPER'fs+MoDEL DATA At C•ti+ Y(le^a FNT psi L7 rs 'D/Q yira RM/Q Fmin ALPHA 17.93 -1409,19 080 1 .. 2ai:25 1 0•O2 w7 * 280 110593 5f467 23.55 143,:03 ^ 3+^,^ 6 1 59,*87 2 0tl3 p:t^ :wi0.36.7 is f C?0 , 73:3 3i^vb9 •^f^^''v.32.
.9, 44, 01 001 W13*233 12•'133 R355r3* t — 34WU9 ^118f:48 -6.04 39033 4 OoOl 12.533 w15f400 wk177t05 , - 7r90 389,.42 1#567 WSQ3.08 5 001 p 0.653 140 -196141 '13 0 449.52 ."90•.53 - -- Ot333 6 r1Of04 OkO1 .20.433 14• OO w213o!56 , ;-5339, 45003 0.
¢' '09a 3 7 x%1.2•.01 O#01 fa23*<233 -15 0 00 0 . 02 28 «54 aa0 6.: :V •Q^ •'^f ^1.1 It,1^^ R: #.. :J^^3:w7 140447..
Qf 01, - •^. 8.7 6fa $.^ 1`-7 X1 . 9,7" rt1'34.32°' 00I 1+'•733 5943 i1Rb2 9 2JI *4o,E67 X103.2!
503UQ 4+24 •(1331,43• 10 0#01. 11 0733 A 859. 54 4f O2 -11573 5#267 II129+•14 5-98 0.01 1#567 11°833 -6602 it w6*83 !i24.37 Oi01 5tO.00 :12 8.00 4.707 ':120000 -46.40 . 12•'77 f,200-84> ' o a &•- 433 4aF67 13 0: * Ot01 '12•327 1 "2-^02 x R71 41567 ^1.1f1i >?122.7^3 0t, Q1 1.4 X 12000 110493 >12'f'.900 w1?^0•'}^.
5x5001 27^85^ ` 163. 0002 6#01, -07.267 111667 _w^;^. X68 r t OF pcllol^-^'%' QUIRLiTy A-114 YOUQHT LaW SPEED WIND TUNNEL T199t , 630 WIND AXES RUN-112 11/19/81 1346 - RUN 1 - 12 PO. i4a,52.33 TEMP 8 8 # MACH 0•:2263 OPSF',75*00 '1429775W VFPS 255v66 RNF1' TOT 702 - T O3 104 TU9 TIP 705 Us 107 1,0 1 0 1 U 0 0 702 0 s 0 0 Til Tiff T15 TZO Ti* TiS T16 TIT TIE T13 0 0 1 0 o '' 1 0 Q 0 -FUL SCALE, DATA AMFS^TYPE 9UPP0RT6+tj0pEL VATA 'AT CtGw - RM/Q I YM/W D/Q . Y/W FNT ALPHA P S I L/Q PM/0 s 1. 7 o'9:7 - 14- 3 1a 8, 6 7 v, 50667 9487 1.:22x.16 25*13 -tOP27 - 1700 -14Z * 99 @-F 2 04 9 67 3 0*03 11.067 'Q 30 85 vii25i10 09,03 *8 #333 11 367 M 4 O R -162*35 L,3 3301 ml10q , 51 0#•03 4 • •+6006 -177031, 2+06.7 6,7 w1io2 33 12 6 000 3408 w98o:49 Uc03 0134633 120520 1*353 5 '-7*92 -201t20 i3e-.933 w2eis:05 1000 42121 mi0l•01 6 •i0#03 01,03 -17s127 . 7 . 1 1^ 1 I * 1 ^ 0 0 01-- .404300 4 * l* 99 14 # R, 6 7- *Z3 o,93 2*200 j'*86 oi*3*37 a -0+03 ! m2 10: , sk- 1 1 5166'1' 0.05 400 -1.23-30 # 6190 .31 0138 108 , O'V.03 7 1480. #13 2: +00 0*467 01104 09 , 60 oi33v50 04•03 39367 10 4004 lio267 mg *i-36 69107' -5*70 -!i280,98 5#687 11#500 --t0t68 50533 -i23#05 -5&76 8e0b 00 , 03 7*980 li#8SS -45#3 5 59387 :i2 -13098 5. v 0 6 7 am 117 t52: X 13 io0o+ 0* 03 .2°40 a25 2 69,7'6: -. 19 ol 0 01.0`3 .1,, . 1 ' s 63 w6ltU 5#133: 1: 9 3 -13.51 l 97' I* , 12 000' 10 0 67: 0002 a 03 .633 ' ; 2 kw 21 5 4131 ido'4* -0 1 43 q, 55 •+2 11 03 3
V UGHT TEST :63 Q
Li5W SPFED', WIND TUNNEL WIND :AXES 17.94` -145F69 6001. 5t867 1 0001; .100333 Y 23 61, ' M147o.16 2 ; 200$ 0={ `t03^. 5s^t9 ri6rS67 33 13x$7 .
>1 10 c^8^ i9 -111 w76'_` - 006?
3 °-099 3 ^0 ` R01 32a7^}0 38 «55 'w21 g &33 310`07 *^i24t20 ,00 6705 00, 00 :20933 4 P270267 .130607 620:43 35::0 5 ' w 7090 04•04 1067 '1!40'92 w3i0700 14#733 77067 d 0.
45 #,53 0 16* 567 0 0 53 6 .10.04 00-04 =35,700 4.8 12: *108k79 349,2"6 .4 ^0 .a.
7 iS4, 98 0tQ* ` n .360$33 150 67 ^1.8«63>1*145r^t9 a 8 (}sQ 0' ► d4 ^01Qr '300" 3 9t7ut 11+06EQ. ^70s' 1, ;i8 •ti 9 200.0 0-04 _- *5.000 11=.567 5 "'25x55 40.78 08133+41 0004 11,.0593 5.•.533 10 4.02 -0±600 ;-39s 4i - 50233 0+74 -!iVoii 11 5098 00. 04 -490. 29 30727 110700 0+596-A <121.67 3 40833 12 8.00 00.04 8,287 .120033 -54wC ^115r69 120:'3 Q4 ^ 41832 *10 .'93 t3. .9058 Ot04 i 1^Cr6b7 51 36 '.
^! 40^8^s ^11a'^/9 S2.Q y 0x04 1302,Es7 450 1 i 4k'SUO 14 !60 00 * :70' e 144' 36 ^'5+t62Q7,
15 0#"44 10s933 isJ
O#OL • 0 GR I, MM I M p 9z i— :4 A-116 OF POOR, QUALITY 'TEST NOUGMT Lew SF!PED, WIND TUNNEL 630 WXND -'AXES 0 1. 1 Q -U J Q v mj m I , - i FNT ALFHA u I r-l'f P s I L/Q 0.02 19f . 539' . 95;
7 6.9 247 12
1 01, ooi 14 P S67 0700 Z :-203 m 0*0 , 1 1, 8 133 : 12 .
0160 45! 79 150 i25: 0 *0 2. : 4 x 7'87 '49 0 45 4i 309 - - w 4 02:3 933 12 i 753: 3t667 329,70 w140w.33 # ,58 4 -1 6*05 -0801, "29o933 13#673 102 39967 q-22 . 84 2#333 !123e-22 -01 01 .03o633 •14000 109o 5 -700 10833 49 &26 W107,58 Q 9 6 w 10 01 5 -0 - k 0 1 x37 . 400 160660 101• :,a 0 . 20 , 49 •122t,68 7 r 00#01 3: 300 O1 434 = 19 412 oM *1 33. &9 18k90: 2+
604 155 +. 7 i
a 0.02 w o i ot Wt 11 # 1 9633 1 , 99 09 2 7 967 1 • 1 1 *2$ v 14 6o, -2: 25 t 260 9 6, 9 200 lo oltol— "6t500. 11*600 6o133 +i67 -141*97 io 4#03 -0401 -1 9 9Q0 11q633 -21 * ,39 -10,26 "135i15 - 0 t 5:867 5*94 0 t 2.393 1,1o733 -36#% 25 11.
08 A133c86 8f01 00001 i ..5 . 00 - - 7 A2 7,787 12,033 -46x25. .
-3 5 4 , a *11-68 v t iV 41 13 9o99 1 O'i 0.1 12. o , 633 i 2, * 533 *Saora.6 59f^04 . oa X17''10' X 1 Z! S" 0, 4 AS t S 14 . 11.98 0 i t 01 17 c,233 13 w 367 ' 15 19e41 X154.57 . 6 9- 3 47 ; 0:x08 AROe:02 wU o 0 6 7. 11.633 20*45 L fl'^ A-3,17 VOUGHT LaW - SPEED. - WIND , TU NNEL TEST.
WIND 'AXES RUN f,15 14UN 115 fl/20/81 0911 1 F0 14*6187 TEMP 74# H O q 2264 .'
MAC GPO 7 1 59 , 00 VFPS 25 6#50 RMFT454882 6 9 : TOt T02 T23 T^ O 4. 1 : 09 Tio TIMT06 707 Tos 0 1 0 0 0 0 ' 702 0 -74 0 L ) Tit g TIS T40 T12 TO T14 TiS T16 Til Ti o 1 0 0 1 ,SCALE, DATA ULL AMCS-YYPE, 9 UP Ft '^A, , "^VS+MdOCL 0 T 'AT, Cka,__-P V/ m1m./n ► xAIY p l-I I n n V DIQ -" It r%l If ^ r^wh I r MA f r- I I I L/Q 17 *154 m R l54w32 : 3 — 0:002 1.1,$67 73 11" • 2 -2iO3 0 4 0#08 pi8. 0 ' 67 42*233 29 woQ "Igo 9,68 i"3 * 99 -0fQa *23 867 1 2 . 9 '00 73x8 2, 2, -41040 3 •11,35«34 13*567 93-09 3 t413 ,07 - 6 -Oi l -02 w29#033 37•. , 92 X1 1.8•,96 5 X 0,: 0 2 m33a353 '-7.90 15*013 104*, 75 23213 48,66 * ( j -109'w58 6 -9*94 N O t02 x37`+133 16.767 9704 1, 1 1, 54,17 -w 1r2Q. s 01, 7 # . ' 145 9 im o r 1 0l 437 9967 19 020 93.77 77 3 r 644167 7 s k. 96 8 -0*00 - 0802 ' 15.92 10*80 ' 0 8144"•'S4 9, 2000 lo o 02 -6*533 .. 700 6s ; 30 6t032 ' 11', 61133 IU*85 "145*37 10 2*00 -Qs,Q? -6P567 11,767 -5o16 w0w!02 "137v89 li 4oO4 w OtO^ -1 * 433 11#867 518u0 #26*19 -1o61 ^i33 •125 12 6o00 -OcOE 2*900 11#933 -39o. 94 5#733 JL; 1 9 *09 0+:0 4 9,07 433:ll 7 907 `12. 1;67 STO 0 — 5, 8 127". 1 4 , - 02. 1,2 10 19 7 3 3 5 3# 15: :6, 17#•85 m153*61 16 s 0 r Q0, • o wl2o040 1,1o833 16o:23' 61200 OF PQGP,, QUALITY A-118 VIS,UaHT LeW 9PEE p - .JJIND TUNNEL, TESI^A-10 WIND :AXES -.IWJN ti6 pd JA^&5187 T E MP 744 m.*(;H o 94R64 : GPSF' 7500 ONFT. 1 5 VFPS,266s5O TO3 T04; T ^%"'^'y o g 709 TIO' Tot 702 ZOE 74 G 0 0- 0 0 - 0 TIS T19 TZO Tli TU `I`13 T14 T A,'^ i'? *, T17
0 0 0
* 0 " o ''.
FULU.. SCALSDAIA A.MEs-MPS 9UPPC[RTs*Mt'.1.oE-L DATA , 4I O.C.
.L 'Q Psx *Y/Q RM/Q YM/Q FNT A LFH A ^ 'D/Q FM/Q M -0*00 -04"02 -90800 f 11P533 -7*64 .. 5e 3 l3 18 I R 14 , 2010 40*02. -145.20
2 ! - 203 9 * 15#367 1 1 67 12*13 40961 8
3 —4*01 w002 o20 * 367 12*831 1 .97s5 29vkrO -4 13 3 45 4 . - 6*05 - 09.02 m24,980 14, ,213 x79 40o52 24400 -!121 35 ,059 -1020192 5 * 7 p 94, -0o.02 w28@800 6 493 iiluo 15 41422 42o , 28 ^-94*57 6 .10 +04 -0s.02 * 32,467 17412'20 32o17 1,1187 4.76 37E 7' 2#233 -107 + P24 -12x00 0# 0.2 .35.600 i9o00 18 .23 3 ma j 35 5053, 8, "0402 -9x8001 600 0 0 ' 114 lit, 9 L "L 02 93 1 1 600 -26o;66 15*500 11 i' 67 *1360154 *v6l ml329,36 lo 4*02 oOo6OO 11*660 -401 , 55 54533 w 1s , 79 ^126o78 -48f98 59500 11 5 # 97 w 0k O 2 3#433 1i8760 -7- p 1* X121*36 8000 m ocoa -55 * 05 5;1 , 53 Aa 7*833 12 * 000 .-1-146, 6 - ^ 11 -7*.22 13 10 *00 -0*02 5 QW) 12 167 12*427 17 , i -16 35 o t I, V #.94 1 1 1 x99 9 1 @ 0 ,0Z 15,767 1•367 -4S 96 4 S GQ 4.
oi0f'25 :S*300 . 18*48 0e02 ,800 " -8461 As 0001 '"9 1 11o' 567 (CJ A "119
P (0) c
" F o VOUGHT Lei SPEED Q ED IND TUNNEL Psi RM/Q PNT AL PHk YM/Q ' D/Q PM/Q .
QtOQ 97 «2 3 0149461
2u o •15.3x3 l
1 3 7 ir-53 30 0 # 133 S3e 5 93 41.:43.
m26#83$ 3**10 "130Ai 4 w6*05 68+:q9
3 ±1 87 .14 - P 640 • 093:3 39t64 w.-J16 5 '• 7# ,
m3io367 . 40
1 31 15 . 800 87.97 46 w30 200uo o35#367 "x.08.91 6 wiO@05 17#647 78*40 .
51: 0 35 - 4 12a01 9. 7'0 ;39 — .053 r11gi57 -19#393 7 ",a9 o ai o" ZO v 6 47 -1,*0016 A la. 500 ' . •a o 97 13iUL wik2iks 12+ 367 - 22 64007 *%78 0137*.45 10 4002.
-0#567 A2#433 -37s.66 ON O 0 1
5 1 793 3#533 ,A liO7 oi310.24 11 !399* - 09
12e*67 ' -474 09
wosoi 32 8 +01
7,927 -7948 -! i P. 7' 46 12033 -54#77 — `3 w1,24,95 +±1 12 5'00 2.3.•64 *55 x.69 .12..00 .1847 -122868 14 , -3'3 14x0 ^61.35 09.5"33 ORIGINAL PAM Is OF POOR QUALITY A-120, VaUGHT LOW" SPEED VIND RUNNEL .,TEST,,;63 WXNO AXES RUN Zia RUN III il 20/81 021 .
Temp ge t PO 1*45187 GPSF 83000 'VFPS 274#34 MACH 0.2:382, ANFT TOt 702 o 95 0 0 0 0 Q u 0 T18 T15 T20 T11 TIZ T13 T14 TiS T16 T17 1, 0 0 ''. I I L SCALE DATA AMel-MPE, VUPP^i- ^-K EL DATA 'AT C.Q.
to a I t L. a pu - I Q y J f.1 0 m j (^ I v m./ f!^ r" i k 11 T - A 1 % , r H . ', /-,x 'J.'r - 1-1 f f ' m I --r w 02 400 .9. 43.4 - 2 0*01 22 0594 P * 28*63 I ! 25o,04 "134W 69 t X92 0001 ^aa*-11040 i:37 -ig7o _ 7A, '"23#2 40_ ; aA ^^ <l 277 # .74. -JISqUo 00 0^ m6o - 00 *10#64- 6 2Z #560 -40o% 5 QoOj^ -8o , 00 e3*$6 W9045.i wl0#223 22076 -204^6* ko 1 0 o, 0 0 -9+458 831825 im 24 660 23190 ,-62#•93 - 0#01 1 7 0:04 , -1? 401 #*8 # 855 24 .55 P!7#09 '-38.::89 34 0 6,9 9 w 2607 .4 001 2 4. 1 25*181 pt 9 1 # 4 4 Q 5.48 6„ , 3 6 9 @0 14* 0 1 -7x 75 - 22 9.67` 9 0001 -16*00 -6*042 o26t08-4 28-76 26•, 0 28 -32.. 10 .52 89 ' lu .e Q004 '*^50-00 %4 4#470 28o861 *3, 8 # 9,9 3 33+04 31080 0 558* ll 000i„ -3.765 37 *53 W 20 6 00 31 #386 5 2±31 w 47916 4351313 *394428 42 Oa 12 0001 -22000 *3o367 34o108 9 7 66 E 13. 1 0.01 49x.79 (:•,06 379, 45 8 ,.53.50 0449 247' 8 14 0, 1 01 -*26*00 m i 2, o 17 7 41*319 -VtO 428 64 0a ill k,45 i' s 0 a ot - -2, 9g0 1 52. 2 8 -2t488 450458 " 15'7. 5 5 03*98 33 3. a * . 8 e2o^t5Z -33 p,39 230,89 16 0001 0400 +163`5) 5 05 1 1 2 X133 +06 OoOi 19 0 , 2 6 2*00 0 8054 234072 o 349. 5*, 85223 *!124 010 1.8 0401 17v56 400 w 7a7*1 2 3 . 165 11 0 -127 #65 -37•,64 325 19' Q*01 6# . 00 - 6 : , q,g * 6 23.699 ^.40 e-54 1 2,( t 15 633 — *I - 149 ,, 1, 8 20 8 o 4 6, 9,937 O.0$ 10006 — 4 5 i810 114 : 2 164 5 ” 16 0 w?-4 3c6!
Zj l ais8 '20f62 2 1 0001 WOO - 5004 - 249799 -k994 7' - 1 7 6 f, , 75 22 j6— *49-w'2Q0o,08 0001 lZtQQ "40 5 9 25477'1 "57*74 6 Z6 867 23 0001 1*t0i 15981, 0 3#8*3 274108 319187 -'231450 -67# . .93 24 0401. 16400 i3o,44 *2,566 28•706 'm74,31 35P594 -2564,24 000 & 18 * 00 w ivOOO 30*271 -74*67 4 i #1I+ 26 0#01 20 t 0 i 02 32 .855 aSS -82o2a ti*75 w307@6 0.41 4"e--T 22.110 -09549 9;9 35v596 -81*62 4 0 4S .E 28 ooc^ Z*tou -2413^9 -3054,05 sa 9253 6 *8 0 , 65 -78#66 «34 2, 9 ot0j, 26#00 - 3 41#367 w 6847i 5506;33 -22 4458 4! 5 8 *345+58 0*01 2$@00 -409*0 454000 w 56*82 550428 -42o,72 w325t32 #01 000 4 w 8. 6 *5 22*-819 * 24 40 - ( 13,3 q: 4 2 X3 49, 39 .5 o 5I2 YOUGHT LMW SPEED WIND TUNNEL TEST,65SI WIN D :AXES f1/20/81, 0911 Hurl Sig .
849 1 pd 1*VSQ89 TEMP PNT ALPHA PSI D/Q 'Y/Q RM/Q ' YM/Q 4/Q PM/Gl - 4 O g 01 0*00 . i M 3342 505'94' 26%35 68 22,681 0, 1459 rK qO.f " 10,0
000t 224252 '24, ' 0136417 28*
. 1 1 go .
4"' 1 i' 4 OtOt -6t01 o109SO7 22 0 434 -21#78 -3t y 93 254;43 - !121152 98•93 5 24P35 0 , 0901 -71 1 99 P10 9 042 +259 .22,741 -21t88 " 7 23.524 -26t26 *124590 2502 ft69@11 0 0 01 -1 0 0- 0 1 *9-699 .
09 29.6 09 0 0, 1 7 : 12 . 01 -5,006 2 4 0 if 17# 500. a-0#37 1 0301 Vf. M 1 3 1 ,;3: * W21, q, J. 1 : j 2 ot ' "14 * 00 0 St ' 6' ms 0 494 . ;24 " psai O ;-*28t6 w26#054 - 1±41— '26 *1 G7 n 13901 4401 30961 10 OoOi 0, 49970 29006 0,40 9 59 o0li481 52,86 390 . 91 li 040 1 - 204:02 -318. 9 2 31 6 236 -42948 0,359361 Q—
U 0901 0 22,01 9 9964 - 34 * 247 0,47,08 0,39o367 47*36 . , 68fa -
0,, . ' 65.30 -49948 W4544 89c46 13 0 * 0 1 :,024 1 ,0 1 3 ] 796 3706i .
M.3, ' 0, 26 0 9 0. 9 3 , a 113v85 o p oi . 00 ' : 0 0 58 51:.42.96 32 * 68, 0 41*826 ..
1 5.. 0 4 . 01 ' 0 48 too ; 4 5 , s- 69, 9 t93,4 . . 106 ii 95 1 3.4c 92. 5."9 . 59+33~ pi 55 1 3 2*6.61 -144.,42 16 0o01 Q • Qi 0, 6iQ66 8@645 22,801 -33969 0*01 2 4 00 -89313 229861 -36ti7 209.72 0,1339 - 50 80u1 ia 0001 19•74 4000 0, 7 * 552 2 3 0 06238. 7 2 i9:12 l+7 0138 *,45 w w 19 . 0 0 60V •..
0, 7x6349 "t 24 35 2.39434 439.63 '171 i24i 20 • 0. , 011 8600 6 777 23+97647' 09: `19it08. WiV "i88l v ,02.
* 09 21 -OoOt . l 0. 4. 0 1 0,5x813-, 2 4 of 6 9 9. 0,35931. .19B4831 27 07 67 2Q3, 22 w4.735 23 - c1E 0001 12 0 00 ' 259602 0, 27t289 66987 -2199,73 23*75 23 0 0 01,+ 1 4 * 00 - 39747 269687 0, 79*33 31-14*6 0,243996 -24 0,01 1600 21&54 m 2-380 28-133 -88920 369295 02689,09 .
.
1 8 00 169 ^29 * ' SIR --8 - , *1, 0 5b • 29OW80 2OW 9 204,0 1 24 w79 X32.7, 17 26, 0 0 01 - * Q s 223 32 w 078 -92,27 46., 566
27 22 '
' O• Q 1 01 900 -lodis 50 . 8 3 19 - 9,23 so 34 6W-39.
34 .7 1 1 -93*60 . 1.
24900 28 0001 03,584 38.313 -62*80 514!^12 -16 6 67 0291.13 29 0901,• 26#01 49361 41,928 -51907 0 55vQJ8 -3202 m309*79 0,5-633 0901 28 4 0 0 459735 -38e*i 59*488 , ft •~327980 . 5491 13 .33,99 31 02 26 01 8 f w17 0 0; 0 0 -89675 2- -937 5i33* A-122 QUALITY k, Low SPEED WINQ _lUNNtL TgST.;630. , ,--VGUGHT - .
:AXES WIND SUN Igo tiz2o/sl 0912 '' RUN 120 .
Ump goi PO 141,*892 00OF 75400 MACH 0k2267 VFPS a5b*20 152134SQ9 RNFT T01 102 TQJ T04105 TO& TQI Tgf 101 110 702 0 83 0 0 0 0 , 0 - u Tlk T15 Tit TiZ T13 %6 Til T18 TIS TZO 1 0 0 1 0 0 0 AMES-w;TYPE S C . AL BUPF 0 R 11 tl 0 - DATA 'Al C,Gt. FULL, E DATA DE .1 /Q PNT -ALPHA 1 Rtl/Q YM/(a Pm/Q I Y/ta wr — 1 0 , 01 •0#00 w 9#900 ^4&033 7# . 933 - Z3i77 - ^ ia$,*73 0*80 Q0.00 2 . 0 9 6 04 U 47 *136*76 w13#667 i4f620 - 4 1, P: 9 . 2 7#687 3 ;-309 45 * 960 68947 8 1 333 38 066 0146w62 "179267 4 w6*05 93#06 9v033 6 7 16i053 45•.42 156.9 0 ' + 0*00 w 20#7 52 q . 80 "J68008
5 '-7990 160*0
0 0 , 00 422o4 , 00 93067 9 1493 6 y10004 66 * 18 m'177#81 0a00 94462 94447 24 o 3 00 170 9 67 , .
7 •12#00 0.44 -4183.27 0000 025 1 500 19#300 91. 0 4 j 91467 2 0 * 00 Q+01 -!129 t8S 2# . 00' 16.43 9 . . 0#00 *6 ► 804 13 .633 _w5 #_43 6.580 ^ I R 6 -.56 10 4#03 6 9 500 0 27o29 7t80 11254-15 000 9 -30 33 13#300 50. 9 8 Oo-00 Oo433 12#967 1o29 ot24.77 -, 45072 60420 04,00 12 8001 3.8 33 , _ 6.467 1 , -64 1-47 -129«84 9Q0 13 9,99 0 900 61 36'7 1'1r09 lw: 133 &64 7*467 '1298QO go $ $, k 03 :12409 0.0.0 it 033 -1141 , 69633 a 0*64 *07*96 OoiV 09 VS -0000 - 02 -9*967 _ 24•:23 *129*14 1#947. 17*00 60SUG, A-123 VaUGHT Lf1W SPP D WIND WINEr TFr :r 2630 WIND -AXES L/Q Y/Q RM/Q YM/Q PNT .ALPHA D/Q PM/Q PSI 1 .35 *128:..23 *075' 7#11 . Q 1. 0* 0t, o Q t '0 2 -9, a 7 5, 14 -0 0.02 7 750 3 : 0 «.25 m1,37 q ' i 0 *-z 04 . 13s475 14#600 72 # i n i: So3§9. 37171, ' . 2 6 3 - ^i5*276 ,t4 8 1 4,02 ' 1-0002 * 0025 43v85 w1589 48 * -6&05 ow Q o, ' O 2 P m * 450 15 * 550 20 94 .:23 9t076 9#500 52 , r58 -+266 .51 5 '-+7. 90 -002 m22#250 16#970 940,08 17oO25 0.15 9,430 52+'74 m169s-63- 6 '-7s90 -002 m22,275 94 .
i li 9*57 -0 Oa w23 *825 '17 7- 1 Q 98 16 q 29« • 0 x02 • 9 : ' is 24 7 25 I A^ 0076 . ^, I .. 15.28 • 0w02 6 6tSJQ^ X125°..36 9. ^i 2.00 n6 976 : "1.3 * 605 .'y3 693UO I .. 0 -0,.02 -3s000 70•28 "125637 4,02 13*325 -27*63 n 6 q 385 .11 8 p 01 . 0 01. ' 02 3a750 12#960 -65935 - 60-1 5 131o57 6.475 -12 •.61 "135&40 12t906 w88 * 62 12 10000 , m ocO2 7#550 - 1 6 V6, 17 -90 1.3, 23*53, 4 * r76 '"0 00 -5 * 8 75 i 4 0 a5 1 7 43.. b Q.
A-12 4 VeUGHT Lmw SP95D - WIND 1UNNEL I rEST 630 WIND AXES I^IJfY 12'2 RUN 122 /Si 091i
1'i/20
pe 14o,4891 2 .
TEMP 800 MACH: 092267 VFPS 258oZG OFT M25480% QPGF 75 # 00 TOI TOZ T03 Tg6 Tal TO -9 - TV9 TIO 1 , 04 T05 0 0 0 0 u 702 0 92 0 0 T i t TaQ 10 %4 TIS T16 T17 T19 T15 Ti2 T 0 1 1 FULL., SCA46. DATA :TY PE: SUPPOI A "AT CaGly.
AMES . RM/Q I YM/a D/Q Y/Q PNT ALPHA PM/Q P SI L/ Q Os;Ol w-5 v 9,3 3:, i;6«18'0 3 010 ? t2;3: 15034 wl*0033 0- 27x39" 002 -1450153 wo * - 2:i 6*31+7 31: 3 4: l oo k 01 w204567 17#273 45 #,b 3 X 3.99' 143,58 40 9 41 - 4 w 6o05 -04 - 01 18g133 68o1,2 51833 w26,733 44080 " 4 141948 -0!01 5t567 5 '-7-92 *309667 19,193 76oi6 5202 *136s8i 5.167 6 -10#04 -0*01 •34,600 20.707 f i a 62 , 99 -d 18!
7 * 4 12#00 "GoTl 5 if 67 - m38.867 22 03,27 : 64. 8 1 -139 *77 0. 2 -0001 16 * 2 - 67 3 •..2:5 7 la?
02 -9«700 83 . ooj 3k t #Z6 .
1 , •Go, woe -5,031. 16,067 4 w ,9 29,68 *i30.24 "0v01 7v*67 10 4*04 -04613 16o267 "24#83 w 2*88 X127957 li 5698 m 000l 3#767 16.300 033 * 35 7 • 000 -^i240-25 8#267 efspo -0 8 0, 10 12 8 * 01 - 1 0 # 01 16.700 w 4 2.2 5 -1.4-;56 0121.59 7# , 101 '17#03- wU 0 9499 '0 001 1 , 2*627 -43 - o 1707 -tJ221 - 06 l* ' ill 00, wQ-kQl 1.6#867 953 6 561 17+ X 4 9.09 21 in 1, 7167 wot; 4. 0 # 63 iS 0 401. wO*01 - 9-9' 33 166167 3w56 ,uu Z 1 2 5 OF n"OL) ((^L^g g A - . —k YOUGHT Low TU NNEL TEST 630 SPEED WIND WIhD -AXE$ RUN g2 __ 091t RUN 123 PO 1*9,4892 TEMP Bo * f,,ACH .,U*2Z,67 VFPS 258 9,20 RNFT 52^480 s QPSF 75t04 1 TO- T0IJU5 TIQ Tot 1'02 T03 : l0Yj_U._ , 1 06 0 0 0 0 0 0 702 0 92 0 T13 %4 TiS T16 Til T %9 T20 Tit T12 0 1 0 0 0 1 SCM E_DATA DATA 'AT ec AMES-TYPE SUPPO T'Q*MCQEL FLLL PM/9,a RM/Q 1 YM/Q Y/Lj ALPHA PSI D/Q FNT - 2Qt81 8141#57 1 0662 - OfQl -9. p 953 0 . 58 7. t 173 16x300 280-84 0144144 ^-Z*03 x0i 46#753 9 w15o333 21!43 43 _ 34#51 o 1^j7 -145t63 -442 4 0'x 0 P?,Q a 933 3 1 Z 020 V 466-44, h5 8 8 *-321 54607 39 "0 .
* 6@06 01 w26o400 181200 679,90 45t08 0138o37 5t460 10 0*01 p w 30o332 19#200 5 '-7*91 75*81 54*•20 *134#,84 6 .10#04 -0+01 .34.200 20*733 69#19 5#107 61#77 -o l*l t89 22s413 50773 012. 01 -OtOl 38 .767 7 6.3*72 w 0 01 6.: 33 33 4,29 7 Co'? 2003 o o i39*66 a 0, '0 1, t 0 -9 633 2 , 34t55 1105 mi 9 2000 1 0 0401 167 16 * 167 *9 - 7 B 7 3 24,40 A130#53 16.307 70507 10 4#03 -0401 -0*633 w24#43 ^iVs.64 "0*01 J6*333 71E*0 *2692 11, 5498 3*667 -34tH 09.077 o125q,, 7, 4.
8o267 7#09° iz 8*01 -0401 16 •80 0 m4 2 *3 1 2 59, 1 - W 1, 2 GO 8 0 7ti*Q - 13 9 a , 59 -0*01 1 P_ q 520 17•280 -44926 •18.99 =i22s*7 o5j * 60 605$ -0 , 401 169667 18.033 14. !12#02 _21 ^47 -7 - 1 38c4,6 wo to 6 p 94Q _ is 0001 1 "91,800, 16,267 3 *20 A,-x.26 F-cusa VOUGHT LBW ,SPEDWIND TUNN9L AXES WIND • RUN 1 1 24 09 RUN 124 0 TEMP Pe 1*0•092 QPSF 75#90 ' VFPS 011, 1 20, RNFT 4525480•, MACH,-Ow2267 Tog T T02 T`03 'T04Toe To& . To:t o t Tog Tu 702 0 74 0 0 0 0 0 0 T T13 Ti* TIS T16 T11 TIS T15 TEO it Ti?- 0 0 0 1 1 0 0 1 0 0 V ;Type l sup AMES PORT A B ATA slo .FALL. SC LE I qATA l*MaUL PIT ALPHA PSI D/Q Y/w RIM/Q YM/G 'L/Q PM/Q sw afs00'' 1 0*02 000 : 02 7 733, 23fli - 4 159427 <13019329 2 1.0 2003 -0' 02 767 1.3•$0..0 o , 21 c39 *Q 3: _ '_3099 40f0a w18a7'67 433 50:m59 '5 37 *, 40 i t8 27 15 k 0000E 4 06 - $ 05 m24*00 15t700 74043 5#460 *1* 36 01494,49 -OoOl o q 28 # J67 16.867 5 '-7 . 92 8813 1 548OU 48 «1O - 1 ,.86 6 wlf^wos 0 0*01 0304700 196993 5605 •146s01 72#6o^ 5*9 1 +7 !-34 62.99 72,o. 69- 0 q, 9 44 Q 84157,499 , 0 1 3 3., • t 43. 7 v 0 43 i158*65 0*0$ mo 4 0 1 :: - ill$ 067 ' 1 3, 1 w 7 1441 WiLZ 1 , 492 ! - 0 i 0_1 ,4 i Q 11 05 6 0 m ig-t0l ZiI97 10 4#03 -0# , 01 Oo513 '13v067 -33 7000 4'07 m 14 5 * , 56 q, 40 * 2 il 5,99 m otoi 4#500 13#167 -44# , 56 7#413 0 :95 m340f51 * 00 m olol 09*56 12 8 9•. 03 3 Us$67 6*833 - K 134#45 +83 0 51 9*9 13.
&167 -0*01' 1 '1 3,o 87 -oR5 ,4 •09 * , 3 5 00: *2* -!1.2`7+41 5067, -o i$01 "!120*20: -0 . MiJ09 w:,Qq 0#02 01' o733 3 23. 005 X 1 st 74, 633 ' pa.
940 14#5187 TEMP QPSF' ` '759 RNFT MACH O x226+ , 00 NFPS 261:26 1478131t, x'08 105 710- TOO TO T03 'T04 TO TOE TO 0 0 3 2 0 .31 0 0 , 0 0 T11' Tn T12 T13 T14 T15 T16 T1 y , T19 119 0 0 0 0 .32 '32 0 0 SPFECTS ^WRSWC CQRR20TEtl .FS .TARS AND IN ; .qA A ^FUL SCALE DATA 8YH'QLE St1F^RDRY OATA Ar C.t3.
v^r, RM: Q FNT .ALPHA -PSI PM; Q LJ 0 _.
a. ' 23z g X15&R07 '^ 0^8 q ^ q 0 '; 40434 : , x ' w t? St3fs8 370 - 56 .
}.;30'x5 2 .` ^1•7:a ^RQO X 9043 5+`613. 5884 . -: 40454 :: '36645 ,157.25 Qsat1 82:65 - 405 i xis 72' 5•SbS 42+77 , vi155,46 . 4 -5.76 0900 *210771 6.672 4t271 101x83 49+19 5 40453 X156:71 ^7174 0000 02608.14 70682 112,74 5,631 57*,89 w172«16 6 m9.76 0000.a30^Z78 ^ 9-169 9R X84 .__ x -%186 t^rQd a'6h6'66 "6$ 54 18 '!^11'. a # ► 37:x106 77 1007"4 97.0!3' 71t.51r ^i$.A.85' 8. X13.76 O.O p 6191 x042 81c > :1c503 i.04r5.3 " ,77.$9 rt1g.90:68:.
' 0$
9 - <..^.4x70 w56 :1 94 040 45x.5 1Q$+?4 ^' bt
240:62 *1550,39 10 0625 0000 503.27 36049 40580 -20109 180, 40 0600 w 154o40 11 2028 34468 50465 250.66 4.4;2?
12x94 12. 5.605 7094 4+213 -149067 4:02!4 0000 8.253 69:30 ` . 5026 40'259 IR147«35 t 6t;2l^ 0^. 0!' 1.3.i06 14 9 .0.47 0400 147058" 8.24 57,24 60495 16.• 35 <; 4i'^1 g .
«2 2 29 10! 30 0 9 L 22.255: ' 7 xc^86 19.5:4$ ^t 4 S 0 ^8 1 4, 0000 49869 -14!87 -4137088 16 '12029 260941. 8+42 . 4 20051 25021 -^126x 0000 5:779 - >96 ° 17. •14024 2.90631 100339 2023 30t24 - 0000 .33.025 61277 `129•.94 18 16026 12x091 3069 . .,, : 330.97 35433 19. '0. q 0' 5t 4E28
'18 aP4 '37.240 i^kJ?40 22 :b3
=35x.82 ► .57.44 2Qx2+^ OtOQ 159 .^4, b6 X137.51 20 39077 40 k 17 ► .04iO31r :: 500*7 at145'k66 2S< :22's2k O:OG 20.019 -8201 420960' -- .xR2. •24028 00, 00 50890 49t4l 01,506.56 46x618 230492 •106x-59 m, 56«04 ,1530'178 ,23' 25024 00=00 250346 61680 490393 m1, 16!'92 00:00 2*1,79 oRi54+69 •24 0*27 N 1e942 59401 38.47 4s267 ^^ ORIGMAL DMI;R , la A—:4-2 8 OF POOR QUALITY VdUGHT LaW SP " I ED KXND_jj^NNEL TEST • 630 W I tj D - A X I'S RUN •33 1.. 20/gl-- RUN :33 Q933 p5. 14#5187 TEMP 861 GPSF 75o , 00 'VFPS - 2$906 45# MACH 0*^2264 RNK7> 5057 .
Tot 702 T03 Tgt o * Tio TO4 101 196 T07 T 0 4 1 0 0 0 33 0 12 31 0, 0 T13 T14 T15 %7 TIS T15 T20 TIT TIE - T16 EFFECTS C0 RRECTED'F1DR,TARE,AND INTERFERENCE SINaLE SUPPORT,DAT'A DATA 'Al C#G, LFULL SCALE DATA MLI -I- Vtw MAA It-7 -u IQ A PR Ir ONT M'If W" I ". ALPH L D Tilt «c6 1 0 , Q o Q1 . 992 # 017 5#230 44073 05 4 0*24 a t a 0 0 1, -2 0 . 89 S B79 47453 i .2iC44 271+ - 30 -147&38 3, 0,26 *401 5 395 - -24027 45 a7. . P42 t 102, 24 0 84 -$ 0i 2 o 4 Qi26 0 6#00 wi * 706 5*658 4jo21 -6s195 23 * - e8 -1 , Q*o'23 Q126 -7#99 0*1 * 027 60240 331.92 wi0t230 209 , 4* 6 Qo26 "9*99 00002 70011 26c42 w14*666 16t74 •-46•,65 7 0, 6 26 0 12000 30 k1 , 5 w is 07 10 11 + 425 -206,80 1 t17 - 1., 4#92 0*26 -1 , 3099 t;gk: 24152 96871 91k64 02 - 4 ( ^ 389 12 11 9-23 0*26 W 11,t ISV,99, 4 66 — 3i75 0289631 it-,as 42`.,18' 3.189 io 0626 "1708 44877 w6t.85 *33080 10&56 1304i1 74*09 it Q426.020#,03 811,7 7027 159853 113*30 -18*-99 437' t 527 -12 1,8,708 3 0#26 .-22*00 90 . 033 %43o044 152o,85 -36012 11 0,26, -23 t, 9 9 I j o r 1 5^ 09 21 , o a4 6 . *3, 21, #47 17,16 k -52w75 14 R26 *G1; 250057 0# 26 13:t s,23 -68 f at •15 21.11;,8: ' ?039016 X3,63 15, 0126 W PMi i 01 15 # 426 , 1^8 a 12 . S wS0, 672 455 . , 7'75 205i18 Q 12 pm 30 s.02 16oA.j8 31to6i t>5 6 0 2030,83.
N 77oI6 j o S81819 ;17 Q0,00 -I4684 - 002ri i- J4 , 592,97 43 o i -65 6t697 251,80 0926 2*00 14948 5 . 43 * , 74 # 482 271,19 - R 1 84 42 4 22'.1 I 19 0- 3 .99 #8 13 dt P - - 3: 1, 18 0 26 01,0880 37 - 19 6 E5 5,841 5.
20 0026 S ► 99 3302 15 W 19599 161,280 2.8 46 061328 -197*29 7#99 : 0 782 5 8 21 0-Sak m0 6*9*4 0 3 14 is 36 ;19 azi, zz Q026 10000 0076 7#716 10,84 -23 q S44 37@,76 m i, 218*91, 23 0926 1,1#99 80902 40.76 10556 0-90186 028#129 -240*,45 24 0*2,6 13 1:98 20685 10o665 8 9 29 ;aj .32a 959 40-41473 1 -258 4 25 0#26 15W99 229 J t 2#73 m o 28 8 *; 13 . 12,351, -30932 38 t 2:29 491 57 1 13 7 ' 26 0#26 17*99 5#930 -4So83 :42 * 830i 45.t 57, -316*57 246233 27 7.926 *58.84 0,26 200-02 16q,627 -48 9338 48698 -360 4 05 ea Qt26 22400 iO t o72 19iO45 .53t678 52%81 60403922 m76128, as QoZ6 234-98 11 4 667 22o1.29, . 53 0'77 *431 t, , 83 w 87 %93 58o*23 30 0126 26*0V i3o072 63#347 55006 "1^65c66 25#263 s-94,,68 0026 29 eD 1. 13 j:— o.l 27 13#.7"2; .271 2 x-67o*O 63 1 14.1. 14.1 w39$936 32 , 0496 30#01 1:30 83 , la 66f1}96 , 3 x62 -40512a 1 0 9,'2'S -47t33 33 0#26 0000 • 1 # 451 ^ 6#031 ti ' *230, 44*88 27#99 0169#27 WINO -AXES RU's -34 11l20/81, '6933 RUN .34 TEMP 1 Re.
864 144.5187
r.e ^^^ ► ai is tla C10Y 1 I-f7 [^LJ 1""! 'V A:. 1 pi+1/(^ VJ(J.
Jii.lTt7 rv+ R ^/ W r rt . Q L./ r ^il i r 0.27. 2:9 to -Qf03 4+1e8:68 : S•.1Y 97 S 688 -gi66478 = '*2x47 2 Q a>2,7 +s 1.s99 rI 966 ^" 5+34'7 i't03a. 28' 63 .t135•-16 3x56 3 26•`57•.^114s'92 0 -04+:00 ',*2s,C11 5+540 41•:92 ;-w3t 17 4 •1.732 25v40 0 0 27- "60, 00 5,937 36•:23 ' w 7s401 r96+41 n 5 -807 21.80 ,•69•,23 0+27 9, 14104 6.533 29•;82 R1 y 4202 6 0427 -10400 17.71 .9,40.25 06207 7+327 21..90 x+16.241 7 0.27' ^32..e00 14x,42 0.342 848%4 iQ R21't282 ,.. +16•.02 8 ^13 y 99 C^•2T 6+g7 1't91 . :. 15*M 832 1:0+355 425:t899 9 0427. 1 . e99 12v74 2+938 :i2+043 1.34 A -30:410 430.83 10 0.27 "1.7vs9 44465 10 75,69 13,881 "8056 0349743 0!
11 Q+27: 0 20 '00 1 6.707 16+339 1 0 1 380584 -18429 99,78 113•;98 4«66 12 0.27 `22,.02 8+931 943!805 150•,18 190221 N 359.35 1 13 9 G27'. -2 11.•2 9 ;229-256 = 94.02 180.53 149+9 t 1*489427; ' =155.67 14' 0, 4 27 8f t26 X42 0046 13+ 180 25.334 -4202 52s28i 1l5 0427 1113.694 :.55.x568 10,14 1198:0.38 28-9410 073x6e 16 0427 -30.00 •72x.43 16.086 31si00 158,231 49,88 0 200x49 Q•27 17 0400 •2 4 230 27.58 54360 3806 - 6t111 -167908 IS 2r02 m 24i37 5+489 384;63 99650 29-2 w17.9x64 a v27 02-4 ,024 3, 19 0,027 49,90 S945 32x08 :1.2.4597..
2Q 6400 •673 360.08: 1-1,93. 61 0.27 -01o800 6'x335 23495 21 Q,%2.7 7#99.: 37.49 +9, 1- i a7 6+868 i'2t.9' 1q 3(J3 *201.:82 .22 4.27 908 39x87 0,021 23t3O7 -215*84 7.752 Ot89 23 42.39 Q•27. 1.2400 10188 84921 -9987 '27-t548 $237x09 24 0 6 27 13.'99 43«55 28206 20.612 =16+73 :32.4.94 -1255,52
25 0.27. 1.6 *03 43 OR
4:x44 I2o,364 W29+71. 37•545 a2889,2 26: 46 e,*G -315,t,,83 Q x2.7 • 17 x99 5#637 44 -176., -`42.48 " 1!'2.I 1, U* 27 1.9.99 49+65 0.27 7.372 .16.369 w574,58 47's2U :358-,86 as 219. 98 9o468 18.981 a+27 . m 7^ .52+618 53+ 64 r.,, 66 -401,P-74 042.7 21.98 25 .5.29709 53i77 9,408 184945 "71492 -400499 •' 30 0.27_ 24v00 53437 11+702 214953 • 85.31 57t6U4 -433x94 31 0^27 2.5.99 53v00 1340:08 25.094 62:e270 •463..95 -93s7'6 280 , 32, 0f^ 12.752 0 % 27 29+803 • ^51^.82 62,412 33 04`2.7 29x99 3y39 12.695 32.639 ;65f825 e406w40 =4_$••04 .164`04 3'4 -0e01 5451U .
0027 "'2,194 54330 ' 299, 28 41x64 CQGvI^1 ()F BOOR QUALITY 0 A-1 3 > 'YOUGHT LMW SPEED TP_a I r' .630_ WF,P WIND .AXES
RUN 15
it/20181 0939' RUN 35 is TE MP x 684 6464.
po 14 QPSF '75 #00 YFF 35Z# 94 RNF1' 157904 MACH 0•'2254- .
1"Ot T02 T4--Z" 104 T`05 TO T10 TQy T08 Tog 0 0. 0 0 .32 0 0 14 31 T11 T12 T13 T14 T15 T16 %7 T1g T15 T40 0 0 . :32 :3 0 3 0 0 0 L 0 ,AND.
CORRECTED FOR ''APE TNTERrERENCE ERFECTS 9'1NGL^ i ; 6t1P RQRT` . DAB'[ ImA T'h'A,,t 'r.n . . : 9 b i i' S Ck L9 to PCT ALPHA PSI 0/C, 'Y/W 'RM/0 L/ G I PM/^ ► YM/a q 01 T1 0975 4 v 794 32:0:51 -a 0 5.55' ,2.0.31 -40.99 0 . 2'S < -0 2 -1: # 76 '
0,001 ' 40924 3167 F -9.58
w $#437 5:1091 omov4 89 3 '"3'w7'9 •+0001 -14#862 5.366 Z8 ton mRQJ?t58 ,78 St21 -lif, ^. 4 ;-5078 -0*01 -210245 6.1;23 98,67 -Ot125 5,:62 ,wliw49 5 -7077 -001 «27.278 7•207 -001. 44 113010? 12071 6 -9.77 0001 -X1.484 5«64 0 8.753 i 6.21 Q±169 15.8,_.
.
7 •i1077 -04101 837.29810,625 7061.- 97• 10.97 66 ", 0: t Q92 8 w11977 , 4040i o•43r510 :120637 1.0406$ -01790 7w33 ;wt*r'37 9 14.7.7 E ' w p't01 .46 7.06_, -17006 f: ^ 6 '13#s!jQ o6 314 -005$t^ 10 s 0024 -0101 -2 008 40827 320.44 -0~356 2*33 -11x89 11 2.26 -0t01 34843 4.908 -04460 1037 -15457 2101.0 12 4026 -0001 50102 Otii .-j6452 8.465 13..36 -09506 6024 -0001. 43. in 5*361. 8+.7'1 -0«295' f^88:' 83,3072 -14 8028 • •0' ^3'R58 1.7.'781 5.947 1.it37 10 18"79 - 15 10.*27 -040.1 '22.7,12 6.858 Gr175 •50116 113..28 14.61 60135 .12..24 16 :12025 -Or01 27.566 ' .70594 n 17085 -OiQ32 17 •1,4.28 -0•.01 300545 -30,23 90882 00828 -109,78 18 16,26 -OtOi 33.606 11:0446 14.60 -40.52 4.31 1.0890_ n ..
r 1,9 18.30 'O M 01 36 w3Zi 14.122 --26 r 72 - 09975 -1 •'09' - g X04 ; 20 20.26 - w &'9 , #0'00 390774 160-7115 +v540 ,9 • Qk166 50 * ,09.00 :22 0/}060' -11082' 21 +27 000001 42:#608 19.6 7 -79#26 _ -09843' .22 •24.25 0-0001 459667 220780 -iQ00.65 -7.87 -10036 Q0296 23 25928 - 001 430105 25.125 w114016 10203 -11t81 21087 24 0026 -0001 -1.741 32054 *0 00505 4'•827 1*78 -11•,80 -- . OUGHT Lays PE'D i' IND TUNNEL It ST •630 s 4a.2p r3^ 046 ^t703q * 8 g 8 4#706 y 0x88 1 i>5"71 «i xb > l 0 01 4*959. *0t9A 3 003 1+ 75 ` *7 .33 26' 5 321 t1^i4 _ °3614 ;03476 ,. 00#01 -TOtAk.i : 3 owl 5100 - -w- .. j l^ +s+0^01 00,50 -3434 #+5875 F *953 52890 ^0l4 4 194y4 1 i*'05 5 - 0 - 0 9383 -4#,29 ' 0 7 a 73 001 71.36 A@44 251 7*347 ee5e r 1494 6 a 9*76 0 0#01. 74 • *3 V 1a8^ #a,*98 7 411#77. °O*Qi w35p$71 -1.0*02i a0*67: °0tb51 2*1 * 75 °Or...01 "42*253 89!x55' . ..1:35t - 6.•'27
& -43 11 *5t*2
LS 6 .
° : i4 * b 83 a Ot O1 a45s909 43o 95* • i*Vg^
3 76'' 91
°1*•06 °0#159 0001 998 4.706 i5*76 -01888 10 0*26 0 0 0 * M0«94 -0*51 4#335 7*33 °0077 11 2 027 -0tOi 48543 -0.07 12 4.825 88 0.01 2.1 71 4,, "1 •$^ 12,2..
eaO1 57.1.:. t 83,:35 13 #816 Sx252 91
*2^ 1 3 0#3( `o 9
•2R4^ • "' °5••24 1: 4 8*2a" 0902 ^aa.7'48 4884 °t 871 1^*22Ci , ..4 ;Q, 949 °5466 6 '- °O'* 0l 92 * 4 38 6i 739 -601 w0*O1 •2*-86 35#:52 0 08353 16 :12*25 26.653 7*758 x7•+59 -0#01 0#543 6#'82 17 i4 #25 28.242 9*645 43*O1 47.go 1#314 °59.72 4.
16#26 ^0+01 *536 I i o,i.95 «eQR73 ^43 1.^i. + 0: 933 &*.43 G Y }?16' ^' 8 2 p ; *3`f67 `' °9i73 .
20 *.2^h °^t•01 39.557 16.812 =w0.88' °t}4°2 •1 *959 °3.36 21 *2#708 =19.667 - 0't 970 22, 21 0 041 -6 9 * 41 0*006 -3 *46 •4#39 22. •2 I k#24 °O*Oi 469292 229940 t o 99-55 Q2#46 wQ*01 Oi 64 °7M04 23- 25#27 49 * 655 251306 ee 114*43 -1.19 =0..13 24 00-25 -O#Oi ee l,#231 4.672. 18820 °1022 QUA LITY k^ A-132 V'SUGHT Lt9k SPEED A11LO,T NEL fiE SY' 6 0 U N WINE :AXES Y- IQ PNT -ALPHA PSI ri,=,rw D/0 PM/q i'iGl L /Q 0.2^F = • kRoi - 3*338 SOS 7*573 -112.-66 .
'' *O^Q1 2 Z •7 3 681 3.11+9 «•133i5.5 v atk,9'a f0 •:42 1«06 3.78' 00*01 0a6kr M 3«1;i6 t p 3'A -00134 = r1i66.
'-;o 1. 53 o y- -OPO , -5*75 •-4,151 34396 ^0«28 X00.82 -171030 -00137 5 w2,«.04 '-7M75 -0#,Ol -BoO44 3.821 -1890.46 -0*t07 A's 09,45 "- 0 * 6 -9,74 01 m n 1107 i2.570 4+479 -204.5Q 020 .a X11.76 -0,101 15.4 63> •5.16 om. 17t(145 262 039 -. 0 43 21.3 g 6r.lkia »13.78 ' -Qt,.0.1.•. *221883 ^i. 073 s •5,85 •+223.1':79 y GFS18 ^ ' .2«:66 j4 IMO 1 * 0j2; 9. 7 V e01 ,.Z5 * 38 -•.741 • M. ^«144 ,227' &85 -0401 10 Cal 24 71539 3«272 -0460!4 -0040 5.57 -112 +1Q 11 26 -O o O1 ,04 21 , 3.588 0 0 * 61 '19.0 203 -90, 26 -0075 . 0 12 4.2 Z„ '' 1 Wo *:12 1 x363 3.886 #876 g.06 ^0 b^"0ss11- i3 f •2^ ► ` k:. * + O6 1827 010 i7r y63 4 -05 0: 787 3 8.2'5 3 ^iC^1 20,$45 514.6 -31" 30Ot422 *"87!
` 5.5 -3.46 35 "04rQ1 "9i., 6, 28 10.28 24.323 4 Oti26 25 -0!01 975 -7q,98 27 0 7a10"S 11 0,8.9 0*317 -1#,-96 . '17 -00101 -1.4*24 280932 8.922 t 255 . m 1.5o07 ^ 2.9.52 8.00 -T 16,26 -0*01 16.07 28 31«213 1:541 w 10#637 X5.31 7.1'7 E +R O''01 0074 111#27 30,789' 12,6:92 Q15*t ' -go-20 .51,23 20 ' 20*27 +Ut01 31.647 1«28 1 789 °' 7Z* 62 • O:01 21, 32.469 16..636 *72 •3.65 85s o 0 •3•:92 , 22 •24.25 -0001 34 J228 -3«45 18«75.6 980.10 -ORQ25 0089 rg ,23.
2'5.25 -0.01. 36.109 . 2:4G O4,86 20 120 0 r 92.5 103 v 10 24 --0.41 3«338 -00,40 0*24 7.639 112.10 -00717 1:•47 ) i f , "( 1 V q c u 6 to 4%
Q f; Q U n L A-133
V C U G H T L gw 9 P E E U WIND 'AXES RUN aE A / RUk IS 2LLa 1 093:3 I - Temp 850 QPsF 75000 MACH Gw2354 VFPS 2$804 RNFT 150iU -5R f 't01 .
tai vo2 103 39Tg4 : , t, o 5 -rO6 T61 log. l ug. 110 a 0 - u . 0 0 32 0 '17 31 0 Tit Tla T16 T17 71$ T15 T?O T13 Ti* T15 2 0 --- .0 0 EFFECTS rNTERFERENLE FeR TARE AND CO RRECTO ) _slNgLK SUPPORT OATjk DATA AT C9G, . , FULL - SCALk PATA, FNT -AI.PHA F S X D/Q Y/w Ym/Q L/Q Pm/Q 211&14 -4 15 t s , 33 7#181 I 3 # 869 - 1 107097 5 t0b 2 # - t o 76 v QvQ1. : 3# 3.686 $01294 . 1'S$441 234- 6S 691 26 0,8 8 " 3o682 a 14 6 9 n',, 33 *23 -14 - 3 * 51 1 3 7 ' lk, 54-74 m 04-01 3,889 61596 39r,26 -w16708 19 4 l, 1 , 6 6 v 4 16 7 6-4 '*7m77 w 0#01 4 , 330 -%1834-65 6! 823 t41 X1714- 86 -79962 4 6 6 6 '25 of -9#74 !LQ-O"- ?.,5,99 6go;n 544-09 , +5 79.51 o379 i.i ON " ' 715 w Oo 01 w17 * 0! 71 1, 2^i $ 6 761 ra04-s 66 7 # 3 !2 9 6 0* 4 3 4179,r43 1 9 .171„ 650,59 8 43,70 0 .4- 2 2 1 8 6o g $3, 6. t 13 86,8 1 9 9 L 1, wee o clE 9 6 6 4 U u 68.'37 w0o , Q «« :4- 7 w o 1 6 6 i 7 2 10 Q9E5 "Okol, 74-348 36909 wlVoli 5t*71 21#23 -RI51t,56 4t5O* .1t 2425 0040 1 10«858 4o258 10 876,0$ 159-83 "1439,72 J+ o 4 8 03 "i36,6a 12 4*24 -0 6 01 13t709 7A 49 , *0 1 7: $ . 5905 - 0 1,33 r03 13 * 6 * , 26 100 f0l, 'I7o 0 47o49 40060 4-A 2,6 41, 8,#16 - m Q * Ol 201670 -505,95 -?-6 0 90 41 Ol w 2c, M -16 10 .. 73 9 o ; 83, 6 4t$9'3 _4 # i 1 66506 04-,01 5tjau -16q.8 ^ 16 :12 «26 m 15002 o!i27s,:i2 274 - 617 74-647 17 -ih s24 -0901 281716 691- 39 11 28 v .97 , ^120#26 94-542 334.86 - -0901 3J,813 110189 + • 36 18 16*24 t.36 6*788 4-,48 w i 1 9,& 14 ^ - 0 19 18 vZO 0#01 :. e,-5 0 "12' 9«.4 31 " #680 1,39 :119 64 1'47' - 4 5 0 6 - 0 3 4' 9 ' 5 9- 2 20, i 20 02 6+0 •, 01 0,62 - 31,777 15*178 74x.25 - *058 "34 0 13 Vv, 7 8 21, "220 , 27 X3 8 x94 -0o01 320798 87*.38 4te33 - 0 1 37 m15 17 . 176.
m0 22 24#26_ 4 #26 .01 -4 8 334-7 8 1 199248 9 54 17 y13 6•,86 50481 09 .23 '25 % -GoOl 35 * 563 20 * 661 98#10 69262 -53*76 "136 #,S3
0023 "0001 w r. 0
2* 7 ,114 3 ot9O m J 09 o, 02 55271 21 «33 16 1
A^134 POOR QUALITY T (EM p ;94 PC . 14x6464• RM/4 YM/9 ALPHA PSI D/G Y/w PNT L/0 PM/9 13*89 Ct^01 •0 * g88 m;'54464 *156%16 1 0.:27" 21686 930'x'6 ' ;5K^66 3:1.39 -*16.19,20 2 L?t01 `., x • 24040 2.706 "1+'^7 wiSG•a1' 6i5^8.,^f6` 405w56 ^° 3 x 3..7'5 Oo.t1 _ • *3^t77$ 286!5 .226:#:26 t w 5 . 77 -4 4 46#,21 OsOl 210 2.843 mi43•. 69 7t,471 Y-185'*59 . 530 5 2.156 1 *195+54 w 7#76 0 . 01 5.325 0 81123 158 9 -74 8#434 61 wr42 6 m 9.74 0,01 w 6 # 688 3* 64§ - -901.60 x -171 • 1P {401: 66*26 W198s89'.
► 08,097 -41814.96 ti.:8^. gr9.0 7. -41Y 74 4 0'x;98 c a35 -001 -..9 *0 3 E+4 46 -41 a0•94 •^i30 5 477 4087$ 466 9 6r54^i 7'2+94; 0=185«1$ X14+76 0':01 w1Q ► 283 9•a5o w^^•'^8 10 6 467 24#07 -4154x04 0.24 Qs01 2+685 -93#19 -0x924 17400 2425 001 O0167 50QQ9 -146+30 11 20841 -78#00 10+60 w6l w62 4094 -4134+95 12 4.26 04.01 i#368 26830 ,0 At o-26 0 # 01' 24863 ^ ;:4347 88 13 14334 *6.1, 7 1 b1+2'7 5477 -4130#29;.
4?'4CS1;' 2c: 380 84984 46 x 7.2 3^^"1 '5020 0439 {9401 3 024.0 ': +12.9430 15 45 &•25 34062 x# 28066 +26 Qt01 3.32.4 +8.86 3t 594 •6027 *1.31 16 1Q 4.255 -4135,,06 3#618 44372 '°110;23 ' 17 .12423 0401 54363 84.63 w 18r09 0141a89 0*01 64476 54969 9 4759 18 •14.28 24.63 4 4!
;d2.2`w2: 41401 18:1 •146*03 >i9 14 . 21 7!631, 44563 4060.
g 3i"31g, 20 i i24 fl4c91 g *7'0$ . " . 5;• 445 .'
0401 - 73 96 3 1246 -29*95 n #132«43 21 -.:20.27 9#521 60597 w.123•:42 - 34+36 . t01 22 26 O 0 0 4690 90.3,6 2 4986 22 0 1.0.679 --38%38 23 29562 w117x20 •24.26 0%01 11 4 832 70482 104.41 40+36 25425 0 401 14S54 - -11200,-4 24 12.352 74826 1,11.46 .s 2.4x35 :01,01 w 94#22 5s3 7 56wQ7 25 0#24 04`957 20684 Y i D c,GE, of 6 3 0^ 4 YOUGHT L6W L TES?
SPEE ---: W ND :AXES .
RUN wa ota^ 933
;,^
TEMP Pe 14+6464 94e MACH 4 w2ra54 QP5F 1.,846164 95t94 YPpB 260+12 RNF'T 710' 1'41 ' OZ 'F03 104 T^ti5 Tog, Tt 7Og 'fS^5i TOZ Q 0 9 0 •3 9 , 0 0 0, 19 31 Ti g T19 TEO T11 Tit T13 Ti* Ti5 %6 %7 U 0 0 0 b 0 4 32 '32 0 ^.
:C,3 AND TNfiAFERENC,:EFFECTS' R1 q ,E , CTF-D FtR TARE 'EL'LL 1CAi:16 C tG DATA SlM LE SUPPORT .DA rA PST RM/Q YM/Q PNT ALPHA D/Q PM/Q 'Y/Q ----- ----- • g 1 .^ 5 i 3:7 6 6 a 43 U'^^ '. 2 :^ l 5 7 * 66 0.24 01. 7 8 . a p :4 + 1' 17 «28 3i X161«25 00! : . Q42 2 +'; 474 X13 +26 4+587 64±56 ^t(}all.
6'^lct^ .170e5^ 3 '-3."1 a OPO1 • , 17.486 4.533 ; ^8•^s _ 47«64 X182«24 t r 5i77 0•.01 51,726 7,!9311 4 m*21.555 9.27.16 54 55 8 +485 «194+-84 5 '-7.74 0.Oi * 23 * 671 69843 13301.7 64 * 47 .25 # S8 ZaB83 i26vP4 =200 * 65. .
6 M 9.7 7 0401 ?`2's70 'x!202 8 1 5`a.49b; 7 + X+79, D 1 X27.891 3 295 S:34e(17 .
': 0+58 r1:3# x+202 60 8 QtOt a30 447 t5 g 4 54'S7S, 77' l 10 144fS2 9b.i 9: ^Fx b: 9Q 7 ;.
QR31 ,:53i b13.74` 3 ' 3'73 1 ,43.
80038 01,88+65 10 •14#77 OaO1 om32+299 33,.339 154.88 81857 24+-49 "161,016 0401 09 643 25«1,3 6.1'0,2 ii Q•23 4 42317 1.59166 5 +694 I506•18 0001 054914 3.829 12 2.27 w 4125 8# S ' ; M1*2«14 13 0.01 w2 i i95 3#6$;^F 581x3: ^i2s 08 tw32.g1 2: 4 784 ' 42 01;18+94 6,+2^ a tai 3 «75'1 14 1.259.
^1 s • .^•^c^5 ^^ It 0001 : 9 a.. x+.695': 8427 A 0 , 11 8^^ ^^ 4.885 , 8•.92 8144••28 iQ•'2k 0401 4.014 16 8.519 -80+39 ^14••69 0•,01 5014 "'145.35 17 '12.26 120400 4.608 • 1,07.17 a+:Ok 1,2 C?1 i20e 7 'eO9f} ^i.4ts4d 1.3 : i . 2?` :'17,599 6 701 X 8`•27, X13734 3.5;*2: 20 18.2501 19.8':Zc 8.427 ^t;2"St3,!4 *Q ' Z*66- K2 atU O 123 ` .79 : 2i 20.t2S O1 210;346 L713 4 20- 5 54 1#!122 3#.64 - 350. 40 22 :22421, 0+01 22.684 mii 8o1 6 2999'1 11 1 020 29744 - 37x95 -*109.51 23 •24!.26 09-01 24@438 .12«501 wii7 r 13 •41w96 •100«.36 Os01 25# 73 13.x#19 •^i224, 1F; 2#79U 24 '25023 5 - 23x52 -157 o-04 25 Qt. 24 D = 01 9,509 5'•921 4«1'1.7 2611 z
OPIMMAL PIN2. M
OF POOP. QUALITY YOUGHT Lm"eeep WINfS TUNNELIT,EST,030 :AXES WINO R U N 41 RUN .41 11Z20181 TEMP $4 * PO - 1*4,6464 QPSF RKFT 14#4614i 75*00 VFPS 2609-12 MACH Oq,2254 T01 T02 103 T04 TQS TQ& TO) TQJ[ 105 TIP 0 0 39 0 0 20 31 0 0 1 0 Tit TiZ Ti3 T14 Ti5 Ti6 Til TIS T19 T40 0 32 ^32 0 I CORR5CYE D FOR TXRE AND rNTEF'rMNCC,EFFECTS E -SVpPORT,^0A*?A SCALE. OAI,A , COG,, DATA 'ALT .,^IWLL SI NGL -- ^ %A /G -t t, PNT ALPHA m I'l P S I Q/Q pm/0 'Y/Q T;-If W 'L/ Q 1 0 *26 0 0 2e342 -96 . °*Gt-0 , 4 -1413 -0*790 86 76 0*01, 2 . -i 804 P- 4, *1 13. 38 -0078 -90 01 *3*58 3. G 0101 .
W 3075 8 *3 77 ' 1 2x902 *622 - d 31180 04 84 0064 00,84 099•34 ' 10 5 s 7 8 0o-01 -3 o 926 Et836 * ,, 148 # 28 L l P 775
5 w7*74
0401 044435 001 .- m J2•,88 3*125 oi62#15 10019 6 w 9674 0*01 06.. 43 3t. 85 i9 8 3 t 15 0^17, wi0e , 46 2 , 2: 3.
7 .11, *76 4 ..189#96 tf 92 Q*Oi 71553 4#033 -407 a .1,3079 , iS -3'•78.
04 01 60 9 e Q66 8!"60, 9 6,4 , 01 . , r 9.
40606 "?Oi0ff 84.
7,79 - . 4 * 98a 96 -208,09 1096
- A- A -6-
to -If-oa Qs27 0*01 "0*822 21408 W 0# - 74 96#14 " 0 107 li 2124 0401 0q175 -1*,64 -00"38 21417 -81*63 w O#120 0 0 8 12 4 c a C-) 1 "'0 . 61 8 1&61 0 64 32 2 1#2 6 2- ..2+ 47 . 1 0, lwa,9 13 6,27 0 Zf *598 viQ t!598 wi P , 66 r 6 0,21 Q k Q I. - a. i. 0 "i k #7,'6 a p- a - 9 # 8 1 1 0 1947 0 1 7 0?.
i s to-26 0001 ij j 2 974 ia 4 - " 1 T-6 7 ^ 1 0t-99 *016 16 .12#23 0#01 50228 2 .255 255 6 t39 Q O#589 -16-91 -1028 0A01 6@343 1 P - 1+74 17 -14*24 3#711 23#26 "0092 -2v32 0 k 0 18 16#27 1 7#434 - ,Aa8 40 * 98 0 , 295 19' 18 1 0 , 26 q,08 02, q, 9 j 5, 00 - 0i Oo*04 4077 157 * 34 '-0 t6-U6 zo ec ' s 26 Q901 0 *36 90424 5t654 ' 73*53, -,,t t 5- 1 a1, 22426 OOPI 10,432 6,47 1 5 814 v 9 9- . 22 - Z* , k 2 6 otoi 11 4 530 -0 * ^ i* 7#272, 104*92 *It237 2%1 + 7 -0967 '23 26t26 001 12#022 44-1,* 7#641 I1It89 m l11-94 24 0125 okoi "0 * 890 2#408 -97** P m OoT97 -0oa * 7 w0,#3-j C3 PnO 13, l Cdr. vs^au A-13 VaUGHT L e ig sprED wrt4b TUNNEL TFAT_:630 WIND 'AXES PNT L/Q RM/Q YM/Q -ALPHA P S X PM/Q Y/w mqGtava . =x«53 ow a* w 0f524 2# 675 -37:0 .
8'#.
- 60 2 v 7 23 , *10 s 51 0025 --3*72 0;',t 0 1 ^ na-#-634 2-769 QcZtiU^ 0*4-T w6wi9 ^-5 v 75 0'..0 1 0#P59 -3#690 2 #996 00613 -8#'47 o 146s41 5 '-7o74 0#01 -4,802 3o338 ocas oo163o83 00772 -7w42 • 6 904 0001 w6 * OiQ 3 67 32 0 862---- 0..1 w6 o27 w 1 7 9 A a$ v .::,w I WI .
i 07 1 Q tot 0, 0 , 44 2#06 4- g i9l,02 , '86
" 8 0: 0913
4 *20 0.t 9 . 4471 r0 - o2 i, i 0 87 l i p: 5 .
:iO:a:ncj 10 0,126 -0*38 Q*,Ol. -00323 2o608 -95 * , -0vI90 -0 0.43 of.01 li 2#25 010*93 0*675 2,1698 -78c68 -00213 0v'97 12 0*01 -10,29 4427 1t7,96 2*717 m6 3 17P -0#461 2..88
1 4 8.27 ot 0 1 ol.;,6 1 t-
4 40 * a 30 :5 il 0 0, 47' , 0 4, x.6 2 24 atol. Sot&Z, 3x72 1 w:l 3 1" # - 64 : 44l w iw13 16 .12 26 ► 04-01 6*129 1+9037 -10.82 3090 "1*445 O.67 17 14. 2 0#01 4o493 - 1 #43 2 s 09 7 7 # 144 22 #:02 w 1#739 18 16026 otoi 8*167 -00.68 5.054 39531 A —. U — 2#4 18 * 27 QtOi $4,971 5itig$ 57&68 7 R 20 92 7 2n36 1 - 4 i _. 3t , 40, 60,8* 0% 0 1 , 7,92 64 002 7
- 2 4 . 06 "22, L GiOl
-2*#25 04-71 2025 0001 11,79 5 7*451 104#•80 "O#897 23+ 25.26 OtOi 12#255 -04-04 5#1* 7*864 112t62 -09761 24 0025 ooOi 8*588 -27 #, -0o37 -0 * 257 17 -0#203 0&08 ^" ,, RICE`NL PPC^3 ^,S A-138 OF FCCR QUALITY VftUG HT aEZg D_k,jNQ 11INNE 1 tERY ASO' Lak_ D AXES WIN Pf3, 1466120 TEMP 76- MACH 0*2257 Q p SF , 75G0.0 VFPS 256016 RNPT 154644 9 0 TU!5 110 , ro2 Tg3 u.4 Tus To-is TO-1 TOE 0 U 18 31 0 0 0 0 3: 9 T17 T18 T1Y T20 Tit T13 T14 T16 T116 T12 0 n i rj EFFECTS MECTED FOR TARE AND INTER f' 5:RF N tt CSE SINAI E SUPF§Rj Dk re PSI 4/Q D/Q pm/o/ Y/w RM/Q YM/Q F N 1' ALPHA 59 2 . 6 23e31 w1*3*23 1 0 t, 25' 0401 $oils A94059 0.590 0,•, 6 6 '*1,1,2%2$ a -Isis 592.76 2 91t I1, - o 2 , 49*27 0*01 6106E 351,68 -11 9 7,88 3 - -3976 R 1 603b 41 *35 w166o87 4 w 5075 otoi -4 3611p3 w i4a q 5s 46# . .
otol p ;7 30490 *160#37 6t515 63 -167077 5 -7o75 -So "e 2 6 3 n47 6 * 602 50 0 0'1 - 6 1 Z Q8 ff -I48093 0.00 1 0, 7^7 51'0:3.1• 7 • 11#74 - 7 o. 9 64 4o - 432 w t$4-50 UOUI 53v42 - 1 4 103 8 * 13 v 7$ -5.4- 7 7, S*Z45 i - 1,97-o 07 4 AP 0#25 7403x04556 3 #078 1% 94t70 5i0 2 0 otot 0 0 436 a Ai,78 •133c98 it 2826 3v175 077165 4v45_ 1 2 41,25 0 : 0 1 1, . A 2 4 . 2 6 PAR * A4 "q o 30947 12*-44 -w127,50 147 093: 393,3'3. 5 12 5 13 6027 Olk 0 1 2#780 3 0 5*7 op 47 ^ 9 1 f t, 0 + b. U,ckS , ol29#77 14 0 01 3 8027 0 4o007 30 837 -,29 8 0 t 0 1• 5,055 *4053 m 134o27 __-_ 5 10. 2 6 4 . 0 4, -1 . 3, It, -10 *0 -(1 , 3 1^ m 8 6 3,92*7 16 12t29 01 - 01 4 . 520 60199 4•.74 12: 3 16 *2.6 3«123 1#08 1 7 -14025 oqol 5#008 1905.1 - 14 19 9,46 - o47 01 1 01 •9 1 -139 1 8 16625 8a 031 5# 3: a O 37#55 - 8 - 216'5 -22w79 •+1.36 1 18 19 18 . 24 0 80809 55o95 001. 5492:3: :-25o60 -1'26^95 20 10024 0#01 1'* 7 : 8 a 9 585 6 , 9 4 . 6 2 72 +43 v I I 10 51 21 22 4 25 31180 22 QmOi 1i o 805 7*88* 105 v-84 180 '3 1 + 0'39 m123028 9. 1 0 jjj 028 29542 ++35 Z3 :25 4 25 0401 129218 X 11 3.31 8o192 23•22, 1 43 *,56 0001 -00 5 81 5907, 24 . 0,24 3#031 -54 - s . 53 OFFOOR QUALITY A-139 VOUQHT .814 , SPPE , WIND _ 1LIMblEt TEST-620 WIND AXES f1/p1/-Al ngaq RUN .44 RUN 44 1*.5973 TEMP Po 76, Y/W RM/W ' YM/Q PSI D/Q PM/Q FNT ALPHA L/G I . I I , 41 x93 3 1^ . . ; 5901 : 2 ^ , , w 9 5 q- 7 6: 4 , J 3, - 14 . 7094, V 76 0 •0 1, , wi 67- 1 3 4 : •1 13 . 7 5. 4-73 3^.
4 6 t!92 36 lu;3471 .*2 412 3 # 16l l 125 -PI 64805 *0 w 65 "167953 4 -5077 0001 -44110 -14600 3#243 ke608 m K j69* , 46 0001 M50353 7003 5 -7#76 %159q68 3.510 ! t 9 *12! 5 O KI At) 4 At -- 6*768 6 w 9,75 cool -6#E56 3 * 946 - 171:3 1 4$L3 .50'#47 j f 7 4 8f § 8. 9 .
Q ai 5 78 .. & $.000 7 183027 8 831. 5261 •,14I'a 49 4 - '1. 3 7AL 0195+60' - 4 0 4 64t^ 56 Y2 9 S 656 0.3 4 1 + WJL4JL"35 7 0 .10• c50 0424 59067 2 30,8 9 -143*47 10 0 , 01 -0,557 3,198 -97018 17016 2*24 0401 0,433 3@274 -77;58 49369 1 0 132-73 il 1 c22 97 6 2 97 4 1 *124 - OZ_ 12 4*28 0#01 1,635 , •3 2 . !5 2 'S7 Q' I , 0 Q j' 4,,6 (a 2:5+ 05 13 S t. 1 1 -24 a 5.6 1 3s 9 06 i"I 9 J , i SLO .
050 . 4 9 o Ki3 2 s, 79 9 A 3 0 139 0401 6o065 4,686 16 0076 34278 -11 0,0 6 w140,28 12927 -16t14 0901 3o1:83 *14Q*58 0 -54025 7s175 5#141 17*26 50564 34# . q n 3o016 -20971 w136o92 16#27 0001 5,158 7J, a 024.25 * 133, o , 03 13, 25 19, Ow 08 6 , * 0 24 5 0 L K 86V w 33 0:0 01. 69.16. L -125048 9«' 754'' 69,00 19869 22 § 27' .
'0,01 2 ` 95 -53 0. 956 _: 0 29 0 96 11$ a-04 2,1 10 . 680 70 90 -35,23 123*21 22 -2*- V 11 * 829 8#047 98067 3t373 , 21520 -37* 45 23 25028 ovoi 1,24330 105*97 W113o99 8*462 22089 wi4o,33 4*932 24 0*26 -04622 3*186 -95oFR okol ^ryuow^UO'..6^^^ u o R 4a GG A-140 VQU3HT. U SP ED WIND '1UNKEL 'TEsT, InL, 6 .0 WIND AXES RUN 46 U/20J'E1_ 093.3 RUN 45 TEMP 76, Pa 14,.5973 Rtl /Q PNT At-PHA Pal L/4 U /0 7/w ' YM/Q Pm/Q Q•27 0.173 .
X 7.874 4.x353 15•,6:3! 19 . 56: *1351:62 50179 ' .x:1,•76` a+ q 1 5.437 V,-40 xil,884 4 . 787 40,56. *1460,54 3 0 01 . rFsL^l ^15a t3 M 3 • 74' 15 416 5.202 b5:92 6^168 r 4,01 4 41•.12 '*5 , 79 ,149,457 5,860 93961 7019 =-1,64,68 5 w 7,76 Q•01 "21 ► 307 6,998 486,89 1170,67 99052 771542 ell w 6 0 5a81 0 01. w 6 4 54 230 4 9 7.56. US w 17 8+163 `'30 2 7 wil*77 09031 , 26t05* .50+72 7;50,66 7'A 7 . 5803+ -4167907 8 M: 63020 18.• 78 0+bi wZ9,2'83 *1555.59 i0i71.8 124%1.1 7 . s34Z 66_v76 9 .x14.75 0- 61 4+7^ 11.441 aq V53'• .
.3Q,m 5 13396 7-1.2:39: 18 .
157 Q,25 0,01 20,.33 *7,975 44418 15,68 5!167 -(133.40 11 2.28 0+01 W 40380 4`727 4,197 -5.81 130.81 -188,13 V2 4,25 0401. 9 5 -1e j 8! 1 4+347 80139 -125i$2_^., 0 1 7,4 4* ".21 13 6027 001 1.36G 2:,:12 ok3606 3 8x7 at1240'$3 4+226 x.2!74 Q+..01 5.4 &.24 5.051 44395 =50436 3:s461 et1.27..35 15 0 01' 81354 _ , 4-$49 -10-1.4 X133'«14 1a,27 w69, 9Z 314;j$ 16 12,26 QR01 -12, , 45 *136.37 110700 5,441 -.90.43 313,4 14#24 53.01E 17 14, 792 6.336 3e064 -17 9 . 8$ w104426 p137,.03 18 16.25 0701 2*722 17.1301 7,1533^ - 3^2± ^0 " 24 wl!36#82 .:_ : 18026 15 0001 19.312: 2036-5 =26:911 8 o, 701 120.19 *130 +77 20 2:Q•C8 Ot,01 ` . 27+8G .21.36.8. 10.21.5 -125,09 .1 8558 - X121:;52 21 .22.25 0, 01 22.888 * 11 4 11.622 + 123.54; -107.29 0 9 5 31 _' 22 -38.:Q2 • 24029 0+01 24,673 13,129 -123••93 -111-73 23 25.2:4 0401 25.573 139812 209137 -99#51 -124,84 ^38'62 24 0,24 010,1 -7.94` x.. ' 4.285 19 +.70 0 134 #7 65 1631 5,1U8 _ C ., Qum -amm. FACE 15 purl QUALrl Y A-141 or.
1 0 - YOUGHT Leli4 SpgED WIND TUNNEL: TERT WIND AXES RUN j f2a/S1 09 l: RUN, 46 TEMP 76# Pg. 14.5973 MACIM Or.2258; QPSF ' ' 1:5456681 '7S•00 YFPS 456#29 RNFT 7 T09 Tie _ T02" 'T03 TO 4., TO 10'6T0 09 To I - 0 0 0 U 0 39 0 19 31 0 ri T2Q Tit g Ti3 T14 T15 T16 T17 Ti8 T1 0 0 0 0_.32 32 0 •CSRRZCT8 . AND. 1'NTERF'ERSNC E 5RFECTS.
, D Ftk TARS sct' s OaT F s ! .0 O^; PSI RM/Q ' YM/Q PNT ALPHA L,/Q Phi/Q Y/w D/Q y 2.37 v8_ 2'.i.t8 -i41'•.i5 0.2Ek0:001 -9:6 4#-551 , 42 ► ? ^ 0$' $r7( .• 46^85 2 ;•75 Cf 01 rw12#823 :7 59 G5 5VSt3: 0+3.7.9 Sca`*34. miis9e*9 0101 r. i7 .453 56500 g5 *94 6t4u1-' '^2M93 oo16906 0401 1421 154 4 • 5.76 4.126 i23«11 71234 0 494•58 177.•29 5 -7.78 01 .#23#796 7.276 132.16 7t692 8#C9¢ 57••28 ^179•49 6= 9.71 0.01 •24.988 80463 122 ! 05 6U:67^ !4172•:02 7 >•S1 .7.t 0'101 ,•27 tb9S 3.728 129.68 7#2#33' .
6.7`R4$: X1.68".06 8 X 3.78 S,9 *,a Q 0,1 • 34. 1 .250 IQ#3'$4 7 #975 Z18U' ` '70055 . 163 .4 9 : 1.4.7'8 0*.O1 .*32tQ42. s• 1:+x'7.,79 50468 21r94 •140#9;0 10 0024 0,01 -9,109 4.661 33.21 0!01 40329 54254 15.69 w1350 08 11 2 .26 5•.481 i0#50 44794 8#155 mi3lo iG 12 4#23 0*01 mi * 796 4,316 •1 ` 3.4 w , 2#'3#5 X3.01 1 ?g 36 13 b#28' 9 r7C^C 4#52t1 - #33 4°1,3..1.
- .
2cY71 -140'*.h3..;_
0: 01 ri18 4#729. X550.0
14 $#nc"U 3t981 X708( 31965 144w9j^/ :^.
1.5 Q001• .8#319 6i-Q& "$Q s99 , 69 •01,454,85 31847 -130 16 12#26 0#01 12o967 5+708 m i08995 17 •14.24 0*01 15#758 60636 ' 0 3037 - 1 906 1 Mi45o77 123435 3023 -24«88 _w141•-53 18 16125 09.01 17#997 7#800 -128•i8 .^ 028i!*6 S9 1-8026.04-01 20.:312 $. 26 1 x;132±22 s 8!565 -X134*4i t 5. -30*47.
20 1 20 4 , 26 OtOt 2 1 * 6 6 7 10 #,381 -1.3 MiV+v94 2,:21• # K10.40:93 21 "2 001• 234 1.88 1.20'166 ri. 23 4;03 0' ► °98 2.2° -37#•96 x+131•'02 22 22024 QsOl 23.053 124#24 4!033 1i#788 n 23 •24.23 3148$ -410 40 X10989 0 # #31 24#602 i 3.307 } i21, + 61 24 25*26 0#01 25#34i 13#946 x+123#00 31237 "40•, 23 0102•.43 O*25 2.1.•.92. -14c7*28 25 00,01 •8+362, 4#6:18 3_a,,q, S ORIGINAL PAW ^S A-142 QUALITY OF POOR VOUGHT LaW SPEEb W'!N'D- TUNNEL T SI-4-sil WX N D - A Xrz S it 2 .
0 0 Ru 41 RUN 47 13— PC 1.*i5573 TEMP 764 75#00 QFSF 'VFPS-256*29 RNFT 1,54566 8tv MACH. ► •2258 , Tot T02 TO3 T , 04 _ Q7 , ,Q6 ,T 0 1:08 TO —TI — 0 0 32 0 0 o o 31 0 T11 T12 T13 %4 TIS T16 '%7 TIE TIS T20 0 0 0 32 y 2 i `EFFECTS C00-ECTED- F , ^iR . ND TARS, A rNTERFF-MICE " SMILE SUPP P ORT DATA r2ATA 'Al C.G. SCAL6 D/ATA PNT ALPHA L,/Q RM/Q yM/Q P S I D/Q PM/Q YIN f12.3 03.02 X 8'.61 59-863 22.82 3x 999 0 .
-.1` • 76: •,02 w136476. 464915 Z * 4 8.1, *136900 5.31c o ' c oz 3 3 - 75 u18 .738 606 5
— 7 2 8
:4 04,02 w 5*74 39625 42#07 ' " 1394 , 10 0224836 7 ► 2r4 102979 04.02 48,•30 k o 149 @,96 5 '- % 7+78 *26 0 669 8*535 107#57 5OQ81
6 • 9#76 0402 W306 , 045 29o56 4o5b8 54043 Wl L ^L
10•302 4 .
7 vs 11 s 7 6 60' s, 76 , sw 1 49 9 , 05 0*02 X33 o 972: ;12tS99 106t81, 4 o 1 578 . " 0`.102 6208 '.1 4 6*6.4 8 - 01 3.78 " 360004 15 .48 1 14 w 94 41468 4.00 4 , . u I 6*t66 smJ48 5 9: ol k o 7E 06, 0012 -i37,136 16.8 ` Qo27 00O2 w 8o508 5-1985 22v62 4034 21P,76 "140*03 L 2025 0•2 W3,301.
6*160 1* q '- 9 3 - t 141#97 5#75 4088 4 . 0002 6 12 24 0.953 6 o534 So3*0 7 9,2 _»;142. 99 w7 o 6 1 1 3 69,23 -4, 00,98 M , J3 9 0 51 690 7 x•254 -2-a 31 4 +6i ! l w 14 46:27 Q't02 8,647 8..*Q26 -4x` 17 1',l 7't , 0 5 -a5 97' * 4 0 P - b 0-8 09 m K il$ 0, 1:2 . 11 4 599. 1 6 i la*Z5 042 450 11 3 2 3 16 12o26 '15*639 10,229 *55 * 89 0002 2926,14 m 11 9,9 9 *1346.44 17 • 14#26 » +.59 00.02 1,8#673 11*809 n 6806 2 v 5 3,, 9 1" 1 5 #, 10 ' 131 18, 16#24 13#536 m 77,59 2*270 -19 o.42 -?125992 0002 21 ,099 13 18.# Q.02: 24 25.3;99 ' 15 * 5$3 - R 8, 9 1 t 967 -2* 77 r 1 2 *2 V - 9 ^) 87 • PR 30 - it i .20 SO # , 26 o 883 -95 f 58 - 0 vOZ 29q2*2 17 2? 084 X124 . 85 2 6 al , .22-27 'o to 2 34.089 P-1 w02U al 10 6±5 6 . 5 olU4 & 1 3896 22 24923 -53 * .38 "14*&35.
0 0 02 40#881 249660 • 127#75 (x%474 1 9 It)2 FS 23 25V22 OoOZ 44 * 5^1 26#580 55 6 -64 -146,80 X 1399, 24 C I - 1 27 0•02 "8#475 5*965 3oS6,7 2, P 1 , 56 )*14197 7 2 3 A-143 (OF p om ugun p B -- u v, YL!?UGHT LaW SFE5D WIND UNN I F-L TESL 63 _ ...^ WIND AXSS RUN .8 RUN 48 1/20/at 0933 TSMP 76. PC. 14#5973 qPSF 75.010 4 256x _^29' 5668t MACH 0.2258 YFPS . RI F1" 4 5 TOT
T1 2x`03 T04 T06 706 Tal 109 T05 T10
0 0 48 0 .12 3 0 0 0 1 0 T11 T20 T12 T13 T14 T15 Ti6 T17 T18 T19 0 32 0 32 0 0_ i 0 Q 1 Rl5CT5 3 TARE: AND :fT'(5R2NG2,'.2FP>r.CTS 0 `, FOR : 5TNGL1b SUPPORT ,1 d?
'' OATA 'AT C G ' ^FLLL. SCALE DATA_ . ^- PNT PSI AL PHA ECM/q YM /Q 0/f? PM/Q Y% 0*0 OsUi -8*751 21,:59 0..
560. 38#84 44Eiut oi *3 05 7r t15 2 *2.0 x.:515. 2U«i6 Q« 2x4U5 -141,«70 ?4Q#02: 3 Q*2.7 '*3 ..98 .9.433 19.:63 3.358 4 ^2i : Q^C 93 ' w137&32 __ M 0#27 -6#01 *10.006 9.754 x 3#226 220 3 45 0130t02 u 47#60 5 Q.27 0 80-0 x x 6#568 21x54 9.561 10#168 43.99 x110#11 6 0.27 .+8.766 -0 10#02 36.3}8 mil#023 29.,45 y 81,P98 113065 -_f , • f-96 ow k2 y00 ^.! 4 Q 1,5.3 17x 84 W7 # 62'5 2.1 26 3 87' 978; 67` 8 1.5 w 4o Q • 2 X14#00 . ,06.5$2. 1,3•.166 X8.17 - ,.294,49 0*26 ;at, 1.6,:f11 X4.880 14t6c7 8.04_ Z4t226` -14%58 2 03 x 18400 10 0026 2#459 x2#58 m2$i07a 11689 30081 0 16x585 9#,38 62.1, 8 11 0426 -0.305 #+o-a31 629 -200-02 18 48 84 -12072 i2 0025 *22400 x23#50 1•227 21+551 80+32 0 38!677.7+69 13 Q:.25 . - 24# : 00 : 7•,18 105:,03 3.039 -24 # 454 *^. 9 92-5 *43 t 5 343: .. 26x00 0,32:6 3.598;6 n t470$.d3 804 27#301: .28068 '::1223.$9 1.5 .x` 13554 0 C5. 0-28k01 4,.42:0 304*86: 030 m-5y 9S5 .
-1,*0V12 .16 x 30 101 0025 *55060 249,18 3. 423 33.947 x 1 .147.68 s 42 e 17 0.25 -Ott , 9.527 18#91 *8#284 36.40 5 4 018 '"143#-33 i8 0025 2.01 7.848 «659 6#787 16.77- *127# 35x21 70 1.9 4 02 12.4 85.
0v25 '07.479 10017 °`x154 15 40 31x83: 8'.02 20 ,0 . 23 21..70 45#580 20 k*3 sm1 =6.515 11 . 94G 54320 21 Q. 23-> 10t(11 W5r8 2 * ' 1 2.1,13 1201 , 9 '19 f,060. 23wl . o ',169 #:7 Fs x x 22 Q#25 12*00 23#228 24#-8`0 *193931 5#011 1.3•232 3.80 25.:50 23 Q#25 1 3 Fe01 *5#68 -3.743 27#876 *217x23 •14 4660 24 0#25 x•2.343 25•:72 1.6#01 1,6#327 *16#88 .33#827 8244.63 25 0.25 -0 r * 28 # 03 58 •:00 28.925 337 18 # 429: 37' 92,0,2 -(276 x70 y P-6 . ' 8 tOl 86;, 0 #2 5; 1. t 6:2 .. R3.7 r75 4at.$06: 37 7 a0 #l 58 -25Q*'037.
2:77 22.x00 20«66 *286 0.25:_ 2.659 23x285 ^,413'99 *7F771. «22 28 0&25 2 3 4oul 26#313 4.750 *48956 52#786 20430 *3';14#86 Q025 16.;62 29 26001 5.784 x45#63 57t2b2 #70 294524 *337 30 0.25 28400 -361t28 5.653 32.798 x33.,13 61. 2*2 9907 , 31 . 0925 304 , 00 •6 4x1;.$ 3.4.25 35x856. 63i -3679.72 ?"8#,72 32b 32 0.25 x 04:01 x-8.212 37.124 2V 37 ► X 0527 .4, t 738 wil+4, 48 'OF J P OOR A-144
QMITY
VOUGHT Lmw -SP2ED WIND TUNNEL TEST= 630 S WIND AXE RUN 49' 11/20/81 0921 RUN. 45 #-6$62 TEMP $5.
Pd 1* QPSF', 7 5. 00 . MACH U ► 2254 YFPS 250471 RNFT 16R906 7+ .
T01 'T02 T03 104 TOB Yoe To T cry Ti0
9T
0 0 39 0 U 0 1$ 31 0 0 T.11 T12 T13 %4 T15 T16 %7 T18 1'19 T20 0 0 32 0 .
32 0 0 to 0 `EFFECT's, C9PRECTEQ FCR TARE AN0 TN:T'ERFEREN(:E SINGLE '^u^?'OR h11^ ^, 't^ATA' T' ^r A e. E; DATA. ^ r^] FULL, SCALE a Psr Lr 0 rl M v^ ttM^r^ yM^ PNT ALPHA PM; Q 4 Q#26 0*01 n 0 : 5±652 84996: ".1,63$;4.9..
0919. - X 97#37 Z . w i , *74 . 0t0'1 93 3.5134 4*130^ 4170+59: ml 112930 1 -3.76 p 01 02.645 2#962 W 6 ZZQ 37:80 -'176'•75 - 32.76 4 0 450 .
-5.76 3,776 3.110 70523 84 01890.25 0401 0 1470803 5 0 7#76 054125 530,55 3.456 0 1.60482 StE57 -1990,96 6 0 9035 0 #01. 06.435 8 03. 60#10 0199o06 3#871 0173.43 73 -7 .;1.39,$7 04, 3;. 77 0*01. 6.6•,6* 7 90 1 0183.37 81o o9 4 • 461.
8 0 01 8 3.77°' 1 ' 0 00 9046. 5 ► oo 7e1^1. 71:7" iS'1 i5!5,.08 X191*.8 9 X14.7 O O1 73#74 -"18 8« •^ 45 5 .^ 6k5 " 10 0025 0#01 0 51633 24081 04556 20885 096,26 •162'0-40 1,8487 11 2026 0001 00568 2,945 080 0 81 50128 01520,65 Sat 44 5 0,01 2 1 0 67 9 m66a? 0 h,.66SJ1.,,1_14t51 2.•5 6 0ililo17 4#2b: 1.3 G?0,01, 5.,82 2.679. a 4 08 Ow -1139.30 K49984 411.4 14 4, es , •01 3.. 673 30540 00.1 -t137+:6 3*356 M32 28. 8 100: 86 0.01 N 82 15 40588 3.591 *l4#34 ni39.85 +1^^:. "`4 16 .12#26 0001 5#631 3#88.5 4463 0 1^7s43 017 3#68 147 17 14.24 0+01 66808 4#274 40841 W 154'. 93 0150,33 13082 ` A Pc1 5 18 16#2 Q o 8#065 2D..9^ 347 7 01 4.Z7 356IR 4o 9 3 1, o„ Y 15 '3.R o 27 1 30:76, 50758 51.r1t1 . 0 0146«18 - 34*,(j8 340+65 30 :2 2`$ 0.01 2Q 69364 -27,78 10#355 670,53 3.r 471. #.14.2*81.
21 c2 # 26. , 266 0 33 044 0 1 11.445' 7 e 1 3 0 .s 3 To 9.2 0 0, •24«27 0 001 x+340,55 01,25042 1.2o434 7#916 56058 2:5xo 23 25x27 0101, 180022 80394 lo880 *+3609 =1,16423 104442 -97 24 0625 0#011 00.556 5#563 24x!85 % 2x918 6 1 2*92 .t* , 6 r ^^ E ^^ A-145 VGUGHT LMw , SPrED WIND TUN K I EL YPfi ft3^ oak s r WIND AXES U RU TEMP 610 PO 1496759 PNT ALPHA PSI L/Q D/Q PM/d Y/W RM/0 ' YM/Q • 0*01 too. o59 1K '' 2.852 - 5#80 1.1 0 0x.656 ka•25 c ^0i 33'131: ^1• 1.672 2s &34 . -1.76#;71r
il7t..5 .. 44k72
s:`rM .^' : r 3 Goal, 4UA78 '-2oA46 2x89 132#52 70232 -+JS8s05 _ 4 W 5075 0*01 48x95 -40108 3 , 143 84262 •203064 - X 146#•14 0#01 58#30 5 '-7#75 050391 8#8b5 3e390 -212&16 m 157#24 .. 9,741 6 Oo01. w 64-44-212,97 2#912 70k24: •M 1.1 t'7b 00i *8#233 *181 7 4•a 4}27 8e 4 ,36 "209017.
f t i 1.
3 5#9 13x73 `t41 : ^9^^t1$; 'J'S9F,03; - 5 «.210 x+'.1.9 1: t'$9: 7x519 9 ^} S1i 77 x 80 14. .1Q.383 5.555 IW197.26 6.s 9.* b -1 .9 61.
..
a 260 4,l ' ?7 0*01 000555 5 1 698 24#77 20819 0 9909 -166x43 11 2027 Df01 fi 0435 2#875 5t.:4x 17000 o A 8501 wi57 57 2 40 *a 0 a P . 1 34 ®«74 w148--26_ i. 2.963 w69!47 a8.1 ^1 41 4 2 &. IK 'Ra als'2ffP SrY i QQ$^,'.r' 'Oy 4 1, 4' t^42 - 0 44 a' CY2k, 0'otl1. 356 61 v70 -1.41o61 2 p ry ? n t 1.C$ it( 15. 1w0o k : AC• 9.` "d .^..,..,e. 6 #i VJ^ .^} [. ^.a....^^..,t- '^:^.t`.C, ^ k ,. ^,.5t6. ^i,. ^ G 1" 7 4.
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54656. C . .
48x47 w 33t:2 fS 204es 41st1; X1.55 20. t 423. 6,- -F 3 6-S X16 62 49 4•. li 21! 2'G«2^i 11.,41L ' 77d1^ z a^^f:G *v8w4.0 X149 #• J ;' 70 : 165 '_, 22 2 8 0 # 01 12 # 5.#12 8 # 057 3 I C52 0 43 024 "13 8 # 24 91 o 67 23 25x25 0601 -44,, 75 &!029,;33 120985 8#393 96@84 2x4 , 40 0#01 240:23 24 0x24 • 0.624 26885 Alofs4.9 : 50667 &1660.84 _ PAGF. ^S 9'. 7 .3AL et%(C- 1 A. - : 1 4- OF POOR QUALITY ' WIND AXES RUN si il),20 I,S TEMP 644 pet 14 s 680 PNT RM/Q ' YM/Q ALPHA P S I D/Q PM/Q y/w L/Q I 2x6:20 r ^ NB , 73 23v85 41159,52- .0 1. 0,4 if a 2 a a 26 0 63.,$ 17x65 9#-36 2 .4 4w w:1,0.*., , at , r6 39 '1,4 .
.3 0#^26 ;-400 i-o,ff2a 2 , 2 o4o, 106,68 ori 40m,74 9U 11 _ # 17 4 0*26 -5o99 8*40 w15o*il 04167 3#106 w1,07o25 -2*8*8 5 1•,16 Q•27 "8 1 00 3*703 w11*o16 -6#326 0,618 -1132*06 0*27 -9.99 w5o36 • 1 09 " '''v ___ 7, 0: 27 w J2 00 1009 1 :: o v 5, 1-10 a : a .
8:72 1 3*34 o i4tU6 •-95#•87 01 75 0#27 0. o6. 86 w37 6 -12 -76, 6.
7#.191 i t 1,.04432 w 1 7 2 -9 9 0, 1 27 .^ 0.'0 46 . -89 ai 1' 5 t lS & 59 8; 2 0 o6 6 9. 3 & 052 -17* . 99 o m ogO83 10 0*27 -12r74 -39*75 l04294 m 76#9i w23o584 0.27x + 11 w Oo280 12*180 w 65105 * , 27v6U7 w 10*80 m17••51 -7o,90 12 0#27 "E1t , 93 "0.43 , 2 5 1 L & 7oR 3 1..
3'7 -1083 a • 27 1, 6 #865 oaS i t, 8 : $ X35 Gb 6. 4 ves : 1,5q,85 `23 0 - 9 9 00 0 # :549 s 1-4 01 , 2T' =P ST 9 9 0.9 32s2, 4, .
iS 0, F 27 0 7 o-o,,64. 4 6 6 *,4,00. 5, 1 4 1 0v27 -30%03 100 , 44 -0, 737' 25j750 9,23 *45t671 64 •,50 17 , 0#27 0 0001 w oo242 2s6ao w 10#3 1.46 5 365 23407 w159996 18 7 a 6 Ju 6,2 8 0#27 2, k 01 .0,180 22482'9 30 -;1 6 1,36 • Q; 3 379 51 V? 2'7` s, 99, QsOZ4 9 t $vS w1,6i*99 3#14U wi07,77 0927 $ 49^65 J. 4 8.t91 r9 0.0 157 3•,5 : 65 ^ 01x:3: • 3.1 70,98 ai 0.27 0: 0. 45 . 07- E; 5 .9- 4 46 3 o; X50 * "a t, za . 9 4-93 0427 1 • 015 1703*8 56%.13 - , 168o,65 4*831 -126#68 23 08 , 28 I1•-98 *185,08 1,'368 2002V 61,,.6 ; 5072.9 -a 1 29.5:3 2 0 * 2 8 140, 00 664-16 AL83 7 ^- , ! --1 2 .2 4.,w .8 Z; j 4 tP -5-o-20. !!Ll s S.
1.5-59 0 $ ^ i es 0 x 28 669,71. w?-071,68 , t 921 23 5 .
$ ' *113+Z4 2'6 000: l g iou 10 , 3 0# 677 :32 x 669 65,7' -5Z8. 9 7* 5 F, 24. 4 0 tk 0484, 1 2 *41 L *41 0 6503 -36*667 -84a #18 66i.52 0425 21 439 -0&986 l4t668 -64r,60 411117 w280461 2- 9 0 A^V 23 o , ^1 8 -0os76 16#920 62w-63 -303091 w 43#36 44t82$ k ;:ZlL 30 216002, 1 s2tsa W32 02 "24*9 45,15U4 - rz, 28.0'; 4 4 wpi ik• 7 22f, 4^ t 0 z 5 1.
5 22804 I1.0 lzl wl6lci.8 9! L ^^^ F OR QUALITY VOUGHT L8W SPEED WINO TUMNEL EST 6-3o..
A XE S
WXNQ RUN RUN 52 52 _ 14x6808 TSMp 66# PO , ACH 0 2252 75tv0 VFPS 253. b 158T49s# M QPSF ^ RNFT T02 T03 T04 T05 106-1'o9 T08 TUS 71Q OT J 0 0 32 0 17 31 0 0: 0 T19 19 `r20 TIT %6 1 .
1'12 Ti3 T14 TIE T17 ^SZ SL_ ^.
1 0 EFFECTS .Fee , TARE x T f^F REN E 05 RRECT2 ANQ .
SQALE DATA P CRS' - OAT,& PULL SlbWLE SU 1M; PSI 'Y: w YM: FNT ALPHA G/ 0 °M^ 0 l,J Q 0•.Cl2 3.«:/E " 5057'1 21x74 81619,29.
1 a«28 6#:816 . ••11 ,3.49 48 iQ vq1,65o,54' 3.0;886 `6s 825 Q . 2..867' ^134woo .+971. 17 34 PS6
' . ali - r t aAf 14
3 X 3.73 0 02 w0 x738 9 F 6 t i46 «15 0.02 69829 42 *174.97 i 4 -5.76 w 4.533 ,255 *170+04 49+50 0+1814-34 5 002 -8.562 4«663 8 69930 ' - 7+77 *+1 4424 -*189.96 0.02 1g6sa4 7+540 56•,4 6 6 -9«77 mi2.974 5.8244w19 Nq 1.8R 42a 63.67; 0 02 ' 4184496 7, 462 -wi i ••76 6:020 420* a x 69792. 6 9 48 1 17.9 Q5- 8 -13#77 0•.02 `,.23x711 7#253 . - 21.3.'71 C i 34U 71X95. ^17+V «i3 .
9 'P 9.02 . r2 7.083Q -216 # $3., , e i 4 9.74 0 9 b?, 2i#•50 5 # 571 X161.17 Q4:02 6,'781 10 0+24 4+00:9 "113+34 0 402 59,437 16#.a5 -+156.96 11 2+25 10 o„G5 46324 *+93#50 w 4R«!^^^ 10« ,9_ 12 4927 0-.0 2 13.613 w73#09 - 50121 /1'.•578 . .
3.=85 ol 83 0 02: 16.6*0 5« 083 ^ 4#554 1.4a 6.26 °+*54x77 .34,81 49St^6 ► =2e,*$- -1.39.30` 14 $.23: 0«.n2 5# 52 19,83;4 r t ^t227 -1;(1v49 -M s, 3604 , .`1092 7 002 ' 9' 6•`774 12 . 5 .
i5 23 X75
5,396 w 1 o 44 w1339.08 :12.26 00:02 27x624 6 , 16 7.914 7«83 -^S29,,1,5 5039 *+24*75 17 14.2+4 01.02 30'#650 90609 27t68 36, , 19 6.86 5 ` 1 16«24 06.02 3i. 533 11_.190 42_066 •±126.99 " 18 "330.71. *1.39082 19 X18«26 0r02 i34869 - 4 9U7 28,941, 52.#. 16 X36`.91;: 20 ~144 x90 °:20.24 019V 3Q 245 1_5,715 4 8777 63 •.26.
042.04 21'..;:22 #25" '01,02 75.16 5x205 X151«73 32.262 ..17.687; -52.:33 w154'#27 22. •24.27 002 34 # 550 84005 6,048 19+969 *60041, 86¢60 71Q12 23 25026 QCO2 354918 21+195 -151903.
2 1ts93 _K15 8.a8 0025 '0402 6,615 4*003 111,14.37. 5#331 • 24 ,WAL PAGE 1 omi OF POOR QUALITY A-148 A YOUGH7 L.AW SpE'ED w hQ_ i t 0
ru,N t:,i- Y'2''s ., 60
WIND :AXES
FNT r3i
ALPHA ./G D/Q PM/Q T/w n"7 0 i %w L C.:S" 0902 5.604 73 6x881 4r'5b s ;OSR39 i^'•02 ;. $9. •
? F ^734 3.$13Q 28 ^ri61
4^F'.^F 0.591: •• 68 3 _ ( ; 0 Ot02 -,16gi77 3.74 -40.737 3.94 .153.96 50766 33x29 4 0.02 39.45 -4.366 4#255 6tG96 .165.83 "5.74 x171.30 5 -7.75 0002 w 8»394 4.596 w185.30 6t6b6 47#-20 4172971 6 "9082 0..02 x12.879 W. 2,0369 55•.52 w 18 i + 63^ 2 ?^ - 19 4 • 7 1 00.02 'w1.^R2b7 6:i^86 7 x11.741 5. 993 .179028 9+204r9H 7ti5 8 •:13.7 f t.02 6.6oi60
•23. 408 7 9 20 ^2 ^^$;1¢ 6+t8 -d17$*i6
g ► 14,76 0.:02 *25.970 7.fi25 •2ika^rt 4.392 69 4"3 : 2 rti58.10' 10 0025 0.02 6.715 22t:U8 51538 •+159.21, 4 . 142 W 1 i0•.03 11 2.25 0.02 4.378 10.158 x 29 ®69 qt'- 4 37 1:6977 m 1,54 e52 12 ^F026 0 0*2 5 0 1 3@ 411 x+.704 w69#96 11N8 5•CQI a 146•$j-,._.
0, •: 6.2$ 0:02 5008 o 35.,19 16.605 .
15 14 .5i+£i7 ,. 4t,4^t7 14 $. QR02 : 'q'k9`*9 '. eo 00 2, 5•. $ 'm124±49.
(^.0.
15 1.Oi$ 23 1681 x 5• 09' 6+_706 .9v.i5 16 .12.24 09.02 m16o,23 27.646 7.978 5:375 wi310.14 12411 X7.02 17 -14.24 30#436 51919 -240-45 941409 30843 9131.79 1.S 16.26 04 .02 31.916 11#352 45.62 6#709 w 36•. 33 x126.30 ar"15 .
1.9 0P.02 :. 13'6}54.
29 ? '140 1.3 9 978 56 * 47 4t'I3 -3 1 99-
20 2Q.2.4 0402 30.671 15.929 59t? 34,06' •14c :.2g 70.14 J44v ,85 Y X21 .22e21 0.02 32 .065 '-399.22 17.769 81 6 - 4.506 22 224.27 OR02 9 , 99 44 3 -4802 19.829 91.32 'S!8.U2 w147•i2 23 2 •23 O•:02 35.527 21 9 026 6t564 -654,58 x 143.67 93 012 24 002.5 4x02 6.748 5 8391 4*082 9109.33 22.27 (159071 ^fria&r.^ui 't -5,49 A UP POOR QUALITY T "Q YQUCHT Lew SPEED WIND TUNNEL. IES WIND AXES 0933 - RUN 1 /20/81 RUN S4 J _ 14t6857 PPJ T M 680 MACH 0+.2251 oPSF 71 SOQ.,Q 253#60 RNFT 15801561 YPPs 101 TOE TUB T1 I 102 T03 '704 T05 T06 ^.
U 0 0 32 0 0 0 0 15 31 Tlt T17 718 TIS T20 TiE T13 T14 TIS T16 0 0 0 32 0 0 1 0 '32 $ ?NTEPFERENCE EF,:FECT CSA ftECT ©F5R .TARE AND 7A :FULE SCALE DTA SUPPORT`,DAy,A QA.T'A 'AT TA SINGL E RM/O /Q PSI L/Q D/4 PM/Q Y /'W YM PNT ALPHA I i^01 1:•40 0.21. 1.p -0_#563'' • 1 a ua. - 98 4±833 x10,96 .: x'(7.90 2i91 -7.^^'33 50 . 059 28e(6 -101:62<_ 2 .1~ • 74 ,. 0.;02 - 0 .
0 x44 1 86 3o 77 .014 3 < 0'0.02 *13.761 . 554 .. 49 -1.028 L5 aw U5 - 0 075 4* 55 60286 4 -5076 002 419.578 68196 -5R1 -0 0;02 1 *.36 l` 5 ' 7.601 72.39 '-7 075 002 .24.588 -09894 2x04 -0; 6 -0.5 6 9076 0002 w29007 02; 10 - 0009
-x',771
7 .340471 84 * .$'4
wii 77 : 002 11 10 0 354 2 M9 095 077: 8 .13^7T Q,0,02 'w^F3t 26 ,120281.' 95#33 -11281 3-042 r4 70, 98s56 1.519' 9 wi 4 7.6 04102 *4 42 :13..332 10=03 .1 .,74 005401 - 00102 120.03 - 10 0.28 -1 0 297 40940 00868 -0+86 -00.38 00.02 2#26 40043 40967 4126 - -0.:72 -1*18 0002 soiI4 -1.08 -00836 12 4 . 025 86500 • wi-- U8: - - 0083.7 2047 60 . 0fOS 13.486 .13 2$: 5:387 - F04.F -2..0o f .3.56: 00;02 `405:95 1* St26 17 0 755 '6.015 00!5.1 . _ 3*56: - 15, •5.335 i0m,23 ;w 0'+2U'2; 10i25. 0 t 0 Z ::22.305 •2'^ 5 ^ ^^W -1..26 -4x6,4 16 0108U .12.25 002 260353 8.125 35018 -6r30 002 0+577 1+53 17 •14027 290179 9*608 57002 -80.90 --6. . 36 18 0002 2.23 1.0661 16028 31.973 11 *438 _ .
- 446 2'.=40.
.13 19 48.27 0. • 02 34 0'1:08 V 14 x817 r99 -U s 438 7 -2y67. -0,0.8 0:,02.'38•-1430 -'/F9t37 -09,868 20 , 20..25 17-526 -3: -0.56 _ O e 661 22.26 0..02 42 * 415 20 ! 385 ' ' -77 -65 0, -3059 -50,53 00.02 23.504 OvS96 22 •24*26 46.554 -1:06078 -50.65 -3067 10186 23 002 490839 250648 - 25+28 1190. 94 -0V9.9 2.39 13.38 -10134 24 0*27 0.02 .331 4e873 - 1 'I ORMWAL PACE 19 A-15 0 OF POOR QUALITY YOUGHT Lbw SPEED WIND-TUNNEL TESI b--U WIND AXES RUN 55 11/20/81, 0933 RU14 -55 T5MP 70# Pe. 11 + ,•6857 .75 OQ VSF^ J57?,61,4 1 . VFPS -25400$- MACH 0 22 51 9NIFT TOY TOR T03 T04 75, O_ - T06 T01 T09 T09 TIC, 0 -32 0 0
0 iff 31 0 0
Tit TIZ TIO T14 T15 T17 TIS T TEO %6 I 0 .32 .32 0 0 0 1 0 R E WERE IN .9 NCE EFFECTS: -:AND p EcTED -Fck TARE T NT SINGLE SUPPeRT .DAyA SCALE DATA 'AT Cody DATA PNT RM/Q ym/Q ALPHA PSI, D/Q FM/G L/Q y/w 0: 02 gw23 1.831 1 5 o 63S 00"64 Q •:27 ZO ^7$ NR 0. 163* 2' - 0 009, 36 t. si x.300 8#785* 35 04 , x.669 02 7 ,- 3 .
.78 0 1.02`'' 14 0 :^ as, 3 x1 4' 0 11 8 9 i8 1 5 20 , 0036 ' 1 4-93 4 5#78 0p' 02 020 9 018 m - h 66 9#752 68#:59 -OP939 0q 5,07 0••99 7 79 • 0i963 4028 6 n 000 2 25o3 5 1 10o847 73o80 4 4 4 6 9 * 73 2 19 0 •.02 w30 a 00 6 . 12o126 71o37 _ O R564 7 :1 0 "'Oa *11#78 266 .41 -0186* 1%16 -, t ^a7 # M9417 o 7 13 7^5, q 07 ..13. . 91 76: 0* ' 02 W429 266. 16 f Q - 8 2 78•42 1 : #2 9 y -0046 .•5 . .1 4.7' 7 5 . 0qO2, 0 4 5 o 3 5 S ' a ! ! 2 , * . 76 1 :6.2 4 5 . 4 , 9 1 r518 10 0'k.02 Q#25 4 20049 M O*63b -1 q ,20 09,29 1 •665 8*605 11 000^ 3.777 -Q *-OO o - le-94 2127 8#701 14f1,i 0 04524 12 4028 01 , 02 9•.24 w 0v469 0, , 47 *4001 8o737 8.882 la 0.02.
1.36315 10t01 -Ot*Ob 0 %38 .*-, , 36 Sal-84 9 F782 i*t08 10 0: 028;• -0 944 -5*40 8 0 26. 178 .
10 ,, 24 0 WO ?. 220436 .b38 ., O9364 -203 46.o2 10 24s23 16 12,25 w3l50 0*+02 26.420 11P758 0 q 4eu -2* , 64 43092 17 -14,24 0•-02 29 * 721 ; 43 "4#,11, 13.051 0t530 1020 71s 16628 - - 6 * 56 0 9 02 :2. 293 14, , 691 72#63 , 11161 7mO3 As 0."
1.9 18: * 26, 0902 34@ . 380 Q ^35- ,P 18 . 1.23 0285 -31 40 . 20 10 .3a0 243 ZO, 9 5$1 •, 30.05 -'01065 -1 76 - -002: 21 .22 o 25 0 LG2' 420 , 476 : - K5•,85.
23*417 -66w89 "0 9 186 0 2+ 22 -24825 0 •-02 46q4O2 26*535 -85 0+4 1 #46 o7t\56 #28 2 1 2 3 25#25 -6*51 0•,02 48 .653 280309 miO1901 11480 -3'35 2 4 J + 0#24 O •: 02 4 i * 532 8.6 5 40• .23 0w92 0 2'0 r7 ` 4 01 643 OF F-COR QUALITY ..
A-1$1 VdUQHT LM .-- SPEED WIND -T-UNgEl-lZBff-,630 WXNQ AXES RUN .56 .0933 RUN 56 pa 14. . 685- t TEMP 70# : 614, t MACH 0x2251 qPSF 75-vOO VFPS 254(08 RNFT 1. 1 572.
'x'0 8 TOt T02 T,63 T04 1`05 106 101 109 110 0 0 :32 0 31 • 14 0 T20 T17 Ti g TIS TIT T12 Ti3 T14 - %5 T16 0 T O 0 1 32 32 .
' EFFECTS INTWERENC e , CQRREQTED F6 : R TARE AND l SCALE U A'T A - SUPP f JRT:,UAT ,FULL; :SINGLE ' A DATA - 'AT C*Gv 'Y/W YM/Q PNT ALPHA PSI D/Q PM/Q L/Q 6 0 1 02 9.1 7 9*787 $7s, : 91 30,58 -2 0,56 0402 Bo856 4 w 5#79 4210945 96r69 0 01292 40,38 -01297 -1h46 6 w7o76 104806 01-02 o47,478 107#. 34 03691 34,66 6 0-.02 09029 -9,75 -(32-368 . 12+319 102*86 5 *2 3 6w 65 0 OZ 33o05a:, QSA^ 1, 1# 7 1305*^ 904, 79 0
5i07 30
8 •1.3 074 002 -*43 4 452 , - 9 w3a ' 4 5 - 4 0" G2 • 14+ '7'6 . 45.'732 16 7 7 86 - 902, 0-6 alS 1 x45 -10.63 00045 10 Q 25 0 o,U2 .-2@908 89560 41o1S w12 t.98 QOU6 1 +14 11 2,26 0002 . 2*610 8-774 32#47 0002 09427 x84 . - rJ6, 9 8.942 26@08 12 4# 27 7.395 3 r a 6*06 - 17o-30 Qs- 02 ! 18.419 9 +230 0# 7 - 23 + 35 1 . 1 + 67 : : 3 8:33 33 ^59$9 0 t 6 ; - 2 *06 -15 6 91 . 0 .
..02 10x8'25. 825. 28 * : 67 00875 1Q• 28 21. 514 -9, 55 16 12928 0#869 4t4 4 )
11,e563 301 . 24
0602 27 q G96 -6.24 0.6089 * 148 17 •4927 002 311610 13*282 26-21
m 10s , 4 7 -40w24
-14@993 259.59 1'#736 18 16,26 00O2 34 * 059 .
.8..54 -6+*-- ^ ^i 54
19, X18*25 0. , 02 : 35. , 62* I8OG85 1 s30
M 2 0 4 (), 2 R 21, -1:0+36 20 .20028 38 , , 20+ 697 7 8't 834 4 8 : 9 . ' 0 : 5 .0 2, «7a. Mki.0 80 0&02 41,881 2:3 4284 m69*43 0114510 .27, -16 , 49 . - 4 1 2 * 53 24425 Q9.02 46q573 .260327 w 88o31. 1IQ22 az •9092 a5 0-35 25025 OtOZ 48-072 28#321 -101 t•45 1#847 1,80 m10t,16 09-02 --2.875 841659 40s79 Go011 24 0024 --I A-152 YOUGHT LeW, SPEED WIND TUNMEL TEST^gO WIND AXES RUN RUN 67 p f5 14e675 TEMP 70, Rm/w YM/Q PNT ALPHA D P S I L/Q .1 GO 2. 2. 42 4 ,92.E 926 0•:02 I o 7 5 3+76: • S.496 0 02 `' S r 693 6, 9 9 a 64, 3,37 m49•34 4 -5o77 002 w21s14* 6#423 -04737 3«08 m5t37 Oo-02 0260218 7,6 1 0 7 iOSt35 -04584 6 ' -7#77 0:4 *019 '0 9*06 9.199 100.52 "01 6 09#75 0402 031s261 „50,80 0 '0y 7 n 1*77 0•.02 0R956 - - i . - . 0 tO;^ 4, 1, 9 w37 # 744 1 ~ 05 -.7 *8 7-4 r4 l *,o 4T 11402 S wl# 7*6 0%02 a46 i99-q lAkwiC3 : ,i i 6-, 8 g 1851 08«64 io 0 24 0,:0 2 -2,375 4,900 33015 -0t489 ► 04,02 23o93 w O#32Q 1•i, 9 -12#-70 11 2,27 20910 409 1 + 1 0065 Ia . . *,66 0902 -0q240 12 • j f 0 25 7 * 793 1 5 .0' 5 o 1,75 2-, "151.79 12 1 68*, 5 6 . 2 loo 6x -Qt g 13* 13'«34 12.0-6 7 7 15 laffi , 25 0 ' 0+02 6#98-9 15 ki, 2io 16 -5o67 =8 e-2. 9 84196 12,*27 0k02 270228 17o( ) 4 01449 *1 89 w69-.95 okoz 21460 07 17 -140E5 31,581 3,713 120o2 a 0k02 34,391 99,63 2*049 -129,15 5 ;, 9^4 _, 18 14424 11.544 .
-6*38 19 :18s 2* Q*02 $4064 4 466.1 a-3 9, 4 4x3 1 5 w 7+73 -1 a 1 - 3 • 17' -7 c 99: 20 X0.29 9 to 38,9Ot '00 i t' ! 4 , ^ 2 9G -I w32- m1 4,54 1 22.27 41.935 1.1 Q 0 * 02 -20,l 12 0 0 8 7 i 22 -24,124 0•,02 46 * 235 0 10705 030 0.0 010*07 23 , 233 -5w94 otoe 1#279 -11$25 23 26.24 48,928 25*200 W 120•53 1*67 24 0425 0o, 02 w2#608 40993 33i45 0 01662 -8-.14 A--15 3 OF POOR QUALITY Tk4N .L. sT 630 VOUGHT LBW SPEED WIND ,— .AXES WIND t RUN ,.58 11/ 0/8i 0933 RUN 38 PO 14..6660 TEMP 700 MACH 0x2253.
a:PSF: 75*00 25025 -157061.o YPPS RNFT T10 T07 108 'Ct T01 _T42 X03 T04105 106 ,.^a.^.`..
0 0 32 0 11 0 U 0 31 0 T20 T16 T17 T18 Ti9 " T1t T12 T13 T14 T'15 0 0 32 0 0 1 0 U CTS I'NTERFERENCE EFFE CORREcT50 Fe y ,TARE . AND DAT A SINGLE SUPP-aRT .ClkTA AT'. C o3 FILL; SCALE ^^l7ATA RM/Q pax Y/w, ' YM/Q FNT ALPHA D/Q FM /Q L./Q 25846: X164*86 0.23 0w00 54 4 #73 n 3.009 5,567 38V13 X164«3 2 i#75 000: a^xp68 33+.2 : R X9.09 5.780 5721 3 ; :. #4,4$ 89:4 5 0 g 1 66 i 3475 , 0# 00 m. 15031 6.1:18 82.95 -17o.#67 46-. 44 -5#76 0.00 6#905 5r69i 4 m22#1% 104x98 53#:32 5 0.00 8.035 6.254 *a176#77 '-7#77 m27#048 106#01 64#31, 0#00 7#,111 8188#,39 6 -9#76 ..3ii578 9.341 $90t, 104997 69#37 *i89.94 # 7 11 i7S 106 ° #.370.691 1.05, 7 9 131 00 , 73 76,.74 '4190105 0 X13.7'6 114 f, # :647`71.
O•aCJ;#•43.909 12.936 S g1r'47. -195 0 34 64510 -v?.4.76 0000 .#4,6.:317 'i4.067 i16929 26wk,9 A165#1i, 0400 -30109 5.560 59433 10 0#25 38952 19#21 11 0400 2.767 5.630 59315 "162#12 2#26 271 , 12 C'82 0000 5 #067 -i59a19 12 4#26 7.7,15 5#772 18129 5«23; •,1:5'$07"4' 64.23 0.00' 61.126 1.2.#10 '12oy91 4t826 . 5.3 +,1,90.19 15•09 =2.# 14 16.664 6#62S 448;4 8+2* 0 . 00: .
7 0 1, 0'000 .' 5#2 3 i5 1 0 126 21 #4 8 4 583 179 40 _ 10 15#.78 16 0#00 8.688 17-74 5k1;68 -1.4449 .12x26 26 # 405 51499 -23#35 "139x62 17 •14#25 0000 30#752 10#267 11#21 8-73 -32•, 00 16#23 0#00 108 69443 ,134.46 ' 18 33. 12.0127 : :18:#_2,4 X32•:13, 19 0400 ` 34.:305 4-541 -142.43 i5:=244'x+4395 -71 >Ri.. 4 0:2.00 7 r 323 ;0 34082 5 4-90 20 20.25 38 r; 18 # 059 4 p3 5 i 1 18 39179 -157.50 22 ,26 000 42,215 : 20 t922 -93'•'09 4!.6.43 6tQU6 ~ 51•:23 "1584-44 22 •24.26 0900 46!290 24+201 -i17 #47 -58*28 0#00 -1609,44 23 '25425 49,520 26,155 m 129+27 71015 25&,76 •r 16 «06 24 00,25 , 0.00 m3,276 _ 5 -600 :37a 8 5 # 2442 vJ OF PO O R QUALUY A-154 VaUGHT (.mw §PFED WIND TUNNiFL TFqT_ hL3 4 WIND • AXES RUN IS 11/26/84 0931 kuN 5,9 Pei • $*c6660 T E MP , 70, PNT ALPHA L/Q P S T D/Q Y/U RM/Q ' YM/Q PM/Q .
3. a 366 939 2 • ► 143; , 04 : 2 76 . . 0 , 300 9.309, 05 47 6, Bt , 1 O 6 i 27 o v , 29 4 4 ' 5 3 w 5 79 i6 3 03o 74, 0.t0 0' 33891 * 306 9 * 737 R6 o 6 5.3{1. -1 4 6" k 92 0-00 o22.271 1 + 0.34 -1510,26 4 -5*77 10#404 100s68 48066 - R 5 -7,79 00,00 " 2842*9 5t6u7 1569,,44 ii0o48 6 -9078 56.17• m i 1 7 0 0 2 0 4 00 w$ 2,31 3 12 - 5 34 iUtArn 6 t W .
7 1 2: + i 7 9 .008, o 9 t 0 0 00 X38 14 :. . 1.
I a t 78 WOO 794 91.
• 244 1.54720' Os: 412641, '7'300 9 <:15 o 03 0 cOO 4~45 6 ji 29, 5 ils 9L + 226 479M 861 49 io 01 , 00 020942 Q427 94201 44w53 418 f J7 21*33 11 2 0400 15425 « 42 29809 9.3.7'2 ' 36425 4033 -140*94 06 , 00 m t t - 4 i o Ab 12 4 * 28 7 356 P-506 10•58 - 29 6,; 4o647 1* !
13 64"3 2. - . , 4 a 413 "14 Zw58 16.. -: 1 0 , 39 6 27:36 ^ 10922 0s;00, 21 t .047 ijo213 , 4 6 8 •8«56 w1 4 S0399 , 1 5 3 16 12$26 * 405 0900 26 129389 30058 5v4lb -14977 -143. , 79 17 -14#26 13-681 5 * 6*6 - 22421 m140*81 0*00 30-947 2401 18 L6 6 31v29 23 0000 33o708 15#421 24ri2 61609 - wi36 o 97 18 t2b Q900 3 4t, 5. 6 0 - 1. 8 4 3 9. 575 X1.9"w . O . 3 5, t -329 , 08 - i ,42a03 74934 r53 # .19 5 1 389 -3647 20 - 20 0 24 . 0 4 - 0 0 : 3 , 2 0+86 4• w14 , 7W59 :55 21. ,22 +2 + O*o 00 41• * 315 2: 3 o 515 wo7 5o,0_6 54576 X 42 22 . 24428 -53928 0*00 464365 - 96 * 38 6090 270105 22 24 * 25 si l."o5.2 --5 w 6u9 W16ad y'll, 0000 48o3*7 284854 -108458 2 1+ 0 * 24 0000 •,3+676 -91, QUALITY A-155 0 ' Y'OUGe LfIW SP ED W INO, u TUN^tEL T ES f 630 WIND AXES RUN bd _ n933 RUN60 J_i112yLS>1
TEMP 704 1446660
P5.
. „E .aawxmau+a.p..., a ...... car
VSF 75 0 157 561 t MACH 091353
VFPS 254 425 RTJFT T01 T02 103 JOY TOO T6 Tol, TOE Ti0 ....^z...,m, T=V_5 0 0 59 G 0 0 0 i1 3 i 0 TIt T14 T13 Ti4 T1S T16 T17 T18 Tx9 T20 0 0 0 u 0 Q p? ^2 eRRECT£D F89 , TARE AND NTEFFERENCE EFFECTS C DATA _SINGLE , SUPPORT QATA 'AT C O- FULL. SCALE DATA PSI L/Q PNT ALPHA D/Q Y/W RM/Q YM/Q PM/Q
0 4 04 .-
0 * 23 21836 1 P 3.244 9.466 436,17 44739 "139464 2' -t176 0400 • 91,543 S•513 60,•38 4t 28 270,80 -141•43 r 3' 06,00. w16#072 33' ► 28 w 9o904 a3#16 :51048 0141t 86 -507.7 4 0400 K22O238 40*38 ,146.,98 98!18 5:G65 ib441i i 5 -7.76 0.00 114348 54587 499 , 04 4,0 .,27.881 108433 *155 4 -9*73 0400 r32+i82 6e4Q3 554.81 i2+635 103,36 '•166x68 0.00 w173..25, 7 -11,76 (37.725. 69665 63*0.8 14 150 91432 8 •13.77 x'0.00 69x44 142.46.43' 15 x' 7.6. 3' 8132 6116U 8 + 4172992 5 '•14.76 4100 w454130 6417k , 73i27 16.947' 84-t 94 _- W172.96 i0 0425 6 34509 94466 44773 21478 -14000 43x37 it 2,24 29265 16*43 0400 94563 35424 41668 -(1374.04 .
0.00 10.09 • 12 4425 7 4l+? 4#61- 1364 5 1 94671
27 4 16
04.00° 5h63 642.4 11:4790 98959 23x29 X1;37.73 13 4x659 14 0.00 -1-85 8'a25'' 164445. 10..5.42, 25955 14 1.598 wR :.40'e06 15 10.24 0.00 f tsk52 •i4l&ka 21.016 ii4314 27#81 50,12 12o?7 4 0404 26.573 124522 5!268 -14457 28.51 .139 90 • 17 426 0400 - 21497 14 304967 134908 22.86 51575 A138469 16425 18 0000 33 3 64363 -29.'2. -w, 33473 857 15.763 21$ 5 5 _ 1..& 0:400 19 ► 25 ^ 30985 1,i 13703 344166' 18e765 28403 5#261 `37.6949 20 2:0626 Q400 .37 2i 4081 •51.17 5.G91 32 * 83 •i41 2'-0 26 Os00 21 -40«38 42t595 24m122 5--, 5#4 '6 -150x56 '27+403 22, 0400 -50.13.58 •24427 464331 6.755 x;159425 -R io3t62.
.
2.54 26 0r00 5$487 484901 234136 -116.32 74751, RI62.66 24 090 0 0 3,344 0423 94499 4 4639 21,0:42 42c 74 -4139965
6u 15 F
n - c.v^^ WIND 'AXES it,/2OZ94 q93 1 -4 RUN 6 RUN 61 P5 14,1.6660 TEMP 70o M Wr At nuA0QIr tt r OM IQ YlW M/© L'; n , Li o 0,2`4 •Q'.00 ;. ^^F^13 •x51.81 i -3,210 3='x . 66 5173 43953 Gt•t^Q . • +x,52+;93 2 -3:?, -5K876 60 ► 5f374 - 31R9 _ ^? {,5 ,15 ¢ r 3 ='-3+76 0 00 .,16.27 5.5:14 32«15 .-0 83.92 w..s^Q ' o. 0+00 4 -5+75 51665 449'99 s4159028 •,21#970 1Crt4 F3 97.55 0#00 6.051} 5ac2b 5 -7.77 ,•2718 5 1.1, -165#20 '24 107#93 ; , . 6 -9.76 0.00 -32 B+9 9 i3 61#,72 -178#14 , , • ^-^.,.^, a . ^s^. 1.0 0, • 'Z2 : 1.: 6965 7 7 6 Q •00 . 3^ +:6 "18'4e29 : ;^.^^. t0f1 7^i12 5 2 91 ;8 8 0+0}07 75094 3^7'8 ••42,741 87, ri80t.71 15 v 537 - 69770 • 9 . . •. •- 1 1 ^. 76 0.00 45.297 . 85;^8^ •^E43 7y 31r $3 8k s 1^ ^^ ^ 0025 0900 24421 - 10 -3+209 91467 5#206 150+97 43.34 •i 2.27 U t•00 2,667 9#53.1 51129 17!70 -1494•45 34 . 81 4.26 0+.00 12 7. 12«59 -146,pi 9,605 27 . 1 __-4. 580 13 6.09 0•o0 5•960 5tD5.5 1.1 992 23186 147,82..
8• b C3t00 a 5t365 -1.1x4>6 014.9.p6 14 56,779 1.^7 • :S^ q 6 25478 1 6 1a3 ► KiSQ'w7
i5 i0 25 09. 00 > 21w . 50 r a5 28•'57 55#666 x+7•'93
16 .12.27 26.640 129589 2811,7 59668 -14•, 30 -147,56
0 0+•00 "22 # 4 2
•1 1#.26 31, 240 13.975 23+33 51846 -144928 18.28 0#00 18 33027 15,63 20,6i 69545 -31ai1 1396•44 19 0 00 w 3Q 144.73'_` i8.24 : 34.532 18.571 59487 • 70 ;-#8963 - ,: 5s5 1 -35«84 z0f2y +ga ^G s+ 783 v^ =151 77' 3 9 -57 20 0 00 ,, .42.5 00 91, 21 .22+27 3 6 -80:: 28 5#59,4 •-41 •}1.9 i59.6 22 •24.26 0.00 469510 60,33 -51 12 X169.77 27+401 -104t p 5 Oo 23 25.26 OQ +26 -60•,56 •4169•.23 49 1 25.290 - 89211 116#12 24 0,25 0+00 -3,J43 24*15 9,467 42+92 5.140 0151.41 QUALITY oF POOR A-x5 '7 VOUGHT. Law SPEED WIND TUNNEL WINO -AXES RUN 48 612.0 /81 0933 RUN -62 TEMP 74, PQ . 11},.6660 QPSF 83 s 00VFPS 268#47 1637 U «23747 }ZNFT `' MACH 583 t TOL TOZ TO 104 105 110 106 .1`a-1 Y09 1'09 0 0 0 48 0 q 13 31 0 u T11 T12 T13 T14 T15 T16 T20 T17 T18 T19 32 0 '32 0 1 ti :CCRRECTED FCP TARE. I,I^tEi FE^2EN0E EFFECTS ANA SINGLE SUPPORT .DA'YA DATA -A k T C g f;. ^ ': FULL :SCALS` DA fd PNT ALPHA Y/W . RM/Q PSI L/Q 0/Q PM/Q YM/Q , ► i. Q 26 0 6,02 . w Z o Ol. 9.365 .48-0:60.: 25 06 ! 722 "t51, t 21 2 Q 2 , +2 01, 9,232 ► ^1ts 26«0"6 ► .^^^99'1 S4 ^9 1 = X140 0s: 3.
0.26 44 . 0.0 03.126 t9'7'6 24'29 50.81 -i w326.45 . 4 0 02 6 -6t01 2#726 43*36 w 6o7U0 24*41 0 91701 010 71 36 062.6 -80:03 =2#426 10#208 11t05G 21t•85 •8:3o.08 Qt26 "10#00 "1.472 1q#911 3 , 0 # 28 .+55x.04 X 1:2*OR. ^ 27 7 0126 IIt,74 s ► - 0x.114 1,2• p 46 1x. 46.
62 ^2 0 R 5 5u :. ► 0 * ` 5 ^s^ 9 1~1230 431638 , 9 `' s 6, o 26 0 1 40:0 *25# 434 $145 Y 36.:23.
2.575: "5'c'7 15 7s'i7 10 0#26 "18.00 3*488 *33e801 702 17*645 67150 i+10 - .9,24 11 0#26 "19#99 6#79 94451 4.389 20#080 o37#999 12 0#26'"22103 64369 23#008 w42*598 4*87 "22,96 121*.04 : t`26 13- 0 .-23..99 $ 187 ' 25. 879 !^35 r 8546 t 7:34 U K2 142 ► 16 1 ,4 O t 26 . 8b..00 28.927- " 16:3 ► 56 3.600: 37 x,48 ,.50.649 2:;42 .15 Q*2b ."28#00 i6.7:,1 9: 11.055 w53 t943 5101 :: 31s797 : • 3958 16 0#26 "30* 00 li,i4O 34#393 "56036 9174 r 27 * 85 170-84 0.26 0000 9#396 51846 2*t85 "2.922 w152 ► 62 47*94 18 0*26 21.01 02.981 9#494 4503 8#7.2* 23#18 "1 +5..98 0...._26 4*.01. "20927 2.6.3.7 5+830 01$7.58 41f15 ,111878 20 5t9 g f 0426 "2:222 46..284 34 .
10*341 30-75 56 -194#96 21 0.26 8`*.01 • 1.347 1 0 RB46 19 t 995f E 62 -209W,42 16.:88 22 0*26 104.02 * 249 42*;28 "0 119787 ke*27 24!030 r-227*15 23 1290,4 0*26 0.826 444.12 ► 124776 28#006 *244 05 ! 7481 24 14000 0*26 2+146 14,075 309927 450.50 w20416 •271 *50 16 * 02 .
25 Q926 159707 37#c51. 45 87 X 91.08 3.7791 ^33•"51 26 0.26 $*00' ► 63$ wi^8.98 47'«74 -312*3 6.
4.793: 17 "41.475 20.02 27 0.26 6.014 20.059 50r7 0 »47.48 '477%i -352*30 28 0.26 22001 7.537 22#759 R 58*18 520% 54x73 -3899.43 0426 .
29 24400 25.596 57t261 54*13 961,42 "67•,16 -413.94 30 0.26 26400 9.301 23427 29+698 -44*•94 58PS34 +355.81 31 Q26:,28 *00 94993 ;624547 18x51 33.157 "39#80 -377*80 3.2 0426 30102.'•b1.6` 361354 65x316 708 X 2.5.:3& "3811.88 33 " 2 0426 , 0000 #862' 26x99 9,335 48,08 #.*243 , 15#••76 YaUGHT L,MW SRP-ED WINO l ` CtMKIFL ,630 7VSj W XtvO .AXES PNT ALPHA 'D/Q Y/W RM/0 * YM/Q P S I L/Q PM/Q (^..2 C^rA1 -^- 1 g•4 9s7 24r9b: X147',.85 t1 Ss404 2 ^2. 0.2 , Aj 4 •134 90 0 . 2 ' 2 r 8.41 5, 383 5.2 2,9, 1=rt 648 3,!5 . ' j• 8/0.2 7- .+ 85.64- :-mw 2e^a3^'^ 3 .0 t25 4 .02 f826 9.395 "i soioff 4 • *5+'9.9 22(434 0.26 +2.725 9*641 w lo1094.82 45 6«272 ,77 5 -7x97 w2,332 10,226 1".4'47 82..33 38081 *9114094 6 ft 10,.01 A'n5v54 0026 *1.262 11_•1:22 *•15•&12 •520,96 ? '• ^1 - 0.2. w a g;• p 3 1 s7 a o. 1ST 317 37:971 .9;: 2: q 5tS '.-24ts 12 ► : ;i99: 8 C14'G6."*13 1.:ZD . 'r v1" 4 755 7:•15 81-9: X2.31' !4Pi^232; x.
,ws1 9 ,25 '`..99 2.637 791 r^ xl•^31t :7444''- 1547 8 9.7.69 10 0*28 "18.00 m34.186 '^ 4•.91 3,470 17.934 70.14 2.77 0#32 .""20 #-04 69.23 11 4 o147 20 4430 -5.20 97.96 "38 • 492 12 0.24 . "22,.03 6.037 -!42 *797 797 2a6$ 124.98 23.248 -20,68 i. ^3.•35.^2^F +0c 74874QrC'35. X47+447'; 0447 •147«34..
+ x '3195:& 29 s x;43 1X35.
14 0 . 24- ' 25; 98 . 9 4:334 8(s o w, 5 4 •16 6 685 -+36 1t , 15 0.2 + :.•28402 10,845 054.430 2442` '119 0 5 32.040 w3.8.27 .16 0#26 : -29.99 114414 *57 ± 151, 8.83 177o:83 34o897 + 28.28 .' 17 -0 6 01 5,787 244.11 X2 . 26 • 2.941 9.577 49x15 - 149.60 18 0.26 2.01 2.891 9,675 8.846 22t5l ,144.60 46 * 75 4s02 19 'Q^2fa 9490 :12:t0b8 25+76 155r.92 w 2.535 3947 20 0.2 6 5499 35^ g 7: • 2.1;Oi 1.:152: '1514.38 10299 31.00 , 39«3a
2i a Z6 8.02 wlem196. 20:+076
11*I14 7«G1 •*209457 _1^ .22 . 23a702 41*1.6 -218.,36 0026. 1Qa a0 0.082 11 . 788 2998 23 Q*26. 43.,62 *2.40•.48 12000 1•278 12•855 -9.91 27x795 -- 24 0,26 14.00 '32434'9 44.97 2.64.88 2.778 14.256 •*21*52 . 0 26 r:82w 46 4.52 25 16 * Ql 13 '37 R 180 • +288 4 r 2 <:15 -'34 «99 71 26 „ Qr27 17*99x.3 24 .411568: 4845 7' :' 17.519 *442«44 - 3Q9 27 '58 51'4.63; ..348.26 01n^'27` 19 0, 99 6. 20099 l48 •.+48 47.092 0 22 * 00 28 #27 54 * 90 +386 .:19 7-719 22.713 -57.34 529281 23.99 559,88 29 0*27 9.264 56.591 25.447 0 68.78 "407.43 30 0.27 24*28 26,01 5.,, 426 29.666 43.28 57.996 N354@80 31.
0C•27 2.a -:02 19 t'50: : 10x157 .33+074 -39.14 :fs2!262 377•71 ..-4 34 30..02.: 7«83 32 0# 27 k24.11 1-66 i ,42-9 *1378.81; :;:36.236 33 0.00 0924 254197 0148943: Q 0 ^..2 1._. 0__ C q 2Kf ECTS ^iiRvooT,t FfiR 'TARE .AND.. FE RENCE.
XNT.Ej SINGLE SUPPf1a.T AJA . l t,ci ,. :FULL_,SCALE:.'0A7A t1AtA PSI PNT ALPHA L/Q PM/Q . RM/Q D/Q Y/w YM/Q Q.25: QR1.: • 2.3.`17 5 ► 901'.' 24«64 A152:85 9 . 49 51.2: 2 Q02a ^2tU4 • 2^5 6.2 3;•3;88 9 . 52w92 1047' =343^1.Q' 25 : 1 3 _ 0.25 9.:227 5'2.4'7 -1#896- 2:4 • 4 0.25 - 50•99 23+•98 0. 30005 9.491 -X110+69 46.09 W 6R23U 5 Q02 5 --7•.98 2.627 204,69 .9 39 39.95 w10vaU6 x84•!55 6 0125 -9.9 9 0r 1.685_ 10• $37 ;^0.6P 4.5 - 3 0 ^, 15.84 • ,6.7.79 , 4!25 ^+ Z..i$. 11•$7 7 - s L7.3si. 1.1.51 5 15060. 748' :-2Sr17 $ q :25 --159 ..R52 30Q:7 7 ► 9'h93r07 1.3A437 rt24l ^C2`.
' Q ^ 8'..0^ :, ^ 9 26 "S5 s59 286 36...47 2.. >15 •: 232 `' 9 r 9'^ 0122 0.531 10 0.24 `17«99 30409 ► 3r6 76,08 17 4090 4 68.91 33!1 + 0023 . w 209. 03 11 3.960 437#707 5x97 19*851 r4r72 10t7•C)8 12 0.23 . 0 21 . 5.815 3017 22.775 T oi .0g K4 20 179 '12 2.78 13 S7•?3' X 23+99" 7.408 35.51 04br623;.Ci .^59 ^32R1 148?55 9.p26 057 05Qi912 4,06 .5 ,167«44, 36.38 45 0.23` .-^ ?8 01 . ^6 .' 5.; . 053 ;32 t i35 X54 755: •1`74+06____- •41 9^ 0.23 -30 0 01 7 *74 1,78. 't, 11 0 003 35.044 -28.17 *5 8 00 9 3 17 0001 0*23 w 9+563 64268 23+17 A154030 30451 51052 18 0023 2013 •+30448 21090 9.628 48.97 9.217 am 11+ at:s 19 010 23 00 ,1;2.1690-, 2,4 *73;.'x.163 +65 0 3.1,:46 9x51;4 4Q•^^ , 10 3+}:03 20 a•23 6,•tk3 1646 2.412 10 3.8& . 30e80 ^19jt-54,; Q•23 38.17 :-217.29 21 S i OL o l#6 5 11.043 L1703 10' q Z4$ .a 22 0#23 10+90 0.357 40067 1.10796 2 -241111 -!222#46 +17 23 0023 11+98 42x34 170956 120836 m 10•43 x'$!197 -241+44 24 0.23 13098 44.15 2.345 14013 -23.43 32,606 m265051 6 0$23 3.757 t.5w99 15.796 -•35095 00 W291092 1 6 0t 37 .
7{.0963 181,01 26 0.22.3 :4.2tl a4'` 4$w`3$ 176.37 .44- , 33 -X31.2.62 27 002 2 , 01 .
3 6.094 201093 +49f 21 47,0EQ-6 51•;12;. w=350 28 0.23 530,80 21 70306 22.782 -58.57 530039 a x3870,74 29 24000 0023 9.451 250583 57062o 55•:02 -68.87 406•.48 30 0.23. 26*01 10.651 28.493 .620545 579, 14 +-43415 -76.7$ d .
31 Q 23,: ' 27 e99` 33 0162, }-374.33 10 • CT6'' c -38 •.06, V kS4 630024, 32 9x9'3: 0023' ' 2.9 .099 03766,2.5 9.215 : 36.122 -,21,•3'7 65t50U - 0 20751 33 062 6 0000 : 9.450 51.02 5.790 24..38 0i52'•59' IJ6' r sp ED 1IINO TuKtd r 7 3T 63Q WINO AXE :$ R UN 1 1. / 2 6 RUN 65 T g MP 62# PC, 14; 6;955 QPSF ' 75s t 00 MACH 09^2?_Si VFPS 252*0 7 RNFT 16O3651t . r I io2 - ro n4L *rob raA inj Tog^ Ypq Tio 0 11 0 0 0 0 59 31 0 Tit TiZ T13 T14 Ti5 T16 Til Ti g %9 TZO 32 0 0 1 0 0
0 0 _ . 3?
EFFECTS Ce FOR TART AND INTERFERENCE.
ARECTE D ..SINGLE SUPPORT DA-rA BATA 'Ar CaG.
• PNT ALPHA F n I L/Q RM/Q ' YM/Q D/Q Pm/Q 'Y/W UO26 9 0600 -363 0 9 x634 2+*,2l m14708 4449 5oge7 2 - 1*75 .!22 •11,.4.8 .
-9x 42. 5 s i28 x98 0900 7 9 6 747 61. , 9,68 o 3174 04,00 - 3 m i6 v i7l, U , 038 84c64 .#322 37,47 - 53 «93 * . 93 x.
0400 * ZZ#438 4 "5#77 1009 - 50418 45 +.52 "166s$9 10 x 638 12 5 w 7#77 53c, 04 *J62o , 52 0 00 627#645 11048 108628 5467* 6 _ "_ O o77 0#00 n _! 6 21' 6U- *1 Ca , 4 22 . 74 27-21 1 7 la2 # 1 2 2 # 5.
7u # . a i i , 77 6 -1., 79.:48.
Q Ou w37020 . :1.4 #357 94#01 6.573 S 3 6 76 m i 0*00 ro42oJ76 156870 83#6i, 6 36 8 74*i8 - 178+79 , Ow 0 89 4 91 6tZ65. 7S ' #67 •R1839 , i6 9 op i * , * 71 442#665 159928 0425 49560 000 w 3o376 9a666 24 w, 24 wi479E9 43.38 S663i 3509? _ 417 , 15 11 2#27 2 + 334 17 108 -1+5"30 12 I f - 1 27 O o OO 9@772 27 6 7A 11#9 7 ml 4 , 4 # 47 ^i A^Ll 1,3 ^ 6..08 " 147041 8 10 * 0 , 61 . 6 612 06 - 00 i1^727 4178 0. 49 wiw ' 39 , 1 , .x 4 14 8926 0*00 16#213 24 . 1 0.62`9 5 125 7 o,05 is 0.0o, -08x30' _10#26 ' 20x9$4 i i 6 449 2 7: 0*A 50566 - a i5l *7 9 16 1,3o2* 264370 13,553 29083 50+34 -14* , 48 "146639 17 -l i t 4 26 6*106 -23081 -R 1 , 45 ^ 6 1 000 0 31±213 . 144148 22j,62 18 16,26 19686, 6#65D3 2 v, 7 6 - w 0000 33,631 1 Ei s 8!j 0-23 1.3 18 12,6 6.*67b m IOf%01 o: 00 35s04i 1895$4 a 26, , 32 32'+ . 73 -35'03 20 20628 QeOO 38.+ 325 21*E17 =57'e6 2` 59 2E9 A149 a45 21 2202^ 09 :00 5x 5. 93 42- 220 2 - 4-162 - $ 2 .24 42't 5 4 o l " o II 22 -24,26 0#00 46•163 27o568 w1,06 * 0, 4 6eS0605 4 • * 6 *166w79 23 25#26 -61,6875 26 0000 4, 9 * 254 7fS37 w468*61 29,@357 - 1 1 8i62 24 0025 00-00 W 34403 5 24.26 148-69 9,633 .4 1 .,46 4 ,4926 " IS onle "Im'm ALITY.
, U.
p 0 0 R A-101 v 155 u G WIND AXES R U N - — , I- PO 1446$b5 Tm p 6*# o p SF 75woo VFPS 252 MACH 0*2251 RNFT 1595961.
► 55 T 0 2 o 59 0 11 T12 Tl$ T14 Tl$ Tl$ Til TIS Tl^ T20 CO RRECTED FOR. TARE G - NO INTWMNCe EEF';CTS SUPPORT DATA..
FNT ALPHA PSX Y/w RM/Q ' YM/^ L/Q D/Q PM/Q I Q120 0-00 w3o343 46i4a ;^4762,Q, 9v666 - 1 9 75 0 o 0 oio*Qo g 9 , o 6 Z V el 774' 5 l734 2 86k 2 5 *14Q•li d00 Ag." 7 9 ' 0 3, *3t76.
% *— A - ..$.
4091 - S , o5 *7#76 0 000 *27#814 $0:is 48 48 -Ri50o 11*481 1Q$t49 w9 7.S I oo b i- j _^ h _ J U 4 w1a 4, 0#00 3 2 3 4 17, iP 7 -1l,76 0000 •+ 37.8 72. . 387 7' 44 0^8 &*-1 6 - 1 6 7 6 8 - 9 1 4. 93 4 6 1, 8 H13*75 S 9f,UG p R i.69ir6 ,9 0, 00 048#04 16 #037 8 , 5 , #,6 t-94 7 4 14 446 , 216, 35 *13$•65 8.6 4 41 69 11 0#,0 2! 4 0 6^ 5 4 42 6 8 160+2 *13604 . 9 &,676 36t4i 12 0o00 13 6#2 A-08 73 #.758' 3*71 IS OqOO I I 10 q 1.59 24113 4- 0 4 , 72
i4 o.bo
8,27 16 *2 t , 75 p ,59 *og
104, , 677 25 9 . 9 6 4 84b V5 10t2S 0900 20.9 i 3 •.
16 12#26 00, 00 264806 ±6:55 543.
142 28 52 48 0 0000 $1 * 098 17 1 I t # 24 1441 22o79 Ei 3,, 9 d,^ 2 CS 1642 0400 33. 83 E5 5 1 2 1 - -q,9 140 5-,67 0, , , 1-9 1842* 0q,00 35.07.3' *321t24 "08-46 7 3 5 x 47* 18 ,0794, - 2 20 20•23 0400 37.986 21 . 223; *1 5 8 * 09 •38 5r2U1, 21, 22 0 a l s , 0.00 . gAi " 800 2 -4 1 - 1 *05 42 624 2*o2* 22 00,OQ J + 5 68 2702 , 64i9 -5 u— * 6- 3 "158#48 44 - 4 104118 -6 - 0000 •0 3 24 '.. QOS6 1409 9#667 16,35 "1399 i7 46452 ^ . 4 5
po 1*06955
TEMP 65 0 RM/Q ' YM/Q Y/W PN7 ALPHA D/Q PM/Q P S I L/Q 0 00 1 741 -14 - 10 , 5 1 9 w s07 -147-71 152 - - 2 A — 'p, 3S
Oo,752 8 652 ^ 67 ! R l
.
q o^ 6,o661 IS 44 1 PA 4'F i 0 , 001 3 . .. vi a i Is 7t4,46 43•-73 *168* , 10 4 -5975 • 2147 53 9.693 1.22425 840501 0001 •244675 100429 136080 52*00 w1764^33 5 -7 , 77 ft18^•31 806,24 59•'82 OaUl x25.566 114676 i - ? P &37 6 p 9o78 8 - 4 1,86s , 61 .x'11 .7:72.'
7 . *870987 1220 56 77 QOI j 8.0 Q. 73# , 78 018 0#3G
.29
4311.
1 .
198 x: 1^7 97; .7 1 *30,4 4 17 x5U6 s 14 0•01 2O0,36 506( 1 1 10 6 *140o87 0,24 801.84 42095 0*01 -9077 130• "136c84 5*460 il 0401 -64947 7x529 18*99 8.x35 noi34 o 58 P
4,29
01 , 01 m 2,39 3 v 2 1 2 :4+3 11.1 01:01 0.926 7v6$15 '4 c3 3 0: 6, 6 :, 14. 0 5e26'1,' -3
892 6 0001 4.618 7•7-95 'Of ► 71
e, 14 q 44042 5.5 59646 -14*.72 *1474;62 16 12.466 12025 8o574 -99'078 50818 0 20k*1 0001 1S•593 w149o51 17 •14#26 94604 0 113000 5*866 -269-72 -i53a0 18 1.6 26 0401 17o698 10,701 •. 1 15. 48 + - 3 1*7 3 X 155.6 .4 1.
is 1' 8 . 27 1947$43 5 '49 s3.1 «65 -34 0 , 20', .4 OR 2 81 •:01 2 1#368 3-0 245 1 V5 * ' 7 4' '168 : : ' .
4. 5 7 9 -38 50 -ti35; so, 0•01 53 55 ii. 9 2+ 1 '22 •a4 2 Oool 24,133 154548 34982 -41429 X115*71 22 -24927 w108 * 9i 34545 "43*-59 A108••65 23 25427 0901 250342 17o020 w 112o2i U«36 w 14 Qs73 rJ. 6U1 2 24 OtOl m9g708 8025.1 43 t. 14 s D
U eu GHT Lmw sa 5SQ' WIN Tt1 ► yn F^ r^c^ ^63L
WXN0 :AXES PNT ALPHA P S I L/Q Y/w RM/Q ' YM/Q p/Q PM/Q .
,.
44.,4"4. -30 i q•24 Q •,02 5 w 9t842. 8+055 «4r5C1 „ 140 74 X147«75..
2 -i.76 0«.02 ift13i525 67«9'0 52:5,4 27 88 80461 ,; . 3.78 36«43 3 04022 mi8 136 9.908 6.49x: :156.93 iL21 ( 0 tOS 4 -5.75 123..34 45 « p 9 m1 66.,66 w2i4728 9.493 7r1.92 5 52049 '-T,76 00104 A24 t 1,73 106338 7 o 8U9 132.36 v1177.86 - 9.75 0.022 r25+335 it 9518 11EJL '5 ', 8.206 60•'22 wiR2699 8,338 66+94 7 -11 . 7'7 0102 =27,016 . AZ-71.3 -1a4.4$ iP0 86 8 11.24 { •fl2. 20194 -0141«44 x :$42 8"175 5 420 44e18 Z•.'S Qs 02 " R 5•g48 : 7 . 1 ` -Rn 5.16E 13.47 mi37.71 8"73 i0 x).:02 8«23 oi33 ,63 4.425 -2.486 7+642 5*00b 0 442 ii 6424 0+.02 1050 3910 7.567 4,855 "136.05 m2isZ8 12 0.02' "P «15 8.22 4s441 7@702 w 42 9 0q 5.137 •.,140.6 66 .
13 0.02. -9'^U5 3.Q•26 St570 7..923 54259 72 1.7 -% 14 •70 14, 5"654 laf.432 8«473 w97.06 1Sr7a - ^- 147.95 0--Z6 15 5'..02 w9*64 8.081 43.11 2:9 -141.73 5.32^i 20 l^ t y^QQy^c Rr t i 4y6ali\ 4Nnt:'a p 1 F[ kM^ A^ ^, pC^0, p^ A-164 TUN B QHT ^,P14t SPFED WIty N E L TES 63.x_._.
_ -_ V LI WIND .AXES nsn3 RUN 69' "N " 54 11jp L/_8. i PC I* V69695 TAMP 75• PSI 'Y/Q RM/Q ` YM/9 PNT ALPHA L/Q p/4 FM/Q 21.38 Q•00 r k9286, -X135.40 i 00w4 -3.310 5.633 46+66 0'.00 5.746: ^#e5ti 0137.09
2 ^i.•77 w 9.376 6384
= i•3,7 R5r71 T•549 33os72 - t i 0-62 3 0wOO 'WiBgA72 10004 e, 4Oo86 +143.81 w 5•76 0.00 40546 4 •21 10.572 99.66 47oiL 5 w 0.00 813 41450.38 7#76 •27.481 119381 107•:80 4 0 w 55s.36 14_ 6 9674 0.0Q .31.•R79 12!? v%160*49 loi,_o Q 7 .55 322 t1.Ua •162.43 9 ^at;?86 61o.'0 a 7 •^1i•7.1 •1404 ' 24 $6o .37•x;.40 419 . 90 67s79< -o163t56 S Not 3. 00 74 Q'• . w41•761 150897 850 .
16~39 at17iwS7.
OwOO 18.bs Rocin 4+0501 9 xI t7.8 .46•2 97 ' 22,45 9•0 0.00 46,30 -ti37 0 110 0023 *34244 9+599 027S «73 15 -1359,25 . 0000 9.664 38002 401b5 11 2.27 2.867 100,98 134 ••76 0.00 9.772 31.27 12 4.26 7 ..421 4' 127 , 5•'7S 0.00 :' 4~259 `i36e76 i3 _. 6x26 12:,225 26.,.65 100027 i«2.4 - ~ • w 1.6 0.00 40164 137 14 27 16,547 1. p +564 2783 s • H 7«96 ai41.17 11:,3#9 ^10•.'75 590yS , 5 10i26 0.00 21 $4 _ w13e,16 '16 OoOO 40845 ""139137 12 927 261606 12*422 31076 -23x64 5#7'S9 14024 0.00 23.393 *!134916 17 140440 10x88 0600 11.57 6.42: -30.26 -131 •• 18 16.25 32•67G 16.129 ^13g•,4g 3 5(355. •36.03' Q OO 35.. 214 i9 1$•C6 18-707 X 23.5 -34.!06 -142e91_.
20 2Qi26 0+00 '380596:. #56«34 5±471 21#'1.48 -X43..43 0..00 -91.53 5.878: -148w55 21 22 p 28 41. 6 24.185 -51t81 -^158*'29 22. •24.27 0.00 45.718 27+383 • 60bb 9.44x69 *58.,03 0+00 795sb X163.07 23 24,25 49.06o 29.555 •1.16..64 22.,48 0025_ ___0,00 +3.143 90667 46..8+ 4i2?Q X136.7:8 24 _ 1543036* MADH • U c,e251 VFPS 25509 QPSF " 75 * QQ R'NFT
Tto
TQ1 T'06 709 TU9
TQ2 TQ3 T04 TQ5 toi t 0 0 59 0 U 0 0 11 31 0 Ti6 %7 TIS T19 T20 T11 T12 T13 T14 T15 0 0 32 0-- 32_ EFFECTS C O R ENCE RREC,TO FCR .TARS AND xN`TERFE SCALE DATA.
STftiGLE SUPPORT i^AT^k BATA "Ar G.G. _.xE^iLL- YM/Q PSI L/9 D/Q PM/0 Y/W R'l1/Q ' PNT ALPHA.
: 2U *66 .QtJ 4r. 2.06 90131...72 1 3,.276 9x.233 49+t7Q .1.74 } . , : 26o 43' -i,3340Z 0400 '. • 65k46 4021 2 9e tc78 9.374 ,.3.77 8 3 ='33.38 oi36.29; _ 9.7• 7 98: a66 ki446 —0 00 '..16!4439 ^ 40*27 -5 * 74 OQ 40531 w141*07 4 0* .+21.903 10*339 101*, 24 41686 46*,86 m 5*.04 5 -7*75 0600 m279647 109#69 14 11*148 55032 6 w9 . 77 0 000 -31* 5031 2 8.4.9 _
692 12 14 V
5.5 • 54 wi
7 .11.77 62 * 30 '
00 ,37. 406 5 2'33 lvS9 • '13 14 ^ 44 ,92 47- Q- ^j.Gi 5.020 6:720 -^163^74 8 -13677: `±41+910 "1.`x^a9C1 8 6 *40 4#846 7'1.1.6 w164 5 9 .14.'17 d'. J0 ;-44 P98 16#594 84 .33 20x71 -1.32.17 10 0*00 3.376 9.266 48.23 4@106 Q*25 14*76 0*00 9*396 4#021 *61 11 2424 2*599 w130 40037 + IQ-, 0 •130057 4.25 0.00 9*471 3 3 # - A 13 12 7.087 _ , , 4e20 X13:1+77 13 0*00 090 9 * 759 '^^.=l9 41079 4•24 0.00 -2 i37 , -.133.;:2 4#598: i4 A*37 . 16714 10 •2'&4 3.0r.1 g t^..OQ'` g.Q9 mt i3 l•99' 5 10. 26 329:53 • 4 99 1 21i017 114-4$ - 13*,26 -gi36.,32 0*00 49735 16 -12*27 26.573 32078 12*156 -24.,45 0.00 S!846 X129* 11 17 14 * 26 290660 14* 074 14x23 6.276 X31*67 91_ 18 16*24 0*00 156868 14.45 -.1 28.
32.869 -3':2•>19" 0.00 35.262 ,`18.0508 5329 -10 19 =23,32 18 . 27 20" 6. Qs0{? w. 38, * 68 -0#8.28 -52..68 .24x • 5.08,44 - 43a36 •145*85.
22*c"'7 Q*,00 41.696 23+684 `.77070 m 158 c15 5U F34 45.948 615 , 29 - 22 24 f , 24 0 & 00 27 , 031 w99 *44 -159.89 23 2E•23 0*00 48 * 692 284884 -112:35 7+378 "55 . 87 0.00 4.106 20*71 w132.97 24 0.25 +3.376 9.266 49+06 PNT ALPHA PSI aM ' YM/Q L/0 D/Q PM/Q 'Y/W /0 2nr4.4. ^rt1.35+'96 dt24 Q-0d1 :,• `.2u3' i F b•266 4 6u6 51::.8.6 :s 2$w49i 2 `,-1,7? .. D,QC1' '_ i0.646 68•,42... -1.35w95 -9+3.43 4f6.61 3 '.s-3.76 0.00 rriX}t7C74:.;.i1r 32x44 n134 . .06 ' b c39 9.i+:25 4*.;ju 1.
. 4 "5,74 0,00 37«54 -q135a02 .,19.903 12,306 i05,81 4.265 0,•00 5 -7,78 m24,562 139482 4t134 *3 0-94 -134,31 11341 6 -9,77 0000 -27.785 50,•44 0140921 15.310 97,E 4+972 0#00 1 5 2, 7 95' # 3.953 54e81° X11«77 .31:1840 1.6+933 -146+97 8 .13,7$ 63•!DO 000 ,.36:071 18 660 411,34. 04153R:b2' :2e:27 : 4..34 9 ad4OT 0.O0 38s32 66191, R18+.05 19651 91r55_ :• 10 0+24 0.OG -3.176 1Q,333 50,46 40573 20182 -4135+•76 11 2030 0000 2.669 40629 10,166 134•96 *136,.28 41,99 89,56 12 4626 0,00 , 4,688 -137.03 7.688 ib n 305 54 3.3 13` 6^•2b 0+0J 335 •^138t80 1t7t594 .
1k3',i55 289. 24 4,?'S9 1r4 ^•^^ Q^c70 a79 ,1.1364 a^, 70. ;• 4 . 931 ^^`^^^ - 138*53
i7
, a -9r17 -143*,44 i5 10;2i4 0 00 22':•982 015 5 266 :" .'3.2+'$7 16 :12+24 0000 4*888 ► 77- 280003 13,054 35913 •-12 -140.90 • 17 •14,23 0100 51678 -22x42 ► *1,.32,,96 30.610 14,811, 16,87 18 16.25 0,00 33,570 16,663 15.58 61463 -31867 wi30.22 ...
0.•.00 18#26 36.501 15 34. 1 I* o. 5t6u5 X3401 , *13807 20 20+26 0•00 -49027 -3546 -1.43-43'4.
39,265 : 2i ±575 5,091 00.00 el '22124 42:•233 2*#466: '-78«x••81 3 -4203 -1.469,•3$ 22 -24,27 w 1,02.83 0000 45,751 27,669 645222- -48+17 wi96+82 23 25,27 0100 -54••, 611 48,922 29«825 +*. 117.34 7e086 -163,15 24 0,25 0,.00 -3,576 4,57: 10,333 5i•3q 2102 0135027 -fu A-167 NfluGHt Lmw TUNt EL TEST -00 spEEP - WIND - WIND 'AXES V.,Q DmIlm vmjn . iN,.r - I", - I f D/Q P Q PNT ALPHA P SI L/Q 2.0 #67 11#613, -*13 4t02 0, wR5 O•OQ e 2 7, 0 5 w136' 91 31 + - : 4 9641 A, 0 - 7 8 1 . . .68 "1*7* `0*00 5 05 qO, 40 40468 32. 0 1, = 135
.• 0 00 . 04 •372
: 3 : 3. 73 1 4x 5 21; 38t3* "03 # . 46 4 -5v79 OsOO w19 #872 12o438 105@39 4 1 Q S I 43,61 "131,20 3#8*0 5 -7*77 0*00 w24v582 13 * 576 113#38 48•:12 3.,642 •135o68 6 -9*72 0 •, 00 -, 27 . , P - 55 15,351 26. , *80 7 -ili&77 So 47tQ93 0+ 00 , 31 -a 46: 92o , 76, 56018 - , 140073 3t4 62*21, -i4ao , 58' 0000 : s-3 6 q 4 -4S 8 iS 76 480746 92w61 , . . 66 r-52 3. 7 23 156.42, 9 W14, 06 0+ 00 J03 8 0 w a -7 : 1 , 9^6^i 8.9 to a(— -13 4#-34 4 t593 10 Goes 0 , 00 -3,076 10020 50w40 20 0,? - 8 13 * 68 "135*11 0600 2.433 106297 It 2125 40*70 40508 o, 136#27 4 1 0 : 3 05 32,57 4*473 8o,76 12 !f• 25 0000 7 6_Z5 3 v 7'* -1,36 *,59 447`10 6 . 2.4 12 .824 io 0, 559 26 o; 63 a'' 24.
1 8•,279 0.00 1230 230 e$ *.,.1 9 Sol 141•07 100:25 0000 .230 50 1 20 ' 1 16 1 0, 57 ^ 15, 4la21 -12 * , 68 m140@57 16. * 2* 0#00 12 27@903 . 13*154 34 x.1.3 14 * 02 5t826 -2308 -i, 2 9o91 17 -1027 0*00 30o694 15oO49 -30c95 86 6.596 158 9 0 18 i 6. 0 '#, 0 0 3 . 30682 16 . 529 24 1 2 -0 - . 19.
; C -9 0. 0 36*56 W137' 63 , 91 00 '1. '61 19. 10,26 0 37#101 4Z . ".35 *33 0 142.
9 j7 , 13 . 2'7 . 00 . ,.Jq 5«1 1 .8 20 220 21 o 7 16 47058, 2O P '0 6 -41098 - a 1.50*67 Zi. :22*27 i OcOO ., ^ 43w , 523 6 24 7+5 0 Q - 24 0 ) -49t.21 "160950 64175 22 -20,27 0#00 46#251 27,770 -102o,40 -56c13 • q162 901 0.:00 29o452 118 *-49 6066 23 25#24 *8,326 *134wi9 10,,399 ? F•4 ;39 20*, 39 24 0424 0,00 -3 * 076 50 Plln H 1 1.
o^jGlNA ^^16 8 or. pGOR QUALITY P5 1446$62 TEMP 85.
1576390.
6FSF" ;'Sa 5 0C VFPS 857491, RN5T MACH 00:2254 Toi T'02 7{73 1'04.1'oa TOh Tp T08 TUB 'T°10 '-" 0 0 32 0 11 3 0 U 1 o T11 T12 T13 T14 Ti5 T1 %7 T18 Ti!9 T2U ' E^FECT3 CS u CTB F5 ,R TARE, ArM Yh^':^RF'ER9-M OATk'AT c.G.. .,^ 'ULL SCALE SINGLE SiJPPdRT':UAr,A RMfO vnc/Q Y/w PSl ID/Q? ?tl/r7 PNT ALPHA L/O _, 2`;3+.51 5x14(3' '.?ec^.7{^r9 '6 ► 63.3 X156•-15 1 uac.''3`. 0 *U0 fi^3n09' 31'+64 . 98t!
7,048 44 2 -1 i74 040 $..642 6.1« . 86` i.a5«53 e 36.93 ^^53R91 ^8«87 ••3.75' 04Qt1 4*8rb' _ 3 .i4.438^'7 «745 -, w^ 4«46b 42.•24 4 84886 -R151ft)9 -5*76 0*00 110.18 ml516ll 48.31 4«386 109*20 wi48t62 5 : 7«7a 0*00 w23«334 10*550 U X1 7 ► - 4• 3 :^^i" • 6 -9*76 0«00 w27.0§5 12,« 7 9`^•Q1 bin46 ^1b3«^39 , OPOQ 1'3« 547 7 oll 74 x.33 •9 4 107#75 .^ 4r^^^...
t$..^ 0r7b O h^C,^bb ,.04ta13 -ki&S 74 Qt .•37 «209 « 873 liao,+76 z8r9Q-- 9' »2* * 77` ^.7 .Y!9 029.51c ? 4 4 r '^8 34 6«857 0^ 0 11 6• 1Q 24+,18 -155 59 0625 "x00 •2.776 5+073 6.6QO 49*70 i1 2«26 0 -154+81 00 34133 6+464 29,77 4w°95 16 . 94 12 9« 15 52 «61 4.25 0 • 4;•84 :_ .? 0 8.521 6+605 21o15
i3
2«56 '+ 149 q^s2 6.26 Q^'(i`A 6 ` 4!'813 13.459 i 27 15134: .
$.:2a ^3r82 81.45 ,i,5 0000 ,, 64 5 4 9 84fr 1 . 8 « 7.497' 17 11,.
► ''nQQ ; -5.55 I=45.02 15 Ira 0866 ;23:•5$'3 21,.29 8 . 416 16 W139458 OsOQ 19.71 W 15M54 12 . 24 27.770 9.554 4t:U1 X135495 17 14o126 5.006 x21+92 0400. 32.040 1i+1.82 11 «26 IS 16#26 X 31 +65 5.454 0x00 ^ 3^8- - ,0 6, _ I9 1:6426 •:$U g 77: wi38a71 ` . 32 455 " +gp8t:&3 (•2.3b .
37 « 16 13 + -33#38 -142#38 20 G&0(r 40sI38 042 184671 X62#65 3x826 4, 21 - 00 ± w 4 Uwa5 ^1^ 22«24 0 43.653 ±&•.^_ 21_*48.6 "9ir93 W^ 22 -24x25 0,00 X 6«84 8151«9Q 47.042 25.060 541b3 w 120«83 25424 -151#66 23 0.40 49.053 « 5U#21 26.679 -132#39 5*745 et5.5 56 24 a ► 23 +• 57 0*25 0u0G x+2.776 6«673 3_• C0 6 J+ OnM,7 1 ! 1 101 11 - 1p^TA- C,o A-169 Off,. FC,5P ,, qmlffl y I ..
1 ; ND TUi'VNEL TE^ST 63( VaUW - T L.VA SPE5D WV Vk F LTA DATA 0 0 - 15 1 r 0 0 RUN 75- " RUN io) 11/2 0 /81 1438 V E SUPPeRT TARES -Ri:,.M-d TW ---- FT^ --V t q l.M,C) - AXES' 0 SCALE PATA YM/Q PSI L/Ct O/Q P11 / (V $F/Q RM/ 9 -PNT Ai FHA 69 - 05 -7,51 I w la#Oo -0o, 76 -3* I I82 13 , 914 124 ,1 73 0 , *10 U, 15 m 28 o 773 12,209 12285 0#753 2 w 10*00 -0 o 7e a -8-00 w- 0 - 75 ' T- -L 4 ^ 4 0, 10, • 529 145s 61 0,725 13 15 -- 1 8, V 4 6 - 00 4-0 75 10 21 6 066 9 , 406 1 0*a* 1, -1.1 4 7 '1 -1 0 . 76 00 - 4 0 o - 76 -iS 6 2, 9 2 8 .1 + 36- il4 6 1:. 1 , 4693 012! 0.43 -120,56 -6,5 1 7*960 90002 1 +699 6 "2 q uo -04-75 8 -11-04 -13*75 7.628 0400 -0*75 0 2 - 5 28 69472 1-729 t oo motlQ 7.465 j _ t go - p - m 1R, , 54 -16*96 59aas PO4'-14 +•-14.00 A 9 o 00 -0- 75 7 # q, 54 , 2-o117 " e I «9* 4 056: 7 400+ 5 4 -2:3+ 9 V 1.
07$^ 91 2o37,9 +,c 1 2 6 00 0 :ii* 2 5 1, 7 G Sa . - 26 -73 X 5 03 65 r : .7-736. 50 . 82 2489 , 7 vo l o 8-G0 -Q # 75 2,890 -24w76 1 ` 4 -16493 -3 . 75 832 4 51,67 -5- 73 - 9 2,144 w 12s60 -10457 9,330 45031 13 12d00 a 0#75 2393 43 u k'' ^.Ja<U siG ci'..^.
kI 0 Fa-1 !
T5ST 63 0 yeGGHT LdW SPEED 4llllD TUNNEL OE^,TA DATA i ZR^,B. 76 ,(RUN ,26-RUN C)t _. i000 11/20!81 1438.
' 'd SUPPORT TARES: ;HEMVY AX_ S DATA Fu4L SCALE DATA WIND RM/Q 7VO PSG; L/Q C/Q Pil/D SF/'I ALPHk P`MT 1 ,-12-00 ► 72 -4.75 *32*846 . 546 103066 0 037 2 "0075 19 104*98 K:3975 ► 00 - 0075 -27 ► 359 *102 98 ,57 0*7i8 8 -! 10 12 _.
w,^. 97 22C ` " ^: • " 0 ..15` 56 6. 1C^ b Q+567 ^ 8 0 57. 10 .
a«03.
5 X 1'19023.4 '- 1 U0!
X6.00: "CiM. 0 , ► 0s775 7 9 . 250 19 . "4*,79 0"" 76 A13..4S,48 8 1./+4:9 •4.00, 52:7 850,30 1.261 - : + K1* 4 3Z 6 rQ*.75 104•'02 L2.CrU 66 if364 7 # 861 ► 92 *542 -4049.
1.294 w lE M "0*7a 50023 7 0*a0 "1 ,3 90 7 . 561 -00.75 + -1211,7 016,18 2000 $0 ► 269 42*49 1.214 8 436 7 ..7 - '9.:38 -+CIO >75 79-9a9, 14+5.A1.i^.5* 4030' 9 4r^^0 . 34 6', 0. < --1:.1.047 338: 37'032;. 1. # 661 'x•51 -0.75 1Q 1 2 *044 ' 7 0.
> 11 -lU«53: *00 W 0f'75 ( '1,6 0 136 "1.x037 8 7.766 38~65 2.
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- •110,64 -0..75 45*96 80289 10 14060 io*00 1- 9• 910 8 ► 272 "9086 "6±19 5*436 55090 i*548 12-00 "0 0 75 2 30 1Q9
A-171
VC .
UGHT LOW S HVED 'Y41140 TUNNEL TEST 630 m DELTA DATA g I oNds 77 (RUCK 77-RUN oCb IC W, 1 11 /20/81 1438 AXES FULL. - - WIND DATA SCALE DATA SUPPORT FARES ,XkzMdVEU PNT PS,1 ALPHA L/Gi D/Q PM/fir RM/(2 YM/Q SF/0 0 0 , -160021 -12 . 00 04 8•499 -485#89 00 59 12.80 1 "1.532 y10000 2 " 47 0.04 0 11,025 wbo94 7 , 439 -179+62 -1,206 80,94 0 *2'4 -asiDo- Qr.:ok 10 7 607.94 -163.72 o30.
-0:910, 9,79 '.
„ 3 C0 4 0.6, 04 20,94 - 6 • . 829 60291 -1460. 63 . -0:097 '*70.21, -iw*4,. _.
W; 6 ,6.1 5 0oQ4 *0 0 8822 5.96,6 -129o45 I r.9'8 O1627 .yo,75 00..76 6 P0 2 4 00 "- Q0 4 3 0 456 5.767 n 107#50 0#764 Uo88 4«04 7 . 240 5x$62 00662 n 7 0 o U0 -87073 ,015 2600 0004 8 1U•54_8_.._59834 -6607 14, 0.568 -`1069 2047 _.-'.O tt 4.47 9 13 0 406 5.995 -1Us.28 +-45657 0.792 0, * 89 160'214 10 &0.00 0*04 -8078 6t2U -23.51 0F974 •0065 .
6. 70 2 $ • fl0 Q+Q4 150Q!^4 +909$' -0,.058 ii -3^ 18.
1040-4^ 70383 10 . 00 6,44 18099 -0068 12 22 92 56 10824 "13 ,2 8 240842 13 12*C30 0«174 8 . 320 -90 #1 4008 40o17 ; 10501 t ` Y OF POOR QUALI A--172 E 0 y000HT 9 T L 0 W $^T,.y,^30 r4 1[,;qP'T,^.NN jL, OE DATA ITA a I0 -d 78.
M I' (RUN 78- R.UN 10) / 3 :00 I^ 11l20.lg x,438 • r -: DATA. PULL SCALE `T'ARES .Kk1lQYEl7 AXES DATA SU WIND PPORT L/Q YM/9 P.,NT ALPHA PSL O/Q PM:l0 RM/G 8 E I Q 0*06 -12*OQ t33 u !36 foal 1 " 33 * 0 49 13+228 113.08 -1 ► 0*106, -27+774 0 8 8.55 2 -10*00 i1.609 99.89 5* -1.056 - 3 00 o k. !o23 81.3 003 -:a , 58 _ 7 X03 08 . 0& a ,1Q • 1.0ib .86 " - o . 41 8 4 w 0 >06 °:.-19.s .08fia 1*91 6*00 8+547 102 til3c ^ 4 8,a 70985 82s08.' -9,.73 - 3 13 5 -4*00 04,06 1._007 0.06 -1.05 v 6 -2*00 - 704 650,.82 " l U* 03 7*424 1-0061 1 .5 0*00 0.04 .0y 62 58 7 0 7.055 50e58 0*89F 1c S 2.0+0 0*06 3 9 5 60800 44*27 0.800 -9•Z1 0+59 ERGO 8*065 -1u ;82 0.56 0006 6.9836, .40.52:` 04:866 0.0 iBs'Si2 6+871 3 +31 1 6.00 U 8 . ()0 i6. 426.
n. 06 1..94 10, 792 35 40-o25 . S .43i -9.64 —.
m 12*.42 U,49' . 00 U.Of^ 2U•3 12 10 91 7+°10 x+6,3$ 1 48'22 -7*11 13 12*00 0006 23,05,1 8.863 57.91 1.430• 51.14 j 6b u A-173 ... . .......
VrJU4HT LOW $PeEO W11140 TUNN56 TEST 630 0 41.TA DATA 1 -12*00 -0#01 -34#317 13-395 170*85 -0#400 55s-32 -IO53 "2642 -10,43 2 -105500 -001 m a9 o:a73 11e766 163,64 -0 * 5598 ;3 to - wp 0 a 13# to If, 9u wl' a l OF1 ^ AO -1.4 , 146 9 07 ::3 4 "6 4 00 4 " 7 w4:1 0 cal P -al 81,575 I A. ' i n . 1! 6 - P c l a 4 + w *,I -P i, mn #Ahq 10.60 0. 0 9 "12 - g2 6 W2400 00.0;3 -80.942 v6o29 -11x.21 7*561 89o27 1o668 wb&61 w10o17 7#26E 5 68932 7 0.00 0 0 # 01 -2 18 24 10299 Qk6 - ft 6 *A 2, -12+ 11 6 61. - 60 1 t'248 IwQ 1 j O 4 * Qo .7 1: t 4. 6 6 -lQi: 60 -13,75 6.3t ., ) .0. ado lk , 13«16 600 - 16 0 5 G o, 5 5 w 9# 75 Il:• 546 Q7 I, 1:•637 ji so " Oo 15 76'8 'wo p 1 70433 50. 56 2. 027 12 -7.,4 10000 00001 2Q6112. 8.035 5 2.1,22 W 12,01 51,"54 4 mn m n e t a C l M4 . 0 2 4 8 1.3 2 C ORIGINAL PACIr-^*, 1,11" OF P0024 plun!lev A-174 YOUGHT Lew SP EED AIND TUNNEL TEST 630 QEL.TA DATA afl IRUN
i a 1 l I-00
SUPPORT TARES N-MOVED WINO 'L SCALE DATA &PHA PSI — /Q P M Q ____j , i p q 1?, 0 00 Z 3 43te1 0153001 i3o 684 130 .03 1 9 447 0 4 " 30,9 67 0 0 - 15 1 2 51 x89 wiSi 0,66
2 y 10 . 0001 11 29 , 204 65 -127 4 . 84 . S. 05
5 o 1 7 L 2 6 4 b w3 9 -169*,35 3- - 1 8 0 06 - -0-*01 0- 6*216 10o55e 14 , 700
4 * 0 6 0 0
36.& 1 3 -i6Z#,26 0401 021-19b 99422 137.8.1 6*317 5 - 0 O. ' '4 15 4 302 89529 27o:62 01 01 117#26 6#853 -4163 .
- Q '086$38 Ziw*O '4161 **3 6 *2600 .92426 6*892 7-995
7 " 0000 1^ o 86 o " 57•;92
^^ 1 0 0, 0, N 20 5 56 7o730 71.75 64464 2000 06,01 6149 2 82.72 "1540 :22 8 20596 7,667 6,307 "1 VI us W-F t 10 6-000 Gko! I 1 " R**76 0 1-f 2438 7*673 60965 64240 8900 1 15 # 693 - 968 0+' 01 1 7, 5?. w Q0 6o631 w I I # , , 0,8^ - 0 13 9 0 ' 9 2 I1 ._ os(,1 4832 12 10#1 00 19 '90 84 ,497 634,04 64868 018t.12 230580 "15 *i31+,94 1 3 12#00 0 .90,459 48.20 .41 54696 t14 ovlrll,mv^ v"w"A" M ()F P00Q. QUALITY A-3.75 YOUGHT LOW S PEED WIND TUNNEL TEST 630 DATA 4TA Q t Qkok *t$tov - wjj i i qg 4uo77 - 148*39 2 8 4 00 0101 w 7o*42 128 - 157 *16 ^i,$5s 7.
06000 4 -3*$8s d 0801 6&575 -1130*05 6- 199 31.41 .1156*93
5 ok 00, 033 ^ Z 1 2 #47'
0,91 " 019 542 542 • ZO- 3x1 Q Q 6 6*s92 1x65;1 -*107070 6 0eU1 64199 X 103 00
0 #0 0 0 01 6 & wa! s- •60 6 2O1 13 #20 2Q A l h * 6 $-t
9 2#00 0001 10 41. 6#267 *6 4 4,t7s 87 7,82 *i47#2Z
usp; ' I r.• V 4 0 Ut t:s " K 'l I t V 4:;j it 9 Itego 6#365 -43401 5.702 6qoo oq 0 1 tS ,q 798 64672, .0132.61 is -21 0, 44 5.601 ci - 47 jollg_ 01 1 4743.
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SUP'PSRT TARES_.RLMeLVED P8 P'NT ALPHA L/1^ D/0 Pty/0 9iT/.0 RM/4 ym/a M12O0o OtO1 69267 73x24 "1111.'90 1 "6 0 6 0 5 3 -1 .
903 5 52.+•80
•00.01 "199.50 2 -10+00 5 950 5+992 -141054 60094 60 808 .5+008 0:601 3 4*8 ,0 00 5#552 • 132075 6#146 81.13 0178*48 -6*00 380, 66 - 169 600' ° 0 4 . 1113 50164 -118*80 60 -72% 001 . 3.460 .4s00 64166.49 w 500'31 _-10508E b e 625 27.0151; 6 Or.Q1. "1,589,51 "2000 '-3071{.9. 20 ► 4+829 -88P.48 69488 19 .-20020 ,1517069 7 0+00 0001 4+760 14+61 -73+97 6e124 8 2.017 0,.01 o - 5.799 7.16 - 14400 2 "l ops 4+6OO 57*49 *0 440 - 9 0136045.
R++01 50536 09.01 9 207 **567. 43+31 6000 0 01 00609 -4001 -133098 4 0 `-280;2$.
10 434 54265 8000 46542 0+8,00 X13
0 0 10'451,. 5 * "9 10 2'
It 01 0-12003 0 01.01 .2e273 4.569 -164,16 -138+109 12 10 00
C, 5,,1-79 5.627
0+139..76.
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06100 fo•ot. w2lt645 7. 0 3 1 1 5 6,699 40 -2 , 61 f45 15 2 4u • 40 6 - *4tOo 0s 0 1, 417i85s -166&76, 7*232 28v26 .12200 6#773 W134549 6 -2*00 0.0 1 6o691 6,594 22o-35 v R 16U•1* B8c28 .
0 10 4 526 06.Q2 6*194 60418 6.328 1b*50 6 - 1551,79 :^ 7 0400 2600 003 w 6#569 29 "i51#,75 8 5#734 8.
33-47 6,200 Q wgj 40, 00 : P 4 0 483 5w5O3 I 1. 0 7 0 6*003! 146 - P 1*5*,79 -00468 - 86 6. 100 0403. 50299 10a34 +5 630: - 144q-86 -14kq 5!965 0 0 245.76 5.oi57 *32 a 05 w.9 4,33 - -i42; v .55 it 800a 56 8.64 0 c03 , iz 10 0 00 5*202 w 65t,64 6i33E "17*12 8 146 # 37 64 178 06.02 12000 9*763 6 1 4 9 0 5 564 w 80920 60316 w0 i4 - °,95 ^ c R i d U ' o C A-178.
^t '' VOUGHT LOW WING TUNNEL TEST 630 SP EED — pEL,TA DATA s s B Y n ( RUN 94 -RUN' 50)/ 10-00 3 k a 11/20/81 1438 z k _ TARES .H^-MeVED a AXES DATA °FULL SCALE DATA sUPPORT WINO YM/® RrtfG1 p$_Y f' i/0 SF/Q ^!Nr ALPHA 4/0 al GI 3..2,1 54.53 6.232 •0.:02 -16495 5 7 1P664 1. W12000 " 60 31 .
2 1.098 Ua61 .3+,18 0002 5 0 7.22 6+153W,33 3 010.00 " 5.5 15 wIJt0*31+ w 0s592 u*37' -34W 5~317 3 3 R8# 0 71 4_= n3.• .7«3* 4.895 4±124x92` 0.013 4,. 06 ,000 -0 6 02 50 J r - 3 * 9 6.92 ii'*09 , _ • fl •02 4.665 - , 1,07.91 0 434 6 4 4•00 = • 3 . 261 "7.29 o79,94 "8 . 619 6 x2.00 0•.02 4+495 -92;x'20 0.529 05*73 -6,85 `1%903 • 4#329 0#396 7 0 4 0.02 0 75+•49 3 00 -7.25 •4+,i5 0,166 2.00 04.02 -00968 4x1'67 - 59 * •09 a 8 '.!
^O r 17 3 -3 0135 Q.235 "b t 0 .0.2 ?} 0 067 43 tap 4.O q s 9 *7s71 ^a1^:0a 0a09$ : 0 0' 42 ;3x93 76- 6 x 00 0W6 88 -26 .
.0wQQ2 w6*94 1x03 1.595 3+969 • i2.76' 8 . 00 00,02 1 ^ f •0 •,18 0'7.93 20424 4.067 0 e x,55 0w,02 2,54 10 4 00 1^ M40,25 o0«04 36335 49265 20.,66 0023 s 12+' 00 0602 \ 13 H fl n QUALI,-ty POOR Of el YQUQHT LOW yjJNQ TUNNEL 630 SFEED TEST .DELTA DATA k J,; r .: (RUN ... ..._. ,
...._ ..+. . _. e5-R UN i. C) / 1. •00
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• 6e00 0 5r8c7 4k x+173.76
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ag °0 0 345 --60+01 5.8'1.7 7.7
0.43.., '4•;8^4.._.._.^4.4Y16 .._.- _._., f - 9._ - -• _.
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016182.1 s ' 8400 042 -116,"03 3 p -6 W -979 7«380 08 55, 4 41.42.
-64?C7p 01*Z*o$'t of 0 02 5.735 33:.22 "1540164 '"3 + 547 7.02,b 00. 0! 23850' 157*69 ''°' S 048 2 ;—. Q .700 y 1.24•.21'' 6x260 4 i ^ • _ 180,04 02900 09:02 6.567 -105957 69?68 M1579^46 6 3 ► 700 7*5Q7 6!695 25 -1521;52 7 0 +00 OR , 02 0 89#,54 law 6#028 ri.no 1(t.7nc t.K31T r GK r. r 2li n2 8s.38 .. -. ^146^.30 ^^ G ,--,.- - 0 -140.00 9 4ROQ 134607 829 - 0 . 5.439 X12 Qitoz 6 44 87' 0 23W72 943ktASO 6 . 00 002 1 6. 150 0914' 59-!587 0.39:50 0132.51 a ir' asoo, 0•:42 7 . 366 X1930 69027 '' 01 031 l.t 19 . 143 – 09;02 .221 - 391 0132901, 12 10900 8#1,76 19.49 69433 .0180,88 12#00 09:p2 24¢359 99163 40.99 w15#76 -1a1+30 13 59681 t P G' Y • F IS ORIGINAL PAGE TY QUA OF POOR LI y A-IB I U0HT 'LOW SPEED WIND Y e TUNNEL TEST 630 k° DELTA DATA lDgNe # RUN $)+*RUN 10)/ 14100 1123181 143 8 _ AXES DA A ULL SCALE SUPPORT TARES.KLMBVED WIND DATA r PNT ALPHA FS 0,/Q PM/Q YM/G L/Q SF/0 RM/0 *33.234 1,50558 1 0124100 000Q 6.26 7«o4 106x46 w1 6i9 •04100 *.56 2"*,:79 -27* 5 93 98.36 -1 * 1i+854 90 2 ` 10.00 erg. -0.802 *U 02 34167 3 0 0 . OQ 102.73 34 14 = 340 06*-00 0.00 4 9-055 100992 X4.73 -041,73 " R 1 8 *767 Qv l3 -40 5 -13 0 049 •6167 00 0 .00 802. 36 *'!^ *.02 81.57 0 9-540 02000 •0,0Q '-711 075 -8,•24 6 63902 0,701 -3041 7+712 .6 47, U0 OGQQ -1+02? lod*39 -4!87 7 7'430. 47+92 0,543 00-00 8 3i902 79135 41*49 0.302 **7' *01 -3x12 44 1 00 0100 8 w7,^64 *4090 7 1, 067 y $4197 *20i 0•.510 0 42 r 6*Q0 7.204 364108 87.97 -4«64 1.0 +00 041? 4.83'7 8*00 1,6 66.8 7*567 4;:13 11 0.00 3fis7^'5 x,274 *'3071 .
_ f Q,, 04 411.6 -2+'67 12 10i00 2 0 + 5 94 84275 44073 812 1e56° OvUO 25•640 13 12x00 90125 57,19 X6,, 13 1+39 1,065 h " " A-182 ' I v P032 p U J. TY ' I I 11/2Q/81 1438 PULL 'MLMdVED eiIND AXES DATA SCALE DATA SUPPeRT.TARES^ PNt ALPHA PSI L/Q n/Q pm/d spin R ri YM/Q *109p1 8 2 #^ +:a 9•;0 1.
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-00 39: 01 W IV26 I ri W, 0 .8 - 8 .
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w Oo x ' Al ' 1 030 1:o 6,00: 01 % 96 . 4 .06 , . 01 0 0. 1 6i3 34 a5 06 8*00 99 ;399 47- 1. 0 6 •89'3' -4#17 11, 1 1- w11 *,62 "0 . 01 2906 -4*:62 12 10 ,0 0 2 00 409 12*071 54,32 6' p x.2,2 12000 $0 0 1 O t 239397 139030 o3 0 13 66470 1x9584 n TY, A-183 OF POOR QUALI , LeW SFEEJ) V15U(3HT W114D TUNNEL TEST 630 f, -I ) ELTA DATA I^tlVO^ ' 11.120/81 AXES DATA WIND FULL SCALE DATA SQPPf5RT TARES.KEM6VED ALPHA PSI L/Q /12 YM/9 PNI pm/a Ii 5 0-'73 i o 124C0 - 0 0#01 -34 o 161777 111*88 a 0*852 0'17 0 558 , -io s oc) w okot *29 S0384 1"03 F34 11 , 8#38 0 0#637 ; l * a aws'.rp aw a, Q VVIT'r c*vv lo wkV4 135w87 ;, n 0 4709 4 , "6 0 00 ', 10 0101 w 21 101 129774 127s,43 Q ► 644 w 1,61 5 -osoi *iS•349 lz#036 11 . 4 , i77 , .-I**36 1 - o z6 #!6e77 w6 , 6 m s 2#00 U #,Q 1 11o562 1 # 46 -14 0'87 * 18 a 8 15 9 0;65 1 .628 7 0900 KQ v Q I p2+709 4'^^ v * 6 9, 6 8 1 3 9 a 0357 75410 1.369' 1,1 676.iL R oa -0001 1,531 -69,62 .-i8o , ,06 a t oo , 20473 ii 0 124 7 19 4 & 15 9 0Q:# 4 0!50 G 33 63# 6-9 17.66 vO 51 • 1 *91 6900. MQ44 ' 1 1• 165 59. 2 31, -18950 1Q k21' 11 * 8 9#00 -001 15P734 1599.50. W9,99 - 17 * 14 1 1 ,533 2 .62 ' .'
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13 001 24 0 063 9+297 42!39 1$530
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ii 8-1.99^ 5009
P146o2j 10100 , w okol 19*847 8#738 60954 7 # 243 m 180. 78 12f00 . 6 * 584 "18w7$ 0137f78 13 m otol 23492. 9 9#763 460, 55 A% PACE, crlltV , or- POOR QUALITY A-186 0 1 OUGHT LeK S PEED WIND TUNNEL TEST 634 ..4TA DATA f (RUN 1 92 W PUN 10)7 1.
11/2Q/$1 1438 m AXES. DATA, FALL.
WINCE SCALE DATA SUPPORT' TARES .RLMeVED PNT ^Pty /Q SP/0__ RM/G Yet/Gi -412000 .n,ti01. 16+551 6Qo57 '-(138862 1, 11794 . 0 4.722 "1.0.00 '0601 48,13 2 *! 29#347 15#730 118.16 4.905 m4 138 ,35 ^ *• •^• Aga ^ •, 3 *p1 13*95 .7 1,38#38 4,i40 # ,s '^ 169 5 450 -14 441, ..i4g:,-3g "00VO v llQw 1# 32#66 w 98 13.1b5 ..13.1#^46 0#979 ^#^OQ . 00ot 3 ;6 X159 00 5 19#436 21#53 1184-24 6#426 - 898 44 .2900 0%Ql t 6 +955 95#87 6#292 17,.66 "1,45wOO 0.00 0.01 m2-822 =141t2* 7 78.56 6 x 1 ,#9 1205 11, • 683
2S GfUU_ VR_T "^v1t /t` *oi v. rr r.. .v
C`l•a6/ U•8c1Y ` g 4e . 0 0, ► B 1 01r 70110. 6x023 uae0 4132w47 99 5 568 I1.
600 Ov 10 I x1- 4 41:9 j j t6- ?2 62.28' 6 X5,.;13 133C!)
w347 ,o 4.Dt ► 1'Si w 11 v13 -t133*39 li 8 OD 9 110901 61#7 6*840' : 10100 0..01, 19 955 1,.2.666 *41:39+82 62.39 M Eu9, 0* 12 7#389 al 13 #2-400. Oa,41 23#719 11#23 X4137424 ^.3r455 58#•44 6x655 r f ^4 V^^ # Gr, QUALITY A-187 YOUGHT LaW SP EED W.TND TUNNEL TEST, 6:30 QED TA DATA :93 10*0* 4 ARUN 9 -3 • 10.)/ RUN It ?i120j8i 1438.
WXND AXES VATA SUPPeRT TARES,KEMeVED PULL SCALE' DATA PNT ALPHA, ' , PSI to / YM/0 Q PM/G PFIQ RMIQ J, s m i?,100 -oI37ti6, li3; - 62 *4668 59# , 79 0., 4 @13 Z- 8 31 17 # 397 a mictoo 040 5 876 ? . iS -876 131,56 8 4 -! _ 5 a f__ 47#48 0 13905 .
..
04 01` * 25. 1 P 40%62 ••141 #b7 3 -8*00 _ t - 3 01, 1 37.37 — 5 - 0251 _ _1 4; 4 w 6 i OO -OoOt -90168 13*301 130,17 3168 -146' 1 6 5 !794 a wit"o . 04tot. -I ts i o, 12 . 636 , 114OU 6vi9 21076 -&43s,87 li 6 02*00 04.01 "8 6 509 16 .*Z m139 v69 1,2#193 93o56 6 # 094 7 0 # 00 001 JF_oQ08 5 * 968 11*47 2+5 22. 7 6/ , 84 t]1_ 2=0Q 6. 21629 j19786 t5 9 ,, 9 8 g 133 o 6 0 69920 5,700 J.
9 *000, 0 * 01 7 •131 li*616 . 6*o6o 9 0 01.3 5 v 795 iO 6 . 00 '090 1 - XV 468 It•SOS 6Q : ;12; - , 6039 '129*76 1 16!110 11, 81 1 -11s29 14 1 3 1 00 0001 IS w 593 12-135 60.25 6 ,731 n 12 10 0 00 O • Ol 20 , 022 12 q 833 60. 0 50 7,323 19#, 75 0136430 bi 6 89 13 12 0 00 0001 23 +625 4130050 5,34770 56(157 6@451 Vqq PAC is J44-M !IF, A-1 , V8 y LA
_
Q g
poo
or
YOUGHT LeW WIND TUMNFL TEST 630 S PEED ik DATA D2 L,.TA YO r 9 4 NCl t RUN
94 W RUN ,.10)/ loco
11/20/a1 1438
SUPPORT TARE$ .mi:,MdVE0 AXES DATA PULL SCALE DATA PS L/Q SF/Q ° . Rtl/Q ALPHA C1/Q PN'C, RM/Q - _ YM/Q— -- 64.47 -.145t07 419000 0334812 270 44936 1 004 17 . 1.14 407 52.7 7 "148 74 PM 10 40 0 0 0 290? . 1.5.945 i15•. 43 541.52 t0 i E.
`, -151 •°07 *r26 *01!4 5.621 46 01, 433t83 3 3 -8900 14 345 354:86 -03W33 4 o#QJ 89,9 13#387 '06000 ',127028 6tiU of J -i5oI27 2b •67 ml64.,03 ^..
1i4o,44 6.466 5 :_ 0 4.09 12 4596 6 0.,01 o 8t7*o 6#518 "150440 1*21UO 12#229 sa*o8
— w1 8
4 2 4 9 i °4 08 7•. 7 o, 2462.4 1 1 51a0 q 7 x7 4 7 0400 0A01 6-4- 7.86 ^143^k0 6o C27 _ t -- r1*0'*Oq: U'81, 7.191 63• 6467 9 Goo 11t66 g 7 0,00 1.4. 25 Go. 01, 11 jw .6o. 40:8 *137«94 6•a0 836 10 11 ► 60.1:2 P *i39r92 • 1:0408: 60.6 'x•05"9 8sOb 0 471 15 . 668 12 . 134 ii.
-I*Sf,46 10000 Ot0l 20.068 "S800 59490 71538 12*909 '+16.95 4 .90 01400.25
0to1 234947 131732 55 6o5 88
12400 _ ' A ^ » ey of pooR QUALITY YOUGHT LOW SPEED WIND TUNNEL TEST 630 •DELTA BATA lO•NlO• 95 (AUN 9S -RUN 61/ io 0
1.if20 j81
FULL SCALE DATA AXES DATA WIND SUPPORT TARES,K0idyU PSI 1. /Q 0 /0 PNT ALPHA 8 PK/a. F m ot-07:-24000 24q,99 -265 61 I 7 # 856 30 0,171 -480.926 2 =0#07 : 1 - 2261 00 60830 28,233 24#46 :i2*t43 8#.42 *46v09g ,i , wO * 07 1*20o,00 40747 09of J OI PR A 1 4 041 ..IRA 27.09 10 2 &0& • 1 89 -00 70-#94, 40 1.6 -P36 3 . J5 2*t6i 4 -0 9 07. 3 w 576 22 1,206 P-015 : 00 16 v09 2 ' t 831 5 199681 n31oi1l • 40.00.
5 62 . 22 1^ *.72 17#262 - 2, f-j q 8 Q 7 15,.71 10920 6 w 0*07 "1490Q 69w15 108 07 4 0 0 07 -124Q4 10295 15#753 63a80 w22o241 -0906 7 14x37 0 # 955 J4 * . 9 l l8s4og 15.7'1 .1, 41 ;, 7 1 8 xv G s 0 7 -w i0dQ0 41 70 *•42 m — -8900: -0007 1 * w-26 -48905 ' 9 0*100 13 *'&0 0 72,68 a 1 2 # 9 1 4 X 97'9'27 10 - -Go07 -649 ol v 0 79 13419 -1a3 8 8207 17w36.
1 1 -0 9 07 so **00 -1-775 13s222 SaC53 -24 , 969 1909 -ilS%75 a? 4 ' : 2 - ' 130 1. 15!# *,28 iz m Q t 0 7 w2 - QQ - 106 27 i2 t, 06i 91s73 89t56 31449 -i40* ' 64 13 m 0w07 0 0 - 00 "1 95 36 13#193 49536 26,.68 - o 14 w 0o07 2o00 *1o656 13o468 88 .42 8.Q84 138t39 28 873 -4152#,96 -0007 4-o50 17 1 9 3 a 3, t, l a 95 1 5 81*70 , 120533 64,00 goo f'876. r 3 16 -0 @ 07 4052 ► 48 72 q , 05 l7o744 1 -t l 95 4,78 goo ^ o 38 09 o2li*46 17 -0 9 07 0#066 14 o 6-OZ . 5806 21 * 650% , # 693 39 * ;83 26 0 278 38 # ,55 m 0oQ7 10 #, QQ 1<o169 "22b w29 is 15 1200 2441.0 1.9 w 0#07 164807 28 4'02 3 . 0 o s 4U*78 -248*83 3 # 728 18-336 *1 . #78 *275.08 20 -5 0,07. i* v 00 16o51 35#973 3 s w.9 6 t66 21 07, 16#00 i 8 1. 19*910 10+54 40o583 -SU2 39047: - 1 22 -0 6 07 18*00 5*2,58 '22*21S -1 * 04 46 1 337 328,13 0907 20*00 6 & 241 50o525 i 37 9 9 0 w3b9977 23 24 9 743 -69, 45 -351-v699 24 -Q o Q7 7 143 111, 16,98 2 26 9Q 79 27 p - 5 91 551693 - 38- 35 25 o, 0 0 07: 24 4, 00 89423 30#572 * I _ 207 37&•73 -41 5' q 27.v' 60#482 1 M
pl ^ C II E ; 1 5 1
OF POOR QUA WAY A-19 Q, (RUN ... 9, 6 so R 11/20/81 1438 DATA SUPP15RT TARES KLMtVIED WIND AXES FULL SCALE DATA.
PNY' ---- ALPHA PSI L/Q O/Q PM/G - SP/Q RM/Q YM/Q I votQ8 31PS67 .
: IWZ4000 m ot 6 4 %450#3$1 3f8 78 c 4 ''o 2 - - 22WOO 1 23*•13 117 9 7 2: 2 3. 28- o lio 6 - 2^. 7 -446. S Q3 - . 2208 3 -0.08 : -20#00 60072 26 29969 # CO7 109"•77 2 6 , 71 *44,048 -0P08 0 18*00 28 .,32 82, 4 4 #8 70 23.871 37,67 • 39' # 410
-16 * 00 4 0 Q,o
5 -00 , 08 21:080 494-217 26,70 50 ^ 37
op-3 4 * 6 8 6 mo*Qa *14400 8 . 1 7 1,,- 6842 ' ,5 x 21640 300 42 1 +294621, 2V •. 41 Q- - - , 1 7 ,-74 7 7 -- "' 62 - -1 8 10400 2 9::02
m0#08 w 10590 15. 994 7^o -20.572 1 6 c 63 '-
2 .9 0 4 873 i5 l060 7 70, 4 1 V5 * 294 0,5 -5 .20 0 104 1 052 Iia•'76, z•8o-35 0 013 - 6400 OQ q 179 4 4 427 84 0-7Q.
-0 0 0 08 •QQ -0-$64 , -,14 i 247 94 - t*80 -4. , , 843 18o*4 "102*43 .
12 *Q #O a w 2 4 QQ w 1 43 86 4. 037 487 wO a-338 2U 79 '•118s-74 14 iQ;t 3 584• 31467 -o 13 1+ *$,} is -0 00 8 0 # 00 "1 416 14 4 337 0''97 4 4 0 R 9 00 -14 687 14-1 . 4 E58 -9 9 # 53 "138ci3 8 * 072 26# 60 1 4 WD-G8 687 I ii. -0 s 0, # 774 4 8 •14 92o*6 269,58 -161 •25 12' •577 16 40 0 0 08 6- -QQ -& +121 , t5 8 1, J + Z2^ 17 t r,$U a3 9, (?6 -0 19 1 *10 " s of oo 0.I o oo a, 5, ,* 63^
68*,26 V •214739
36.89 10000 18 M0008 1:• 36 V!i4 0!228 *.3,4 386 j 4944 27&';D9 • iq -0008 4Q0 2-754 31 * 3$3 34 4.54 37.5'9 N• 24 9 4,44 1Jr 5 2 6 4,44 3.6 6a 4 20- 0 40 8 14 4, 00
22,84 35,331 38,27
^27 1'9,78 21 16.00 -+0406 2 - ^66 79 # 711 6.
4 39#6 44,6 SeqS6 w29669 22 00408 18, 1 00 5 , 569 , ' 22 372 3093 4 1,4 55 N!322 f,,*6 444822 23 0 4 0 , 08 20,00 6*984 25 045 * 2.08.
500213 4214 9 .4 367 •zl
,. ' ..9 r 24 22*QQ 28*Q12 *14451 564572 *3o. 30 ":Jdd •33 g 0408 2* t 99633 QQ 121 25 31 4 *26431 604k )4 )4 42! 4. 38 -413710 ORICIMAL PIMR. E$ OF POOP. QUALITY V. 0U UHT L d W SPEED WIND TUNNEL TEST 630 DE4TA DATA L a t NO 57 g al fm 4 FULL WIND AXES DATA SC."ALE DATA SUPPORT TARES ONT ALPHA 'PS I L/W n/Q ph/G y Q la *4 , 0 y Ml .1 t W 12 0 00 0 0, 03 " 3398 17 0 424 114986 7.248 62102 -162444 -10*00 43 w29#426 15*836 2 2 _ 127,10—, 7 - o, .98 -167-,4 X 0 0*4 *,00 0Q 3 , -256. $68 0 43 138o3B 7,I07 4 5 , w; L 62,,66 -1 1 4 . 2' P -6*00 043 *2(J*629 13o,35 131 *48 7-F, 272, . 00 00 160,01 5 .
O 4,03- -14*745 12@765 113#36 7 ' • 372 ^ 28 1 - 166,025 "2400 0*43 w 8 w 67j 12o277 9SP86 11 A ..7# AV L 2 2 w I b U - 1 4 3 0$Q3 M2J5p ,2 J6 #-/.o 16 V.22 -14bo.64 • 0-741 i AR5 1 868 6 9 8 "149 21 - r — t 05 ,5!5 2 i oo 0003 2 * 73 3 1, . 4 :L 8 62.62 00- G o r oa 7.3 17 6*348 404 7-17 1 1 . 800 554 8a 3 01 0 Zj Z Q 55 4 11, 0 -a 00 0 3, 110 3 4^: , ^6 vo 4 47 -, 3 It 3, 3 ,70 tl
00 0.0s, 15-S oi 1 1 L ZO C 59w . 94 . 6o - 940 i 5.8 4 *138 13
t 60092 usos 1J4833 7o , 203 4 9 -14 4 11 00 24 •9.89 %.
60.70 00 OOQ3 24,519 1 0601 6#28 , w 16 * 78 - 141*26 13 12 f . .......
.......
ORICHNAt. IS or POOR QUAL V, YOUGH'T' L5w S PEED WIND TUNNEL ,TEST 630 QE j T A DATA ZO * 98 #.NQ JO )l (RUN f
98-RUN : 1 .00
11/20/81 1*38 AXES DATA FULL SCALE 'FARE'S :8tMtiKEO W'^f^'D DATA SUPPBRT L/W D/P PNT ALPHA,. PSI PM/G, R'M/Q YM`/Q $UQ a 1 -12400 00.03 - 1 33#553 174408 57492 115#68 -11,55k06 64834 -29-491 48036 -+1:56.67" +10+00 0t'^3 .§'816 2 x 6 . .5$5 1 2: 57 _ .
.25 -.8 47 3 m8.00 10,339 ;wldQ0+4 0403 136.156 4108 0 64844 0..03 -6-00 -20978s° 1314. 33+85 -149,43 4 . 15 130+16 6x757 , *4 . 0«03 -14.810 ' 64s ?.4 26 t 44 -iJ+6*53 .
5 . 00 1a#7-62 1120 1 35 , 6 - 2400 0s,Q3 -84245 * 90 -11399,10 12#282 93099 64525 19 0400 OcO "24389 13#70 0127tiZ 7 124028 76,78. 64361
200 0 903 2#696 68490 7.'L =i cn'sic
8 #75^4 6#OQQ
.
1 4#00 0903 ' 7.1284 11-6805 U.40 - 1 14,9 15 5 62t,,95 6,rt 1.00' a ir,4y, 0'0 "!1:2.6t.78 6 . 0'«Q3 t 69 t. 60439 *!
io -1I 637:-. 11 4 9-06 8 s 00 0.,03 15 1# 493 6 0 t 2^ 11 493 12 t i.68 6,671 . 0 11 x,34, 97 w 06,03 206315 8 -113 5&08 10100 620,44 1898 12 12 4 804 74108 "- 1 t 0*03 . 24478.5 13#781 60,,16 -118#09 0137+0* 13 12+00 641,62 }
i
A-193, POOR. QUALF01 OF VOUGHT LOW WIND TUNNEL . TEST 630, SPEED DELTA DATA , ^ ARUM: 99"RUN 'IC)l il l oo • 1112018.1 1438 . Mk!MdVEL) WIND •A KS CIATA FULL SCA L E DATA.
l SUPPORT TARES PNT ALPKA L/Q D/9 PM/12 YM/0 R M/ 1 2 t 012000 6bw*0 -176o50 0 43 "2 6 017 15 6 270 150*03 8135 •0 .,03 t 352 54,48 -176's91 •io s oo vm 25•2J3 14oO52 151s51 8 , M1,64«85 15*f5i 4 1 4,4120 3 0 8 .0 00 06, 03 -24 4 051, 13 0 099 6 153 +K21 • 36#99 16.6 044 4 6000 0 403 l o 117 150 o.6 1 7+980 77 1 2 .
0 : iio3 26 *43 -mr14il* ^3 m 4 4 00 '003 18PO ISS 3 5 i2o * 186 - ZgS59 , 6 w2#00 0# 03 -14 # 224 91953 J63 2u,84 ' K I39#-73 10"795 7,163 7 onoOn 0r: wii * 3LL I il a F; 76 74, * ,39 8 t st ' p - f; 12 * 39 - ( 133 C22 2#00 8 0•,03 -7*0J7 2 IP 932 4260S 6,446 5,81 0130"*'52 ( i 0 . 2 g 4000 0*03 W3 0131 — 91603 9 19#59 6 600 0%03 0 4 ' 69 9 39 7. o 07.
, 09 OW03 . , 9 0136 v,92 84 2 : 941 t3oa -a2vo3 4 .6 197 . "11V16 1 000 00403 680 "119 , 59 0135#16 0 99 91572 m 46 ► 18 69921 0 ., 03 13 12 # 00 9 , 750 10o100 -71o. 04 6015 1.908 - 4 1351495 .. . 0 tl ORIGINAL OF POOR QUAL Y A-194 1tOUONT LOW SPEED WIND TUNNEL .TEST 630 . DE 4T.A DATA I „ IQONO# 100 ;LL t Ci . ....
l! t./ a.. ^ .w r _ n x , . ,. .. it ..
/2D ^;1 1'438 I^1 AXES DATA FWL4 WIND SC ALE 04TA SUPPORT" TARE S .RkMCVEU p PNT ALPH& ^PBZ L/Q n/Q PM:/a YM'/6t ,i QUZIL17, A-195.
YOUGHT LOW SPEED WIND TUNNEL TEST 630 QE I-TA DATA [D O Nev 101 1'1120/81 J438 WIND AXES DATA TARES.Rk.MMYED FULL SCALE CATA .
suppaRr
PHA PSI L/Q, YMZQ INT A L /-Q PM/Q 0003 *36#304 18 i "12 q 00 307 14307 16#6iQ 71..92 v!21*v19 OOQ3 OR 2 -10000 16,771 58,,45 1 200 0 30 0 929 139 •,02 14 l ,849 3 - O 8i*0 043 = 200983 15#385 131#12 14 # 579 46,00 "019414 4 mw*e 00 g s,03 m?-1 9 1 "168«28 Got 14911.7 :1.251 90 13 * 636 3b W85 *28 4 4400 0*93 m$5*3!§9 -- J ,4 LU 26-93 -015-5-57 1 3 0 -9-2 12-737 6 02000 0*03 " 24 f 905 08 12 O8 95971 11*944 2U•55 "145f20 0w03 -30428 120461 45 7O i OO 130. '4137x33 81448 100926 8 2i00 00,03 70*27 1*997 i20166 99678 8.06 -!128e% &1 7 9 4000 0002 ' 12*068 "!122'w73 9 624,85 9.372 06*61 -!120&46 to 12o239 6 000 >06 03 100 7 , 73 5 7 &.9 4 , 9 440 11 8#60 O.W03 1,20.23 x 119«,,63 63 15 0, 169 129522 564 64 9:451 t2 10 0 00 0 03 -190396 l3 s Z20 58601 I -q 12& *'0 3 9,524 wq 2U • 09 0•,02 '230869 14ol9i 13 12s00 56017 R18#70 -q226't.02 8,257 OF P OOR QUALuv A-196.
LON VOUQHT DEED WIND TUNNEL TEST 6,30 DE DATA LTA z'02 102-RUN 10)/ 1*00 tRUN 11/2081 1.438 TAREB.H Meft-D DATA FULL SCALE DATA SUPPORT AXES WIND YM/Q — Lin D/9 Fklm/G RNT ALPHA - PS 1 i 0';Q,'2 036 -212*20 1 150871 66,97 0q12e00 o180 1 7.9 1 -14 80 18 M JOGOO 6 s 8 9 - 199_ 17 309726 1 6slf52 00 0 4a$16 '"IS O t23 0 0 25i978, 1560,80 0104 's 14.294 3 1 48 s a9 13**85 33*62 •166t69 4 -6*00 0*02 10 * 11 5 0 13 . 763 1 28 ip 8,O 2 1 r .
25.10 01634,14—
-4*00 -0002 *I,5 05 120921 ii6so 12*451
0 50446 1qo6. 9 -1*1*100 00 , 02 120389 9505'8 118474 6 0 4400 124, , 18 "13200 002 0 30588 12#066 85q . 35 10.571 7 0#00 0#02 90 '28 2400 10923 11 . 833 72.83 d ip 8 A 3- = 4 11 A^ a 19, 2 A 'A L ii -4 Or 5 3 ;v 41 $ :3. 7 1 '% 3* 01 1b# -009 63.
6,00 .
10 A 0 tC2. 3 1 0 0 937 11 1! 840 61•+x1 5t?-70 • 119•:0 2 042 15 . 20'1 1?#233 690841 81 00 0 it 1, 9 190 .-2u•79 * , 26 0 002 415 120937 59191 9.387 12 10900 W421146 24.020 8121,3 "19422 0•2 13.835 58977 13 12000 a" - YCUGHT LOW SPEED WIND TUNNCL "TEST 36 OELA DATA P
a^
_ _ _ r^ ZQ ^ HQ • 1..03 aG (RUN 103-RUN i0!/ Y000 :a , 11120/g1 1438 WIND AXES DATA FULL SCALE DATA SUPPORT T'ARE3 ^REMCVED sa PS P T A L/0 M/Gi PM/a Rm/W YM/0 ALPH SFfQ X32 r 650 ,192.,58 `1,2!00 . 0 r02 1.9.91.1 63w35 1 •141 + 41 14.043 "28:83 3 "i92.460 2 ^10.400 0•`.02 i8 o289 . 1409:29 1.3.684 53+`76 ' T g e17 8 0 , 8 6 00 } 0m,00 j 1& 20 4 1,6t+61 13^FtO4 1t°
3 96 53^^74 * to
/ ^ 02 ^ j ` 12 , r r^ i + ^ 0 64 0 0 002 -20*2*7 .13owVs J.'^.,1 ` 54 ,16612/ 15 .6 2,01 12.345 w ?*690 -154 98 6 000_ : -0t42 -V5,0112 i4+260 114#37 1 #719 6 -2+00 06,04 "96552 «73 -145%26 1.3+550 99*24 11#867 18 7 00-OR "13606 0000 0 3 . 987 12+838 1U 58 84+96 10x999
r
2900 002 4.t^0 *130",,66 a 1-928 ^r0.S09 - 7^•G5Q 4*00 0•:02 ^ 6117 +:f 85. X126+ 4 9 1.2.5 .3 9•.974 3r92 - 00.0:2 -R122 *93: 4900 .121639 r fo l l f i >i5 1ST 61.17 9C%04 $'C'0 Qri2 58.08 15.03 ^'i20r82 1 6 -826, 13 # 168 9+898 10+00
12 UO2 219156 13+700 610 6 9.757 : 0 22rv4 x!126*84
12000 •0.02 F y126r67 13 25.653 0 769 )^90 8.546 : w 2U,-85 f , p s ^m J ^ v b .^ i a^.^La kJ OF A-198.
SPEED YOUGHT LOW WIND TUNNEL.
TEST 630 DATA - DE LTA ^ __ __ __ IQ Ols- dt u i Fi tit Ni UAfRt?N i0 D l 4 900, 1112CZ/81 F438 .
AXES OATH ,F2EMdVEU WIND DATA SUPPORT TARES ,Pg FW A PR A ,, tw/Q 0/Q F ♦ t RMIQ YM/Q fi/U' SF/Q 0 *130t,00 W12000 009 31 0 047 190827 125007 51634 47057
i
•0•:02 260.i1y 3 2 n 10000 mi 270025 128 .79 5 , .128 38 .«28
17 49 7 6
- 08900 GoOa • 24*42+9 1:36wZ9 32r44128a1'7.
16 +1 55 60086 r .
-6900 ° w 19,8i9 n 1350198 4 0r,0$ 14.7;96 129+87 6.702 27 -- 1 5, . .4000 -1 4.5 84___13 s 7'22 -1394,68 5 04.02 115,32 7.Y2 194,42 .
6 -2400 0woz "a-9i0 14*,86 -137e28 130218 920'59 7 *1,44 e 0000 00.02 "2+889 "1361136 8.89 7 1.2 . 721 740 , 92 7,082 2.00 0902 65 .:7 *133073.
8 2o230 i2o367 2.59 7,i0Q 7f651 3:53 -132'l018 4-00 0002 124 1 60.01 40.12 7.337 •, lZt585 +t132'iI 102: 6000 0.:002 57'976 420372 7.551E • 0 11.7 °7 0• 102 17.392 _ °12 . 968 56.24 0 130 f g!
11 a 4, 00 , 7.831 a 14.53 - 10.04 '002. 210880 570.76 - , 19097 *94 12 ,130570 7.955 i2000 26+031 . 00 1 080.X1.3. +146 00-02 59027 13 140392 70087 , a OF A-1 9.
V O UGHT L o w SP EED WIND TUNNEL TEST 63,11 - L) E ^TA DATA looNe q 105 IRUN InmaRLIKI tali lonn i1/2Q/81 1,4?8 AXES DATA FULL CATA -.RkMf ES JYED .WIND SCALE, SUPPORT TAR ONT ALPHA pot L/Q 1y/Q PM,/Q spia RK/Q.
52*88 *146o81 i o12000 042 - 3 0#9 1 16#518 1284 . 00 6.336 4 1
2 w j ovoo 0•2 - - 26t6 6j -J^,767 12 ^ o .Z Z
6,173 -, 43, 89 0 1 4 71^
-0148*is 9, 8 ,000 Q-02 '023 ,9199 439, 0 , 3 5 ,12 qs z8 60774.
36 9, :L7 IF 0 1, 307 -6 ' 00 0*02 10 1:91416 it : , .7 * Jt 9, 3V,20 oi ibU 0,83 13'5f 02 5 w4too 4i65443 009 w 1 4 i 392 10: 0 1 ' 67 . ,11303 7 * 507 24469.
6 ' " 000 2 9#476 19141 -1:55#,58 -1:55#,58 88•i5 7.537 00, 9 2 ' 08 *78 9 owoz W -1154--99 7 0#00 40588 86901 14,77 67.49 76529 5, 1 vac 2000 0 Q-'Q btai
8 2 84 1 600 "YZ500
24,996 ''149 91 8,501 50,983 7*01 v o 9 rl 4 7' ovoo le ts'• 10 10 . 6 6 00 4 0^7 + 80672 *6051.
7,08 *9- 2 0 1 ' 0 l X139' 84100 0,02 '17#6a6 9.002: *14.51 50 ^ii 47 4 7 IiOg: 0 CQR ?I t i al : 6+206. a 114U,#,56 12 10000 90704 48#52 51 7,688 26oJ95 loo630 i2000 002 w1802 "1346,58 13 49938 6#7S4 OF POOR QUAL17 Y A-2 0 0 VOUGHT LOW EED wINU TUNNEL 'TEST 630 SP .DE^ ,, TA DATA a tR.UN X.AAMRIIM A S / i.hl7` • 11^20/^i 1438 F :.ktMCVED WIND AXES (BATA ULL SCALE DATA SUPPORT TARES ALPHA PSI PNT - L /Q 6/0 SUR 104/9 Yt110 - 0 0 '' 0 24 4 00 9.631 90.22 414;83 1 07 31 4844 x! 1.14,35 ml 50.905 1 1 9, •0407:-22 4: 7 , 021 28.229 x85 .11$`.65 0 0 4.67 -45.775 19 a98-30 : 2;3,, 96 3 -0 : 0 07 '"304,00 4 w' 8 75 25x070 2446.7 -*,l#OV .Qr07, • 1 g 3,521 69• 22.228 33.52'36.•066 23 r0S 22 +00 40,7 r 1 . 6 : o093 f 21..12 ^! s fl03 - 19,561 4 ` 364,61 .
b6 -:i1s139 -144Q 2+113 ..0.07 60.64 15 . , 26 8426 16,941 P26.435 ti ,+0.f1T rl r-.^ 1 17110 1G^ ^t).Q 52 "n'p.QA9 i5.22 16s.26 8 X0.07 10. 00 1+017 1:9 45 039'*.96 15.057 60037-,1'7,893 .: 408,,00 -0.07 9 1k4340 X7.38 in0s 'f15 71 o . 84 ~124198 -69 *;72 w 6 .
i0 .0407 .., r s644 & , 0Q • + 196 13•'918 77480 2u«73. I •514e21.
'1 i i . .0.07 * m 4.00 - . :6KA '_8ol 31% . Al5mm -'. .Af 71 2': .7^r ` -!112;t39' 12 00*07 2#0 ..1..6 1274.35 13.543 86.'23 ()+4.44 .24•:12 Q 26 13 "0.07 "1, ' 0`00 85.53 32..41. *'142x91 134705 44307 .446 "1535 14 2.00 ,,3.26 -1434:99 00 0 0 7 13 * 913 85.10 9#340 4400 -00999 15 0 0307 144311 74053 1,.44.028 ;. Z* 79" =1E,Gi01 "0.07 , t a 6• , 6505 33.07 !*2X11`«88 26 O p - 004 93 144730 159.21,6' 17 9.00007 aWOO '0 66. 5.437 3f.5S X216:.45 253.501 50+7 •,235,37 .
0 104OQ 3%.•24 18 10 i0 7 1',965 34.96 2!84333 16*578 12. 38.96 r-2604:311 19 - 0 .07 00 344 46 174817 24.26 3;1.945 "0407 447 0 94372 3/.61 0285,,53 20 14400 x 3 .632 ,.^ 6 4 40 14•_23 .
_.' 37 * 45 .-303.33 200964 4,'1.758 21 -0 1` 0 7 1 60, 00 5W8 0 22 6.476 • '42.20 - 33.1*83 -0 . 07. 1$*M . 2:83 -6. 0 46041 6 44:_015 .4365.'68 23 -0 0 07. 2000 7*420 25s876 Il i 2.s 29 610216 8.037 -0407. 22.90 45479 m396*36 24 284511 -26,01 $15{785 43,.32 -416412 26 -0 0 47 24•-QQ 314639 -37.88 ' 6Oo799 943 40 s t.^
ORIGItIAL P.-u- .V E 0
OF POOR QUALITY 2^-2.01 , LOW S P VbUGHT EED: WIND TIJNNF-L TP-ST .DES TA DATA 060342 7.505 43•32 "122*06 i !12o00 09'02 "163 96 30940 o 2 *i0000 0 902 I W S 0 1 +151 6*992 R 150•;53 3,618 3101 Oi13•,28 i als# 6*6*6 to() 00, 3 r ^ 0135954 3o 4,54 2.60 ' 17 "W' % 23 `" 4 '87 w 06 ; VO() O•02 -11 . 8 00, '*'R3 38 264 , 7 3s632. a 4t ilfi lr oo w U W, 0 2 '20sis 6 -2#00 5#626 86w8 50459 16•,35 45 99 0 -Koz - W E 0 0,65 5 # 394 -75032 5.829 ilt ,* *`15U r97 "loiag 8 01-02 6#032 -60oga 5 , 64 6* 000 ,.46 .
00 2 8k 4000 0402 - 0 . 0837 073: 16 0 , 1.
0 00$' 0064 . 4''7 ' 54166 tli 022 • 32045: gi0o, J+0802 :."16 M.436410.
1'466 10900 4#969 m16o. 84 m 137+'07 ie - Qw O2 2.273 -00 ; 53 6w127 otoz 30092 13 12900 591.63 16#09 6*08 .-21*2 3 "139 0,03 .
\^uvU^'a^^J1§L :1:^ il'^J`'.-ice ^( J A-2 02 — r VOUAKT LOW SP EED WIND TUNNEL 'TEST, 630 •o^'^TA DATA (RUN it.1.11 10e -RUN 1•'p0 s/20^81 143s WIND AXES DATA FULL » PA TA, SUFF8R7` TARES kt^hBy^U ALPHA PSI: 1./Q D/0 YM/Q PNJ PM/A 9F/0 K1, 1,6484 04!03 o"6 930S 34436 1 w12 6 00 79772 m 16614'36 + 34275 -50479 2 m10+O q 0.W03 7+253 ot526.06 2#71, -4 2* *. 52 *107+61 -8*0U -,.
'00825 1.9.50 "100*05 3 0scQ3 6.784 w 135c13 20446 06.00.
0.w,03 4 0 384 4 16.;1,8 .m103967 6.332 -10024 24703 03.60 5 0 *4a00 >0:03 x«928 *1.03441. 346.25 11,40 -(1259-14 .
,.10734,73 m208$1, "2.00 00.03 5.674 *88425 11}22 54040 ^^^ t1y^a 0900 003 7 Bo 496 7 "759 76 7^°^ G oil 0 a ► 47Y s 8 2000 0443 "1#- 060 3405 59175 60+34 5+630 01489,80 r.
4400 "0.1907 9 0«03 4K899 — 45937`. •' .c5 1.41..87 5 'g 6.9'4: :0 •oo o:•.o3 0 . 71$ w*/- *81 14137..0, 0734 - 11.0,: 54600 8.00: 0«Q3 : *10.!19 1+5^7'_ 4.802 ^1b•64 5+564.; w136931 0000 0*IQ3 2436,8
2 49935 -0420 04 16al1 094384,76
5+672 09,03 13 12000 5#065 0141041 17438 54684 0 17•, 15 30140 a .9 ^.
f z atl ORIGRIAL PA""""' 131 0 3 OF POOR QUALITY YOUQHT LOW SPEED WIND TUNNEL. TEST 630 - .PE^ TA DATA a .—.T. _ _ Ica:. ^a o 1 ^^
0 (RUN _109 - 10) /
RUN 1. QO 11(2(7,/$`1 ^,k°38 WIND AXES DATA FULL SCALE DATA SUPPORT TARES .htLMf 5YED -PSI L/9 PNT ALPHA D/Gi . PM/r, RM/12 YM/0
sp a
.6#,470 1)o 0#03 .g 0{r90 1 7i6O "163.57 2#062 319-70 wi0#00 0 "5.579 X9 2 0-03 7.2:22 -151.80 25.25 0.67 1#942 -M.g81
3 ess000 043
.•96011 60845 - X . 1^*Z3 135.88 1 #741 4 , =6900 0 * 03 435 4 -92 51 6 419 *11098 2 076 1605 IM 5' 0.,03' _ X3.6.38 6+068 _ 4900 -102.$57 2.78b 52 55 0106«38 .
06,03 020864 m2 # O0 6 59785 87 x 2 3 1,'_1 78 30495 12., OoJO 0 '^%v ¢1 `^' 'u c 5#532 X12?
42563 86,64 9#:42 00 043 q3 8 20 w i 5±036 w 58.^95 209 1 ^1 85 #0 79 4.692 2 * ^^ g g 9 •^^: ^^ ^ + 160 000 •4VFJ ~ 1G 5.169 43.98 4#877 I 0.*0 ' ,„27.52 .Q 6 0.03 0.74:7` 4.835 •21 x12.0• 9 10 #03' }0 1 #5 95 , 1 R^93 : ^ X12«5 5.22 ^IJ2L, I.
+ 4 ^! 11rOb 10-00 U%103 2#,468 5#069 3#47 P!1?13'.:10 12 56386 0 1,bs, 49 30297 5#363 1.3 12#00 0c0;4 16#62 wi803 "13t!937 5#559 R C c 1^ A-μ2 Q 4' OF P C, t^p ()F POOR QUALITY A-2 Q5.
^ y- 1111 YOUGHT LOW SPEED WIND TUNNEL TEST 630 .DELTA DATA a ,(RUN Ili-R'UN 1011 100 11/20 1 1438
/8
n A74 9 pATA: sllPPeRT TARE S , KECfCiYC —— WIND ULL SCALD DATA L/fit ALPHA PSI 0/Q PM/Q Res/W 1`M/Gt
PVT SP / 0
.00 0vQ3 " 24+0 431 0#669 36.51 =-87•:62 1 • 12 0 17 5 91. 11 0 *70 L 0«03 -96x98 2 "10#00 0 21+346 w 31.65 10#580 160c34 Y.280 r .. 43.198 0 + ^3i• g -1015,K*3 1. 8• :C? *652 2,#573 27.21 b • 00 0 03 16 +"3 0`2#24 -^122&76 '° 38 81990 -123*0S 4w31C `: 5 "144,t al -4900 Q«03 89633 *, 104..96 6,196 16.77 #1419;83 -145987 - *00 U•,U3 -11:+287 6 2 8#365 -82096 7#019 1U#'69 -0+00 0143 81329 *9220 - i4e*t52 7 '8+165 0 74o7i. 7#062 9 21.00 0 nfl3 -5.25 8.366 .^54. 1. a 7. t 0f! 135, 48 - # 04 $6 4.00 • 9 0 8.395 -1 13 31 `36 0.68 6a.935 s w 7-99 0 . 499 !18879 1p b • 00' 0409 &•569 - 1r9,&25' 6 , 6 1 -13«48.
8,00 0003 1 31500 -15&12 r!122a80 1.1 8*ROR x+!0.37 6f9399 o _ r L J uC^! 1 L P u4Sv ^ 7 vauaHT LOW D :WINO FUNNEL SPEE TEST 630 -DE^TA DATA e I I 1D^N0^ 112 tRWN lit RUN iCY/ .1-00 11/20/81 1438 6A,TA AXES •F4LL SCALE TARES' .tit MOVED"' WIND DATA. SUPPORT - D/0:, PSI _ L/W.
PNT, ALPHA PM/0 SF/Gi R.M/ Q ` YM/9 . 0 * 06 1 . 412too 35#-90 Nig3987 a 21+193 10+708 -1759.22 29839 010#00 Orgy 0 ^18f04 99820 x N107«19 2 +167.88 2,619 29#-35 0.00 3 -8r0 0 -4w* 758 w 1*4#10 23 4, 5 5 9'+011 51 29429 6s0Q p 0005 8114467 P^120ISO 84, 450 ^123a.50 3.393 1 2A#40,, -000 ..
5 0"-05 7.864 — . 16 s 91 yi2^'.^73 ' 2 0277 ' 0 110 o, '38 4, * 874 ^.
.2900 "14yv2Z 09,06 6 -696Q2 7«629 -91#-52 124.28 69514 7 0000 ^i45:,:ro 09,055 7#529 -3 0 465 x 73 90 5 7 +293 59VQ 0905 •06502 02.38 8 2.00 w64991 *1391 7+713 7+573 21 5 4.0o 0 413'pep2 05 St275 7 .5 29 -35*74 7 #-737 *1.50 ,10 6400 0+05 1;6.:68;° ^X2'a044 p• 597 8!236 7r5'+2T ^1^ 73 8toD D«p5 l rO^M .^121'*4a
11 6• T4 8 35 0• 7 6#-78'5 "#-
10900 Ow05 99898 12 9#100 1891,9 -22927 -116151 69391 09.05 .12,452 99963 -113"t31 13 12 4 00 37w83 6#-150 :-22x84'
om^lma: PAC.."5 9
A - 2 a7 OF POOR QbALI Y 6r VOU GHT LOW SPr h WTND TUNtdEL TEST 63 i .DELTA RATA 11 3 10%00 (RUN 1 1 10 3-RUN 1.438 AXES DATA FULk',} $GAL W11N ! , E QATA SOPPQRT TARE3:.KE.MCVECJ ,rM/Q ALPHA / Gi ANT PSI L ^/Q PM / D SE/Q R'mIQ 2t00 09.04 -+37.7 10 ' " 1 16942a 1 86 74 a y * 63 X11,2*65 3to42 00•06 2 A1o.0o -36 0'5 9a 13.031 124.21 2*465 32.58 -107«2.4 498.00 '0«0 `*883 3 lZ*285 "118 4304,58 3.01.0 24.00 %20 ..6:00 -0s,02 1 A 2$0138 10 0 054 115*27 40090 i9rZ5';%^iad%35 r44 - 5 w 00 "' 22.6 15 9x203 t* 30 0% 0-1 906:43 5.524' wi461021.
6 ,29010 n -169584 09,01 84,491 64 9.36 1v9lo 19150.00 i -d = 'f 4 n., 1— 0 a B 1 LTL V ^^U r 147 7* 7 ^& A VW 4y, 7-,494
Vi c * ^v 0 4.97
- 8 2900 046 05 9970 80200 *136.9.4 23969 Ua 49 7o573 ?_4w "R A•74 o *000 82.59 9.75 7.x1.68 x%.44 `134*26 0.:06 , 24674 10 6*00 8*438 °1x49 -ti.76 .41.26*75 6.826 0.:¢6 8tg0 7.0.79 ii & x 835 1sr238'' .*13.56' x!120. 17 _ ^^^ ^^ h^ 1 ^ ^U dk 1e-i YJ A-2.0 8 (RUN 114 10 RUN 10)/ %o,00 .
^ir2ofai 148a WINQ AXES. DATA FULLISCALE DATA SUPPORT:TARES *EMOYEn ;PSI T L /Q. YM/0' PN.T ALPHA o/A PM/Q SF l Q R:M/C 00Q1 038.0 Nt126t*?- M12!0p 96F1 40..62 1 01 iS I 446 8 3093Q Ali0000 36.'27 X114•+.16 0.01 5 *q 38+2 130116 154sPO 2,769 ^61 3 wa«oo 040t 05 $ -ia6+ + 48 b2:r . 65 3^37^F 44 i1 : p •6o0o d(Usg7 > i44 A31 C'40 155+39 41921 - ` 3a + 792 iQt120 04^woo 00ot , '"'4 . 750 15.51 -154+83 5 9.248 '128+94 6:t26Q 94162436 6 -2+00 0•.01 -19+009 8+720 96•, 46 12•, 0 5 7.767 I •. n_nn OrAA -1?aAc 5tA3F.l, 6 9.,53 7 ,,...,, 7.x75 -156.05 ,,,, 6f19 --.J 8 1100 0401 8«234 46.99 76926 w1.41 -148+,09 -7'47Q 2v8 9 4 0 « 8 . 299 7069 ,7r53 - i4 7 .0 0 0.1 - 34 001 27+94 ^r
^ a a^ o ' ► 2 & +^i34°^63
6 x:.. 943 1+ 8+411 11 49 x
^t$ 7A ¢y n aQ+. 1 4 1 1 'K.A Of A,. _i!'.'.:: .C^}Y{/. . 8t.^:33 ::-v.:l-R ^i,6..
; . ..i1 .- !:6599 AQVQ 11A315 w 1 0000 9 @2U. 0 X1,26+.38 12 0*0 1 -7+30 6 *75 6 1' ,404 15^, 8g4 12100 O•.p1 -131,98 :-2028 x!122%36 13 10x268 6,216 r `NI L ?:^ n'^ Y y^id F^ _ -^^^ off' r - VOUGHT LOW WIND TUNNEL .S PEED 'TEST 630 1C %I •OI;-L,'TA DATA r IL^^KS, i•15 (RUN 1S • Ry^V to)/ 4000 11/23/8 0g^8 A LL DATA WIND Ax SCALE SUPPORT TARE8.KJEM0VhU P61 . L./0 _ p/fit PNT ALPHA PM /0 : RBI/0 YM/0 SF/0 •0,,0p "38 Yi2 , 00 41«66 !i23*,g9 1 1 9 84,0 } 471 106, • 3,843
15 '23
0,:00 *380 2 ' 10 • '00 "122 • 148.90 35••55 -116, it i3+334 2.903 - as "B OU0 . 1574, 60 - 43.
3 S 65 3.264 26,, 94 11* 6#00 *29.860 w 139 t=6d 4 0 0#09 145,v82 4-.690 10 o 399` 21 r43 S -4t00 0wOO X24.84? w155« 90403 ;1250.68 6.297' 15.:12 13 - "2#00 6 *161,36' " w 8.794 93977 11,>16 Q9 QQ @5 43 7+726 0 00 65y. 6 7 Wives I'+rte.--3ca w- 7,795 4w96 n154*70 8 vg1«84 2,00 0*00 "7+ 5 37 +400 440 *146s;So 8 08 7*800 -2 • 9 4x00 r,Q g *530 23.28 0 12u1Q 141.8a$6 71 7,441 0•_0Q 8,668 .112,57 0021,955.
1:0 6 . 00 t o l96 7+92 7,33Q 00,00 l i 8. 00 • -3 wo.g.. 6 # 932 . P *16 t 4 9 :412,7 r52 ' 6. 679 8 . 969 ..
.c13 - 8 &i4 12 10+00 0.
1 . + -11c(6 1+3 905-97 6 x625 $1a51 09 41 1 6,1 :w21.66 12 0 00 -0 *•00 ^1239,2?.
13 10+430 "14,90 6,350 '5 4 P S u u H A-210 r VO OT LOW EED WIND TUNNEL TEST 630 SP Q E'^'TA DATA _ '101NO. 116 k t,) RWN 116- O RU14 0
10 t 00
ll123/sj 0 818 WIND AXES DATA FUL L SCALE DATA SUPPQRT .TAEtE6 :REM VED -PSZ 1./G D/O YM/9
PNT _ ALPHA Phi / Q 8F/Q :> Rat/4'
00,00 60 475 87 111le07 0'12000 70f;99 38 0 1 '"3 15 # 451 2,871 29 x4 "1000.94 !+-10 ; 00 0*00 -4 33 .+362 19t686 85.24 0 ?_ 2• '09 a 0.4. ii2fi 9 1t- .12«033 qiti6r59 a, :':229 94«15 28164 ^6t00 , 93061 20«88 X125.80 o w oo 0 25 $74 100650 3651 • 21;1318, Os00: y 977 9a 5 • 4800 79+27 *gS A . 160 49 9*331 6 0 I m 2 . 0 80527 "148%03 0, 04 011602 51 62,88 64406 124.12 0000 0#040 "100756 55.62 w l4* h13 7 84195 41050 60 942 1 c 'N.nn h -a:. 71'. n_na^, lx nn _rn. ti -A _An ^4']7_L^ v' 1 w .^ - • MT V U 4 ! x 1 j ^ ! ^ - ^ ' .
*00 . '000' M 72,: 8#325 x7 0.62 *1331w2 2 9 80'62 7016.7 .
2.i4Q 60.Q0 0^0Q a«'4}8 *+12«, 7 ^csav9' 10 • 2x29 7.09i x0100 .
E #woo
# $02 - 900 1 446042. -119F79'
i1.:' 6o 62,6 ' 8 60^s2 _ 0400 10 , 823
j 12 10 4 00 9.293 08019 x"19.95 X1160.20
.14 , 3$3 «0v •, 19W57 X115:028 a^ 13 12 t•OQ 10 9 268 N4t86 51,916 aI VOUGHT LOW SPEED WIND TUNNEL TEST 630 QELTA i DATA t R Nd.
1.17 ( RUN i 10)/ 1. 0n ll-RUN ^?-a/81 ^.
WIND ^" AXES' ` OATA ARES .REM(IVED I^LI. SALE DATA SUPPORT T r ALPHA P31 L/Q /Gi Y'M/0 PNT PM/q SF /Q ► RhVQ 0 0+01 0 39 0 15.821 .tE29051 42.;82 -4122-K33 1 "J2 00 968 3.631 2 43 60235 3 33-35 .115'0,30 m10r00 0.01 1 1e,53 14.101 2.9222 QtOt -8100 `433 519 3 12f343 3.0 218..41 , 0!1200103 140 1 ! , 79 X6.00 .
Okoff, -097.70.3 1,1;.084 x,134.
:' 22&28 1
'421 i 75 4.,.1! ► 0 x.4.00 0601 1.0096^ 170 . 01 -1X15085 "2 2•1 1!4 ,431 5.424 9-1 4} -2000 04. "16.1$8 -152t*6 0 2 9.487 6 14x34 17 6+744 7 0 •,QS 8607 4 150 v42 0000 w l O o 783 8075) 4,2t 67 74356 2000 U•,53.4i43. 5g 8 0.01 `"5 9.000 26.54 7.566 • $7Q .
9 0... .. .M _ •640: 111138 x:32 1 9+099- i.'1:.+.51 +640 OF 'w,4 L - ^' . L. J /S w I4 N: • A k Y. ^ .^ na ^ r .. . ^ r .^ ^. :: r. '.1 A' .—:. 1` h' rti ` `. N r M"SAM:.' w. ^vp !l .. y. w ^r. ..s v.iV iW; —AG^oV .- "(Q 7.^wVT „p0 iC.34sa •x U 0 ..6 1.6.43 ^1"cf$ $O0a, • 01 « 655: 9^53^t 8 6a5,,,1) :` •m!ZIa,28 1,2 1o # Qo 04 Q1 l -IS0 10#00* -10.73 6 * 757 "11229:62 a .00 • 0110 15.295 . 0 21 1.82 1^i2002 13 i2 10+930 -17& , 25 6.4V F I y s A-212 UIW YOU 1 WIND TUNNEL TEST 630 3HT SPEED LTA DATA - L)E 5,94 39 9,60 •0040 74 97 1 "0- 0 8 - 2 4 @! QQ 30 0 078 24*17 w 43434* • 100;08: • 22 +-00 2 -1 4 181 26+ 759 -m380674 i 3* w29 57 0 4 24@41 6 .
4'. I WO a 08 fo is 0 ( ) o ,i w 5 . o2eq 2 1.693 36* 90 . 1 30 0 t 63 290,32 w.« • <06 9' 675 24,.02 5 "0 4 09 .1 16 , vo0 19 , 608 4048 5.'7=23 85 - 2 6 m 0 4- 08 . - 1 * 9, 00 17s230 20 0 ,15 :-22- *^33 -- 893 07 63#,64 o 21 o 027 11.4 - n ft 4 4 1.
- r% ,L 4. Q 7 -0 6 08 i w 1 . 2oQO 121 %3' 16 v f IQ 6 0 4 ^ Q - a A - f f - 7 1 - 040008 -iosoc - 94940 o 18 S:B S -68 +;E3 15 813 65•7 w 12#258 .Q a, QS S 9 :3,5 i 5,08 , t4#874 70.47 -7 18, 12 '^ 9 M O•OS -61 i oo 458 i 26- "?1'.1 • 70 15 1:Q a11. .14 r82. • 2, b 5 76 -1,184 , 10 2 9 *1300.62 11 -0 .00 9 - 4 iW-1;0 '8 13 144307 s 69.38 06037, $ "Olos R 1,0 c036 210!53 M136.199 M00 1 4 4 #331 65,58 2+98 2 "0 0 08 0 @, 00 59*25 2806 - m 13 4 ' ti 0 3 13 - 9+ 1 81 14 +819 44789 MOSOB 20,00 " 8i5 96 14 144370 67987 74470 24*58 •!1231'99 115 '*0,0, 0 ' 4 8. . : 40 8, • 8 . 3 1 56 12 6. 53*94 , 1. 0 *: 6 3 4 - , 22*42 !o f 146 q90 ' 1,, 74 1, 6- 1 * 0 i 0 8 6#00 'l w 7 0 *9 9^} 116?697 3: 57 54048E 45, 6 055 2 - '07 s0 :08' a woo J60025 46.3,9 2.•' 6 *157'9,63 1'7 8 361 P.6407 18 ; U - -08 - 10 A VY - - b - t Z 66 16-927 38w6Z 21410 1*17?477 19 'MO 9- 0 a - iacoO 260,38 •19+C53 284,48 264843 7 - 543 92 17 . 970 20 1 - 0 * 0 8 144oQ -o o , 4 50 19#331 *4 27 * 54 17010 29#900 0 223 }94 1 . -1 6 i Q0 2 1 ik*6: ^ , 2 6#. 1 5 w q S Z *8 T 2 1 S 9 6 7 : . 3ko-, 72 8 pi 2.7z «26 w O:fOi 635 U -v25 24 6:4,2 1 • 1 21 28 0 248 12 t Z A 2 48*386 L w 4 0 ' 25 -0908. 24,40 -2-771 020,08 504819 1002 *291k97 30 # 754 or. Pool" A-213 LeW ,SPFED WIND YOUGHT TUNNEL TEST 630 DATA DELTA .(RUN 11!3 wRU N 1* 00 6 1 1'1/`23181 _.
DATA F?`6. .R4116,YED WIND .AX DATA SUPPeRT TARES - PS 'I LoN D/Q PNT ALPHA PM/G SF/GI RM/Q Y M / G i w O -08 :-24 6,0 9 30t464 5603 78i27 28#20 -144 9 21,9 2 -0 , * . 08 - :m22toO --4,777 -38,594 38*69 58': * i 260882 2903 ^ 1 14 i(3 3 3 07V#-686 Z3 s 923 33 44 3 - : 34 • 78 2 -3 * 4. :00 0 '08 "18*00 ' ot*73c 3 9 9 , 5 5 2:3':88 8 21026 340W m31 * , 231 „ 7 , 0 , 8.
5 -090$ -164 , 00 M0025 19 • -k88 48'#43 mi 25 o 693 , 304,01 6 - 14 65922 * 2 8 * 7 2 :0 0 08 a -' 6 - Q - - 5 9 0 ,37 16*567 =20*9RE 41 + ! 13 : OPOS m j?cOo w 9*'61e 7 160459 579•02 o 17s1.E4 249,08 -'490 , 29 .
10« v 8 "1 - 900 183 156508 63*.36 wi2 * 262 i yf 94 'e d 75-%15 0 0 -1, Q #L5 G a '- a • 9, "OO' 53. t*#642 . 69021 -61865 .
-Sao .6 , -O i o# 6 0 i I S 7 3 5*74 -2#877 2U'098 ^" 4 *69 J, 'j**00 • 0 » -10,719 23«$6. '13 6).8 14"1:28 6 . 8#05 1 *0 f CI P. 'M1; 3 9* 12 -0 .008 -20. , 00 M1U•1 20 1 101*3w00 4 6 2 89 65661 3o373 ? - '4t77 13 08 6 ovoo w 9 o ' 54g 59, 3 , z 00 0 31 *,43 -146*65 4!52, 14 + 548 5#271 J* -0008 '2000 -84855 140759 566125 7-E 5 48 26v-04 *133•140 2,+•61 .0+137970 -70 5 9 ••85 jo.s.555 L ^i* 1 1 r,V %f w - - a
.4 sw A, w - , ' k f It
;wc -WG .-T r -. C -W • 0 q w i f
32V19 I &5L 4 1 4 3851' 17 -0* 0 8 *00 "1 : 42&56 18,385 1, 18 -69 00 199660 -0608 10'QQ a 833 326'82 80 1,6 2ia970 3-40.14 19 0 0 # 0 8 129 - 00 " 5 32•,00 V , 19 6367 196,35 26,965 0 21* 17 0 801 * 144 00 s 20 -0 0 08 - mm * 6 3 49 18 516 51•65 309181 3! 47 360,5'6 2 J^L 008 _$, 3 4 w2 6 0f82 35.0 I IS' * 0 To, 9 5 - 2 L, 0 - 8 7 1 0 q , 22 29 # ; go 36x 49 22. -0 6 08 1990Q 8 3, 1 22 W380 .35#890, - 0 291 '6 *7 "11690 M o.j C 8 2 0, O Q t p q 2 -17 + $ 3 1 ; L 23 kS #063 3 d 75 0409 2 79 1 QQ . 3 6 .91 ;2 7. q ^56 2 -18-19 4 9-917 25 et31 4278#01 13*77 49*886 :0@08. 24 ',O Q '0492 17 30 ,8 14 A--214 ': SPE;D WINO TUNNE I VaUGHT Lee 'TEST 630 - U t4TA DATA 1P O N156 i?,U - (R UN I. O Q w RUN 1,01/ F4LL DATA RESMCVED , Hk^ W 1 NO AXSS SCALE , DATA SUPP5RT U ALPHA ;PSI ^/Q 0/0 PMJQ YM/Q PNT 0 RM/Q 002 "26m370 -d2000 jQ•JQ^ 6jr94 4187*08 I -144o20 35 o 737 0 - .02 i 25 o 2Sig 2 "io i oo 140446 -147,, 50 iOoVi 53917 23 i :! #'7 3 08000 t 0 - jt!^Skw 4 1. * .9,1 *+272«45 7Z*45 •:0a 0*455 -146t.92 R58°: IQ 0,9 (1 -145 # . 109246 33 12 .503 89 .
' s -4 4 00 , ,• 1 8 * x : ' 0 2i A2 . 64 - 35 2 4 P , ,7 8 : 43 11 . 7`62 9*796 : •.2 000 QN. 1404 "199« 6 rc il#173 92# 90 58 . 46 04 17*58 ^— M AQ -to ;RAt A 0 e Of _66_., 1 4 v 11%32 A 1 3 1 17 7 -60a as5sa .$ 2 , 00 0 oU 7 4 6 4 3 0 3 x 7 7 - ! I27w69 2 6 7 8 1 80247 9---A Q: 3: r 99 9 4i 0 k o f 'it 71 22+ 00 6 00 01,09 ^- O - v 63 2 1•. 2** 5 2 i4 00 $a 8 0 037' -Q 1: .
2,60 3 .39 a•00.' 0a 9 . 702 --ig 4 7#864 it 8 0 a Qa 19;,*2 "1320,63 1 2 10 6 00 4^ 9# 669 — 43 0 7s891 • OcQ2 ."22w63 *I35q27 13 iZOOO 9 008 . 69480 10O882 7#649 .
lK ail r ^ ^ ^i POOP, O P SP VOUGHT LeW EED WIND TUNNEL:TEST 630 DE[ TA DATA j OoNdw 121 =-RUN 1111-RUN 1Q}/- i•00 : 11./ 8 23/81 081 r z D WIND AX€I L... SCALE SUFPDRT TARES >REMOVEID DATA j , d ALPHA P$l 14/0, D/0 ,t4 t Q YM/Gf PNT F/1^ Fr i/ . „ i "i2t00 04;00 A 26.943 1,6+138 t t3' 8 101065 68oU? -19304 too 2 010 0..00 "2$#484 14o383 1 v,a v 09 104354 524,19 - q 185 89 _.
Q . * 1 j 81 x+174:«03 o 0o + .
3 ' 4"7.59 1C s49K 69 13 . 53 boiC}o t »o woo *21.:. 17 i2^4#32 10.2 7: r 1^9fi ^]6i4'99 ^F a4xr , 1-3 494 . 08 0*00 "is: -aa4'8_ _lit, 765 .:1:23.56 23 'x 75 •152"!kl65 94508 6• 2.00 04-00 • 14i3 41,55 934 9.269 17 05 ...*+139 X84 69 11 71 0*00 • 5:0+83 } 10+686 R4^^7 1OC62 "1314,Ro 0400 66.57 0400 " 2 0 00 2.59 X126.-49 8 *244 10+239 43151 8 ;7'7 g X4«9'3= X126".19 7,9 936 21x61 br"QQ ^1'C^.r34, A^i28`14 t0 QrtR 7lS4 9 . 8x3 7"^53 1•«^51 2 'SE4 4.ik0 ^5,29,98 8.0 0 p. t4Q S*753 rt19*19 7.783` • 90 ;;1d4,36 12 10+00 4>00 0207 94773 - 43.67 7.799 :`2U ► 13 12.00 -0000 9+921, 10.148 ' 013700 • 70,18 7+202 :*21., 05 0 F P C S) P, VOUGHT LOW 630 P E9D )41ND TQNN5L TEST T UE A DATA tRUN 122-RUN 10)/ 1000 - WIND AXES PATA -7FUL SUPPORT TARES.HEM0,YED ^GA.LE DATA PNT--, ALPHA ;PSI Le g 0/0 Phi/0 8 F /,Q Km/Q YM/G *12#00 54 0;50 o1*20-98 004 * 39# 744 18#76* .117#61 6 .
1,4' '126 04 *u"01 -1*2%13 P- -4 1Q 00 0 0 - Ot '435 -490 17 o 176 6+ C19'.8 too 6q4^46 33s , 59 - 6 145*21 3 so $ ' 1/ 0106 19-715 129.23 484,62 -147*34 120 # 98 7• . C)74 fs O V 4 f 00' 000 1 , 96491 a r, U 0 4 9 3 776 - 1 4 8 %, 6 a -7,1106 0 C ) I * 6,50 6 "2*00 • 1 13 239 -148*34 71w9 1 $, q ,635 9 ", a 1 9 0, 0 a 1 ' m i C ;^ 6439 M$42V39 4 85 *4 90 U; ^ 4
7 0 0 00 0
-6,, mu 1.46 8 2•00 0 12#700 39938 a 4,966 1+135•!69 y131Fib 9 - W0 0 0 5 1 9-2 8 9 49 61*2 It 3.
0. 0 , 401 2 9.0 -- R 1A71 % 2I 039 14 0 i 1#893 4 GN 13 09 b v30 "122tn 11 8100 7&034 13*500 3rap- 8#320 IM A 12 10000 1988 894 . 22 . 00 23 *28 IRU 0'57 0 t 0 1 ^ -o 3 07 14 #0 04 14# 1 3 12* 0 0 0++01 5 4 6 2 850 049 7+584
, 99 : 0 2 0 #. . 9 2 1 V9 *, 3 - 9
(RUN 123'-R"J*N
1114$181 0818
- ^S DATA TA Y.IND AX SL:Ppj PST L/W On PNT ALPHA O*Qj w S #6JS jSi4l+j 1164E13 6.4612 5J o,43 '"146o 66 *12 00 6403" 4. #37 0141oi2 2 "lo t oo 0401 w3540 92 17 1 2dS 122 ^22 —o rl ^f 1, 04 9 6 6 50 , ^ Z^ d #!^6 To ;d ro 11 Q 1 150730 t Za 4 7 5 l 00 w 27 ' -, 6. 0 4. 0 - O i 6,1, , 3 120, # 68 6a 2??$ # U7 - 1 * $ 6 V al: ^u #,66., - 1+ # 6? 0 , OoOl -^ , i 75p - 1 '4 ^i 1 50 9K 0 0 4, a 4 1 7 I ^ f Z2 —@ 72#23 Em 1 2 j ^^7 97 14 1 7
u'Ql &A 1006ac
7 -0 10 0 '. 11 7aA-, ^ A wo P * i - 9 117 T F01 ^ ^i 4 10 600+ - U*P i 2 6 1,4, 13; 66 1$ 073 71.03 cis O t S 7 I q 8 is 5^ 4 5, 12 14-00 2 kl 11 0 0 14 15 — C 0469 P; 41$1 00 74 4 13 12 0 0# C, 6 w 22112 w1l94,7,9 as 140926 7#475 Is 4e Clo ll FO_ P, '.
vG.,UQwT 4 * C1W ;sFErD WIND TUNNEL. TEST * • 63 0.
.
1`A DATA F- IV a:x^ ^ i ^ ^ ^6^• 1 g^1t+FtEl^6;' y Ya^Df 1i«QQ x1^23/8i 0818 .
.
Ct'4TA"' }iIN nt, H i n A AL2 9uppdRF ,TAR S ;R^PtQVE^ Rkf i AL / VrQx iR ^Q. ^4Mfa ^ I^Q F 1 «+12900 • O;v1` 5'4 9 4161«89 -34.995 17 4148 :125#x48 X#683 1
2 •1u400 •001 !31 +603 35W441 125 @,94 6.867 - 43.98 41521;32
t '41 l4i: t3 2 t1 ` 1+^G «96 ,. i v86! .6x92 sib
4 «^6sl74 #ups 2 ' 3:3s3i>
2 ` ^f139I t2T 27 ` be^5 a. 3 i5 '^^ll '-^T : ^kk g 97. .3/6 ':'23^45.".^iddY., r4 0QQi . 01937"- 1Q.2«k5 7f " r 18095 x+162089 • 6 0 2 0 0 0 0 4! 0p 0 14 60 10.357 8.583 72#10 7 w0900 -0#OL °-9+751 470.83 9#326 1U * 06 @R160vil0 9 x 797 8 24.00 •0001 • "'4' ; 958 94594 31 *06 90493 1#.52 ^151'^s2a' ..
•.
:. .. ::^. z; s s> ' , ^.
4 :h 86t;;:: ^^ y i z . ^'^"' 1 1< :.K$'6 ^r53,3 . ` ^^ 1Q^^xQ t"'3l^^,25.> ;;52 =325 r. 9e.04 ^63s5i!tiYl2:< ^' 8 00 M.^ x.222 .lot to* ' . se` na :' 11' .., :7 `r 2ir .vi.0' 116 78 ___ q 1039 ^` 12 0 #179 10^ 58 ^9«14 To-965 : 0 23 y 5 @1 13 12 00 0401 16i129 .11 4 976 -18x12 6*086 : w21*66• -!S`25 N53 ij xi 4 e, • vauaiir ow g f*M, W II ND TUNNEL : - rEST 630 -DELTA DATA 1avN*w 74 .74- O RUN !32) 1 1 Od., , R3/81 1,303 :ri/ WIND AXES UArki CORRECTED AMEZ D*rx-ca gp icm. SINGl • g ISUPPORT 04TA
"Li/1i. YM/ 0
A6PH*.' PS I On "PH/12 arla- k 76 4 s 600 w 12 00 -0i 6,0683 .-2509 -0o074 5 .k*I 3?ItI6
-10600 w0&76 i V144 0,400 03.,04 2 91 0 5
6tSiS w 17,1 06 , -iQF.70* - 500 0 -! 0, 0 6 %;X JM & tl W 9 -&i*O 0 0 , 4 0 76-- ko, 4&, '4s . ;aq
5 ^0 4
^ 40 74 1;326^ 6094 wj*iag*^ 14 93.' 3": OF SNA 6- 93 -i3 i 6 -Z*00 -0,16 T••732 -sol* we- 21 63080 m 1Sv89 t #897 w0 0 .
0#00 *76 w2v 69 7 932 5*338 m 1246 1,648 0 2,•65
2*00 o 0- % 76 lisge 5 036 - 63 0;9 8
a • 22 6 #6 55 w o 0 ill' ,7 A oAr_ *2 fm s .OPA ma 1p,7 7 1 7' r i0o , - loo" j, ^ 497.
71" 1 v, 2 15 9. * 6 0 40, , ^ 46 .
400. 0&76,^ .lo i Ti,, .8. 1 ^ 2 ^ 0#848 4 #599 9oao X9,80 1 1x -6 r50 llo , 68 12 10*00 i n .76 * w0 I 0, 9 jo 16;9* 0 12o , *76 4,452 5 ,.*2 00 w2-•'173 1 -23 8? _ 0 = , AXE- 0ATA :. r*oxKX " 7ED,: WIND ME-5 : D*T"KfmCdRRF- ' CTED S ; L F £SUP - CART iDA.FA TNrA , .._ , .., .,,..,.
,_...
., ;.... •: :> sue,.,,, .
:> PNA r , St, : :,Al . , " L/ a' " . o/Q . :P^4/Q .:: ^ 91^^ s R'^tiG Yht/^ PMT" =• X0*76 7rQ3 1 - 12 . 00 44703 64619 ; r 26 12+07 a5 3 09305 X0.76 2 wiO a 00 •` 6 . 7 r04 11 «99 740 — 35#27 -0.309
413 s i
r
;;:: ^8'^^ ^r «..7^.; ;`^5$.. ?
j 6 r6:7^i4 i R22:: ^.^:vb^ 2 '^1^•89- " •^t7 *2.3'^, .: " ^ . ^ ^6^GC^ ^+. ^4+,^4.^`.:, ^%$^"6 &^"6::9.3: . "F^18±s^3" < -Or,033: :^2^:47::::.... "^t•2S, ' ,^•" ,". • 4^t^ty +."+RO^,^'e'° 1:;x'2;4.:' _, b•'^$6. "`^17` ► '.55" O'•r31: ^ >" ^3a07: '9;'•t#g : _ 6 —2s00, r 0o.76 64409 w3a51 0417 14238 r 15F99 0.6127 1:211 7 0.00 •• ^O.76 O W0.9 60127 x 144:20 O a 471 .4 0054 - .Q.76 at 2 x 00 50335 r1r34 g -12453 058.2 =O•i73 ..
S }a0 tls222: r : x72.
0o7fi' "+653 O•g84 +4'1497 +8..46 ', 6 F Q^i+ " ^O+a^IR + ^1;^52:" 50:• ^ + 'C : •Z23 10:^ r:5°A7&" °^^^G7 '" •742 i^ ► .
r, ;r x.3.47: ^0.,76^; _ +^4;^649 •^6-*.^6 ^_.:.^i ` : ^;ot^.. <'^ ..5'«058 •^. 1"..68E^ :SASE: " ...____^^ x 0 476 r l i l*7 1 2 10 4 00 10421 X3.68 -7%53 *-690 x7 449 12*00 0 0a76 : x 2;215 44930 r3w24 r0«64 13 r 16V22 1x1:33 r =Ya ^ :^^Q.
^ • '.
.7^-I^11At .361 ! ..
11023181 1303 Na,r4^E^8 x. AT^4 CQRR^CTEp AF4E8 zDAT ^^1RR ? EQ . . E 1SUPPdRT .DATA = ` S I^QL S.
RK PIT' . A ( Dili D141 PM r ' / YMOrr.
Ga RM .
-12000 1 -O%76 99,35 -K18 1 4 6 *0 6+866 30*85 0.836 3;94o •8 I 4 •-3 r 008 2 -1 O ^ 00 - -0 &'76 e 4 6i57 -t 4 ' =$ I QOr`'`''{^1rf^ ^G'fQ" r.•.s6.1+5';. =18w76..` 3?3'.8Cj:^S .
y ^ :i{^0. ^`: ^ G • 6 ^a I X02 7'23:.
^! 7; 6 ^65r6 = 319 -0•,035 g •O«. 2j86`r 76, .. :.Ra^Q! ..__6:628 -18:«36'...: Q.222 x ` n 1 X26. 4; r'QQ -0o,76 To747 6 -2900 60291 0 00622 e Ue•56 -1*03 19.65 -0«76 1rs58A 6#197 -i9 t o1 7 0:00 2.00 -0076 Otb 2 8 5 6 822 -15#90 0053 0-49 w4;i9 =Gw7( 59635:. '6,98 9 s00 ff^' fa$ O'S2 _ '^U^03 .Q a:RO^}..i •+33.3 .a:'1:«& r7 «.1 C'.
T f" •'^ «'7g . 'x.'.37 • • = f'*4''78 -0 76 -O#931 10900 4 s 789 -2 * 06 -7906 12 -12«45 10365 .1 r49 12+00 : -0 w76 w 19660 13 4 +906 .-21910 0 885 -5•065 C? ^a Uu' OF F23R A-222 , , YOUGHT LO 'SPM WINO TUNNEL :TEST" 63.0", LTA DATA - DE ^IQ^NQ•.. 77 . .
,.
!- ..fRDK.:'f`7`^RL^N "37 it f.^0^.
11/23/81 1303 OATA:.,.' CO AXE r r l RRILCTEb O^ ► ORREC^ ' 81l p PORT DATJI 1 .IND : z , KKE S TX • ED S. N LS wy ^.
:^^. YC1 a
P14T• A^ "k: PS `S. a /Q. spa ftM.<a
P ^
i
1 »12.00 0003 oW 1409,86 21 84 3 .2 2? 6+652 324.01 -1.923 00 •043 3.1 7•96 1Q«03 2 x+10 . !363 , *26«89 095 +•.S«0.0... <.4Q3 •; rC^g^,; ts2'S 873 .;.fu573 !M^'^R6S:.
als77` .
6 .: .. rQ0 :.6:.:x.74.
^ r.84` y7 .s3t5 ^0.^0 ^ p.Eia i.S ,: ♦: *s00 54 4 M .: +S +1c.E . ,•,t3 h3 1t n ^...3^' *' .;,.^^^R,' n el A .44 -4, 4 :15 2 1 64 , 056 .- 1 39,46 1 q(•3 22.81, -0#325 8.9$3 'h0,24 1^&2 7 0«03 m 22.2C m 0.377 0.00 f 1"57 0 a ^ : nn n .na na7tis4 to, -ea ca^:53— ' ^ A;3^c v - +• v 5.**,83;. " 44.00. , 2`1.fa%^ 20.. g 0:* ^: ^! X496 ., _, : w '.:,O,:K69 .331.
3Q..a`i8::^.i. 47.1?5" . . •.
^.^, ^^ _ao s .: a • Ott: xO^p -^^9 O ^as . .r^.. r0 1:29..'
0 *; 'j 4 . 709 n, 13a74 04,87 1161 10 9 00 0t*45 1.2 '0''98 3:..56 4 1 451 13 12;00 . 0 3 4.62 -13.13 001 4 0 a^ .^. , .. m o ^ p a ... 3^ 4 c. a xs , - et§ r r e - y o e+ c aaa er r.. • .
acf-aY w'-rw.Ya :aFff c1a m e c ..a r. as ". • ORIGINAL PPI I E: M, ymuaH LOW. WINO TUNNEL :;EST' 630 S PEED * DE L TA DATA k e* jI 78 11/23/21 J303 WZNo : , AxrLs, VAN , C '[fp _AME, % 8 DATA-CORRECTEC. 9YN(#4E : ISURP.SRT ,O*Tk .
tPBS` „' LlQ /fk YMt/Q PNT' ALPHA _ PH/ Ci $Rl9 R!f i a.
. 0«05 c 1,2+00 4.437 6.548 w i•034 7r19 16.7* :-2102 000 0 006 3:521 20 10 2 1!+10 60331 - , 28 x20 c i.63i 5.,75 ..84c'0 1.6s ,b, 3 b.r7 iO'l4. 8 051 1:8'*.. 05 ir07 4 ^6^Gp +Girls t^dN ; r ,x:232 n 60,.38. *0;40610: =9Rl.
:..
: }tea.
. " 045 , '2 ^.. 9 .. 44 00 . : 1 %99' -r52 105 , 6 wo sit' X68 ^ ► 0 r Q:32 3 •0.,95 1 08 6 • 2.•00 5,855 .-20*74 3r74 194 10 0#319 7 0000 0 41 'S4725 r18«66 4x65 3«70 03 1 • +422 0*266 n„ n-nw r0_'?r f ^ . c ^va ^a ^_49 Ye55 2iiS d Givy VaV a/ S 4 V^^ V IJ m a Z i3.
, 5 . 0.
g. j %.R 1& l}s. :3.*06: P 9: 84: r +233 e :s13L, 4it6^2' 1 ^ '.:: ^.Q(^:. ` k . .. f ... , .i '. •3:x'16 1^,^ ifR^^^ : t , ^"«'^^h7..':i .,^9,e'47«•. r.91'.. , , Q Q ^ 'l.3' .
R a oQ a .Q oa« t- Q*3:: I.o 37 x .4*7*47 L _- 50.08 12 10#00 0+Q * 4 0 426 -12203 0,899 U•12 13 1:2 ++00 0.05 . • Y+717 o 334 w 19w09 0«767 1w2S r ' CRuN. 79riillN .?' :^^'1.% Y (4,R xt^23rs1 103' ' :Q A ;... a r •EQ AMEq C^^cTA-C CRREGTEQ 92 ^^.: ,8t^PPe^i3' .0^4^"A r "12*00 •• -00;02 4 4 44,26 latO5 1 568 6+099 19«59 -0r862 g • 297 *..46 2 - 10! 00 ,: oi 0 4,02 V74 6 5 5 x52 8.0:65 -10 660 y 3;. R A a" 9 +^.9 >w .Q r X42 f. 8239 ! -t^.r5 1 ^s2 ,',s X43 .^ •6rt^tQ . &< ' 40OQ ^.$^g 262 •^^ztk • ^0 moo r 3sE i t yfi•96; , :..^ OQ •> ^ ► ^^ao,co^ ^^as^. d+^16:1. .•^i^^a^ t:^^ka ,^•^b^, oh3 r+^ .^.,^., - OwOZ 6 -2*00 102i4 -60009 A 16w74 00496 2x63 14,52 Oi0c ' 04;02 00910 34,89 3 «49 7 0 54764 -i5a60 09OAkl 8 2000 0 0 02 0 0 325 5 5 435 -IOC16 Oa 28 4r39 kdi2 ^pQ '* • .
1 •:43 P. 0'.s33 Z y =-OR. ► ::, s6';ij ..
`xE7 CsO(? i^ , ;s93c2: 7xOQ5 2'855100`.
v 0e343 ..
' RS $RCip. ^CC^ ( y8.. 5^w99 ...1 *^`^^:^#^ {.. • b^i2.,._ <. w.6^' _^-• .: ` . 1.^ , . ^r'7`5i.. 0 • , ` 4^ ^, 4 ^ -00608 10 . 00 :. -04, 02 IiP25 24,79 12 4*434 -7e66 00653 12.00 1• -0.:02 4.658 " 13 W ti+55i -13*64 0.177 5x46 8.51 ORIGR I AL Pl^.00 x-225 QUAL1 Y OF POOR 11/23/81 13 03 .
WINO , , AXES pA7A.r. CORRE 9ZN,GLE; Jl8UPp. V R r
T EO; 04E8 IDX - w CORRECTEa G*TA' rX , Y ^ PSY ` R"^^' ' AI . PH,^_ E^l^< s. '^1Q Rhl^ • 'Yht^G.
PM1Q^. ' ^F^/a • 49672 1 6*319 : w 2129 30-14 36846 01200 0-- 09 4 -1;9799 2 *10900 ' -0 , 01 3/301 6+411 w18«49 Si477 2de41 M 1.645 ..
.',,^ 77 - k3{i 6"' s 0 S'. 40 « :7^. X6, t X1:6:«63.'
+ + Or,Obb :Q, ^ ; C i : .x •2.,G • 6OE }: i i <Z^F3a6' . 9 ^ i : 33 Q ° mil:&9?3'; .:..1?,^5a: 4, , yy p yyL c> 't !MsQ . O, lilkR:.VR^.f p1 . yv6; 4•'r'3^• 0-Yff63 ...-'i3•t02,:.. 0:•. ' 56:7 6 0 2 . o 0 0 IkQ -2 9123 1 1 8 7-69 50786 -20928 0.893 3.03 ll ^ ^ "0'^,2s 7 004,00 ^. -0101 11i3-Lli 55-706 r1L^tn n_a74 - ^ - o -654. o . fie - _ - T W T &G r r NV 8 2+00 0 0ft01 0i856 59487 -14637 0. 96 2+17 1*44 , .
.^ .. > ^• l.. ^ : z ..i(a 4;; 4 i s144&' ..wlZ 06 Q. ;' 47 ^•: +4^ 4 3 2. . , • 0:: ';.: Vk'f . <' F..r g, •4*96 0-Q.:*°.. 4F96i '^1OM8' 111 '9Q r ..
,.. -9 0C. + b: a7 :. 11 8: ^Q:i O$ . • ? 4 «. 7s " ., 4,.:735: 0 ^ . ^ 3'r i,^ ► .
59 ¢ -0 0 3%13 12 10 0 00 - 9 •.01 49458 364 -10996 0.689 -20-71 12*00 0 0,01 . -1i283 1.65 13 02 0 -169.25 -00195 3991 4 61 Q or %1/,23/81 8303 , , : 3'.lhEC^LE ^811Pf'CRT` ,C+^TI^ ..::y;zNO ^7^i g;::06TIk::,S, 1^ H^GTEq::•. ^rME^ .DA.T'K^ ► ECIRR^:^TEQ ^}^/fl YM la PNT' " ALPHA ^P^BT L^^i; ..: Q/irk< '> P tF / 3F%fl ...
33r SO 1 •0+100 '-29«16 • -29 720 745 -#2.00 6+376 393 21 4454 35e71 06.00 8 i9gg .-30sio w 3. 36 -10 1 00 - 8.267 ^S#, ^?
^ k :xgQ° .t•2,f3 g3 : 4^^2" ,^8#27 .: ; >^.r2.52 '!^+d'S..^23'-: ^: 3 ^0:*^ k t4 76 Q':Od^ 1411 1r?7 : w.S46 2#^/2 4 :t 6R p'0 .-: 1_7185 =b. e 1 3 .^. 006 10:'#02".
6 :..:,p :00. rH 10 F9+. ^ 254 ._ QQ .;'., . '^fl . ^:: 6 «1.26 '. '943.*1 - 1#270 3x64 40120 6 -2+00 Or00 5 . 947 .22.33 - Os7i8 7 -0x38 OsO n Oa00 1;136 5.683 •23t4O •ay666 44.22 , ws01 -109 01 0 . 599 .-24.25 -007 28 8 2;00 •0 00 ' 59418 •^a ^i^•'1 t^v 9r . *04M •O. k^b r 000:, $ •5«13$ SOS; kr19 C^4 ; : .
,^a .
y ; ^o^p^ia .
.^R^^' : ^ OR"^1.
k^^^401 . _ ^"^:. g ^^ ^o^w .
' x.0 69 . -^^.;:4a: ^ •^^ . .%-x : 2:7: ,. 4*80^ a:oa t, 'jG!:'*00 t1 rw.
m2•2.7 4#550 n 0.82 0 «00 '0. 74 .-14+44 0.283 12 10 0 00 wif,48 2x96 O•, OQ .-1+650 -12x69 -0.595 13 12 . 00 4 . 327 K 5 t OF POOR OUGHT'Lam SP EE6, W TNOIUNNC ; ^ TFST 63,0,,.
.
.
- UE ITA DATA 1IA23181 003 :.
-AXE& a TA iSUPP.l2RT",DArA'
WINO CORP ECTrm- ' Ame . D'ATX C-IIRRE.;,TED. , 9,;:R . GLE
m RNA ! ' ALPH A ^*^P%%:' L ^ROI Z Q i MIZOO - 0 X02 20237 50-823 .-22 1? 14 w2 3 P- 1*08 19152 -2,,906 11,66 17197 2 -iO+00 0 0 6-02 1 0882 6079 -22,1 02 .
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1, 4 A * 0 . c ! ^ 0 . 335 , , I .. A* 2 , 4 x'82, 2 " t , 2 0 1 0. :489. 1_64408 . - ' ;-26*93 0.8,64: -t .
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NOUGHT LM4 3PE20 RI ND TUNNEL °TV9:T 630 -DELTA DATA A:RUN ..86-RUN 15a 0 / • 1.$0 }i i3.1•231$^ 1303 .
WLN p AXES , DA A ",: . ED• , rJATA, gq -E0 . AMES QAT'A - CORREG ? SINGLE SUPPORT' ALPHA, ^ TSI. L/ fix. ^ ' . )/Q Y'M/o° RNT 1pti SF AM/ Q * 12000 • -0•;C2 f+7'6$ w 33. 3,rt4 1 6 q.465 ► 26 0 3:344 42V67 s ^ x+09.03 40,29 46+s0!5 2 , -io 0^0 V 772 y 6.45§ - 3268 r • - 6 0 3 * 51 + Ir?MQ^Q ' . V yQR4^ j 1 `f1SQ 3t;2''7 ^^^Of_ r Z'B.Y93 ^^R9si. 3 ^23r ^s ^ *ao •c^o^r ^ a:^i^:. -- i.si ^a^^r3 • ^ - sRa^3 ..-aa8^ .^^;,36^ .^.^.
_ -2000 *0,:02 6 2+213 60108 i"20v.42 1097 12 69 w 1+07 '-22.95 31,96 ti 103 7 0400 1 w O 02 2 i 166 6#039 -1#202 8 2, 00 -0.02 2 31.92 12431 r ^0313 5+715. W ii8662 -1.413 ,
ga0 aqz 9,409
' ^iS ' .cn^ • 3:2z .u`_ e4a A. C V? b i 5 c32• 3s , 1:0 6 OG ^ y a .. k^Qi 7 5 e = b3 2,9,6X. 6X7"2 40 ' ' Wik'43 1 -A • 4,3 A; a.. ,too .'• X6408 0.:X a 85 A 539 ii 4 40020' 00+ 8: sect-i4a 10+0© lo o 442 0 ► 4"66 4 -0#063 w14rl* 30,69 12 X51 X 10.02 y 0+.02 X 13 12 0 00 363 *0499 "K0.740 39,06 00'*46 4 8+27 YOUGe ` ► ' LObi SftrQ- V, INO FUNNEL : E3, .630 ..
.aELTA DATA 10 x 40 "87, : 1i/,23/81 1303 hi'TND kxE^, t^AY "^ r caRRECTEa = 11ht .'aATA- dRREGT ^ sI:Ha E &UPFORT' BOAT*.
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g : 2+:217` _ 5.^3+Ok+6,}. <`S ^tl',:.
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11 0 #
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A - 235 OF POOR QMAUTY L OUGHT LOW, Wr E6. WrNV TUNNEL ' TeST 630, . DE LTA DATA CRUN, ii/23/si 1'303 W IND':.AXE-%! CtATA . .
COIRIECTED AMES , ,0ArA,-CelRRECTEQ' 3IRGLE.;5UPPORT -DATA Li2 0/6• ^Pmjq RNT ALP44A tPSJ 9PZ2 R?fj'Q YM/Q I Wi2o00 t- -09off - 3208 - 1 * 044 807 6168 5 #4 40 5#997 -0*05 c 2 -10 4, 00 , 3.825 14*v40 6+ 172 -9206 im i 684 x .49 .
W .
3 -ai0o, OOS " 1*145 .
''-9 , 1 1 9 , , ' -Q s 96 77'; r ta.
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2 0 00 - 0005 109-94 30,9,9 6 - 6,157 '-22t*6 =41 ( 83 0#370 X.
7 0900 -045 6-039 -1.9.84 -Q * Q5Z 50 , 55 wi*85 li670 4^ ckgj agog roftoS .
R. " 2 r w0*88 w e vi9i 4,91 .,36 - , , , 1 5 064 r +ioo iw o. 0051 I I 9 5, 5W499: 1 2 rt48' , 4444,- -zifoo 43, ^M li ,440 IK33:, Q*654 , , .
t - V 12 Lo g oo n oWQ5 00262 4; 9 668 cAl 3 * - j 0 0 0+0 0•06 *05 1 8 * $ 5 V5 12 1 00 -i i O63 4#36,6 , 0.095 16,28 2,005 Y1/23/S1, ,1303 1; ' R"T / ^X^a; t^k^A ,. E Wlt4D D ^P' ► e3 it lll ` ^'" dRE^ECT'^0, SI ' NaLE tB PPQRT;tiDATA „ ....
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:QEL'TA OArA +RUB^ •'59?/ f..en 31/23
130 3
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1 4 5. 374
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3 !9".4* is«30 a ^c t- . 2;4ff-,7 :01«327,
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s^QQ y = O,QI , 1:591. ^i^66 0..(5 Q Q4^. 6a " 7 3.2 .
4:0 0:ea Q T13g,40 004 •. 1'^:a3 aico 0901 _ 4w773 Si r Qs.71Q '43..91 3:*7 10 100 0*761 4,677 0, 12 of - 0RQ1 r0f01 0,0
-00 09 309
m 16o11 Q 226
12 +00' +408 4 + 3 18
OF FG A-238 Y alIGWT LAW . 'SFE ED WI NO TUN EL::TEST'6Z0.
DE( TA DATA RUW .5a mRUN ri/.23/81 1303 iSU PRORT) DATA ! :AXES ZA.TA CBRRCC^Ttv.. EW -SINGLIE ifZND AMEW MR-RECT , L,1 ALPHA A PtI ► RM/Q ym'!q, PM/G:l s n i 6.368 ' 1 3s.56 3**74 i 12 #0 0 - O A O L 56475 31+74 -ZoClSt 3 w36 31 +70 2 - -10 i 00 -0401 4 05 14 6 0 377 - ' -21632 -2 , 234 . 1 .
I v ; 4 h oo,(t m o o '«.0Q t 74. -;06 W " 0. ^ 0 0 -0 118 i3Z,; iol 6 U•26 3 68 5.816 .-230 ! 23- w 06-205 - 2100 ' - 04 01 36267 3" N 35 0 +00- , -0 01 2#72* 56438 -19*20 -0 f 264 2*31 a 2100 •• 5#474 w 17*69 -0 * 360 2v55 5*021 2•i84 0 0 ^ J ftl, .0.3 3 7'::^- Pw0,PV9:7` 1, .4 2-* 6. 7 ' 1 0 w; 0, , '00 & 0, 5- w 89 12 10000 "001 0,48 44551 09745 -29 , 56 k89 13 12 i 00 -0401 n O"393 0361 m 16-, 32 06091 102 8 xo •.• • -..r ecr rc-ns A • • •v • • • a .e cr^^.• as • rs• •va• •-a^a xssea• rr.-a.•F p w+ • .., w•¢s ..aw. swan .vo+r ewm ^s-^-sa ® o^••• rn•w sea r V •••• o waw v R ?6 ^ a L yy^^ +^ p p ^ ^ ^ ^^^(F^1 ^^ ,4'x`2 -39 SAY' POOR 11 ` .
U 11, ^ 1Y y4Utik17' LOW'sP-EED
TUNNEL ,TEST 630
. DE i,TA DATA , lQ . ^.
RUR 11oA 23181Y 9.303 <: Kka' AIES, a*TA C RRECTE E U, AMM DATA w nRRE^1EEi '• 3L t t^E..2,C P9?ORT ,O TA g .: Y Rp$x' ^^ L'^Q. ' PN7 .,ALP14 Dla: Phi/ YMf F^ML__ .
1 -12 0 00'' W 5,294 38x, 12.
OOL 6+268 -31x52 -2#, ,47 3957 .6001 2 m10i00 ,*, :1 2i219 6. 1 6*478 ' 3&• 9^_._.^^ ;'.S *(to wo's9i' ' : 3i: QS .6r^1b2- 'N26 gA 3;` 3:r6^0 x 17',cC^ .
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YOUGH,r LdW SFEEO TUNNEL. ,'TEST' 630, RIND .OELTA OATA Z_U "95., 11/93/81 1303 iSIJPPeftl ,O Tk..
WINO. AXES= DATA 7COJRRCUO., SINGLE AMC$ UrA-O CORRECTM^^:' :YMI/Q _ Rm /Q.
PM/0 "Is F / 9., i w 0*24 'w2$.- 0 9031 12 t 7,82 -6j+ s , 48 vs*oas)l r 39045 7 x37 2 -0*24 U 260,00 i i i o 759 51 * 45 -2. 2 i k 36;63 3- ^ 92 s' t7S , -F2 -alp I 2 ^ 9" W 1 " 'lo" V S, oi3o !Plo 00 il *go a 4 9. ' iim3t.31t.. *^IZ .
6 - O w26 -18,40 24 * 41 7q37 0 , 859 11 ,9 440 •-37,49 w 2 55G - 4 f-,AA M . R . N" d 4 .4 04 "an =A- -4 4,L4 1G-514 7wRO Lk 8 00 * 24 4w'00 90 , 75 1. 1_13 T 29.3` - 11 4 322 - w is845 13010 o p V S, 5. 52 *a:.3*, ..8« 1, 9.-4 3 329 2 • 0 60 00 15x.52 12 4 i, 2 I i 1l s 977 -55 , 20 -1*273 0 0 &5 1 -.9'4 5 -09111 01@46 1 13 -0 23 -* W OO 1 16 83 11,959 -54t32 0.37 li*^03 14 -0 0 23 -2 & 00 i i 877 ii OS38 - 14 + - 4 -10,626 5 5 J02'' T o "' O T IT T47 7, )+ S.', P,761 0,04 Vi 29': 1 63 11*827 -50 *26 -607 W42 is w o'2* - •6 "OQ + ' a# T*7 1~ •8 74 -S,2i w 68 19 02 4 - 477 • x+ 49 -0- - 8 -00 i1. • .13 2, 3 65 •• 00 9,_9 6 -10x:92 20 PmO o' 2 4 10 io730 iio768 o5i,,24 3 , 4 19 ---1,34i3_o e 7 4 6 1 '_2() -0 #486 1 1 0, 346 9, ir 52, *,693, 2 3 -0* 25 .w25 r09 24 18*, Q0 06 91 110825 0 33*23 504 7 17 .-28*09 Q o 25 -0*25. 2040 339 ii , oUZ -32f8* * 8$4 s m !30 s7l . 40 2 2' s , 2 9 ► -0 2,15 22 ► 0 4 * 908 113*.-34 .- 1 7"53 26 0 0+ 233 -12-227 . -35#• 05 7 -PO • a 5, 14 (f -0-00 5 lil ...
aw o 15 : . 'l lfi+ i 46' O'c' ; 2ILWOO j, -1 29 -Of 2.5 894 ; 49424, #ass[ a.0 r, ._ _. .^. raei. c . r.s .ws ac.• ..... ,... a . eaa . s nd .,. .> .... v* .ssa xrw... .-a .. .c, .a•. .vw +ee.* .r.... eau • .• •.. o e-+ss*n "—
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A-241 f LOW S YaUaHT WOO 63q PEED, TUN EL :TEs1' .DELTA OATH tRU?i 9'e -RUN- •63.}1 LiOO t1/23 1303
j8 1
WTND"'AXES1. d'ATA , CCRR .ECTEa Ann aSU.FFeRT SQA'tk GA .TA RNT `..XLt'k PS 1^+^{i ..` ; .L1j(i 3F10 4 RK/ti L 'YM/Q,.
:PtfilQ 4 . 103 13 . 651 -68 +64 -54603 31 w90 8 «63 1 -0 9. 25 :!28 •••0Q 2 -025 ."-26 +00 VO3 + 0 2 • 56 ^: ^^F • 35' 29,56 3,55 s 3 •0*24 1!24 COQ '^'^3. 1,i!M .'12+: aX 403` a,*. 0 41, #• : 9, ^^ 'rb • 2:.153 4 . g r23'r^2Z? «Od A,":ae:0:27:::1r2^`2'S3,. , ^3' g .66.: ; •3«:g2S 29:0 .
,^ 3.-8'4: a' 89. .: 20 66 3.• ."dill r 2'` d0_:'_.'Z.^722 52^r9:+ 6-x.1!!3 284.12 18 089 6 -0 0 27 -18 «00 2 153 13 f 106 0 39#, 79 • 5.646 0 0 6 25 !0 16.00 7 23..52 18 x1,9 t:993 12.590 0 35w39 0 5,210 ON300, 2 # 258 12+431 20w66 $ -0625 .!14600 -40658 17,79 4a 5.!^1.2'9D024, ;1':2't$S` a.. e.2.6Q ' *7[39':. • 11 «96, ^, 27"!'S't.
0«QQ 2R3'3g `i'0 'OR'. - •SwQaS• -6k 4° :' 29 98.
2#,.3'8:-'' '' ;x '9 ^7tQ ' . :f` 3 iz s r' • QF25 ^a` • Q' pti 4 2fk^223: —4#544- 2:90` 11,,: i -m0 # 25 -640 1232A,3 3.111, 12 9885 • ##52 f 57 -3q957 .gg 924 2f494 12#984 — 480,05 '19984 22 ;03 - J + W.. 00 2981 1,3 n ..092+4 w 2w00 14 # 815 w1,16 57 2 , 118 i2 • 4 1 4f6q • 2alIA .
g _...4.2'5 ,. «Q«Q.A o'tsAl^7 :5.29893 5:x6i :2«!F9 4r19,3^9495 g6a39 1R+«2$: .:2.Qa ^^Z4^ ..;.2,;586:,. x.39f6'^`' a'0`,QO' .. •1R23 Z.".^i3k ..
4 C5' ' ^4'wOO .5' 1T ^d = 4^Op :12 , 8.7'1, % 38.79. 1r 18 • *1*73 0+25 •6P00 1*916 +890 •- 40+67 12 29359 INS f19 19 "0+25 •8+00 19988 12 .508 -38#93 .36 "7061 393 '79.32 • 0-25. io; oo 1 *966 129760 — 41#-64 20 4.25o •11997 .w13w96 aOg 21 ..{3s2'S'` 12•w .: 562.. , ,14'92` ^1.45p.
:'l.2^473': si*78 ^, -ova :.:; X4:0. , ,'^ :^^ :•i 8: . 4fl.r6 : 2.^ca . a Iva _ 2 . 3 :..
O , 25 Y 6 . 20«35. .'15::3:7 «QQi ^ T8' .:.1 #093 36,28'; •.3.726' : # 24 *0* 6. 18*00 1, 43 02 11 # 5178 ' w 28w26 4#703 :-Z3-01 .-2?-r42 25 w0+26: 20#:00 1,x081 129164 • 28941 44572 : • 26w12 .•199.72 26 w 0926: 2Z*-QQ 0- 3 75 1.2,648 -32#:58 46`87 : 0 29x43 .-14 17 .. ;, 5.0 4 3^ 2;R +'0 . xm;::w &' O1 . w:13' 2 X3;+4 •+23 ,29r(y s2d.s. 2 6%wQQ, ::'1° 2 9$ - 13gk-82 -4Q. 7d; 4. f64t ^9=33959 'mp^7^1,1..
«QO s -c«ad. Yaa^ .
97^a x, 4 .7 , a .98t: :-36..;27 = -04-ig t RUN .
N Y1l23 / 81 1303 + AXES, D.-Ar :• caRRcC-Tr&m ,. sU.PPCfRT,,DA-TA .
WIND , A-mo'•DA.TA CORRECTED{ S.ZNQL.E r P147 ALPHA ;PSI,. Y 11G, = d^Q ^Gi aPh^ . sc A PM^a YMIO rI,2too OSOS 0 F4 , 20175 1 0295 6li*22 - pw 3Oo73 04066 i3 1r .
2 Oloi00 16 24 09.01 4.390 0*3_69 -26.78 -o#o6i 4.07 .
3 '.g.^W ° x 0*01 f 3:3`i1; :' 6:'^36fl '^22.+c38 0 ° 3 X2.:9':2 ^ w5 • ..
: . ;-iOQ" 4 'r.4S ^' 3x4i& .. 0;^9$ 6^•ib5 . ` .22`:•81 6 8- .Q0.;69b .`' ;2;.5.2 pi' 3'^2 ^2S.^i0 Qom? 3x70.
&^1i49 6 -2+00 0!Qi 2-Sak 5 928 w 3x25 2*25 21r7O 0.363 L 1A M ja+g or.^, a •0 0 0.0i 2 6^a 03 7W'23 v 0 - r r —a./T.7T 7 V 11 D i 00.01 2 x.603 6x32 8 2100 +124 -16. 0. 46 4471 Xi. 8..x.2.3'.
9 ;04 . 04 8`p 51;•380: 0•Q'+¢b i_^39.
. 15' 27 : ;.
x, rp : "r 00` < <4«Q 6 ^86.t 6. : 13. 0:0: 40&7' ^12t^2S'. `; . OyQS : t^r g : , < :Q.
S«00 ' ^0c .x ^J:7kg: ^ ^]'3 7 Al .^.4.843 Or52...:.` 0.462 1x157 110.00 'ok(ji P1,78 9604 12 44622 *i1a40 0#371 12*00 • 00.01 G•t97 4.283 •30:12 "". 13 -12wiO O+io -0.186 . .r'` -i+^.:-^arca.Imo...:...• - „ '=r..i..z''-4 auku a. 3 r-rv>u.iwsc.- t 1:i /23^$1 1303 .
y^,r NO ^4id 3; pJr ► Tk a CCRAECTD "'^`4r .C.^3RF^TEC..' SI^+^bLE r1^ g ^1RT ,^/47^ ► E^ C^?
'
i Pl.T iL.Pt•C ,: S: L/D /G-.`': n a^Mt.tt? Q >t1 RHrG'. y
1068 A6684 m 12000 0091 510753 6+378 :-290'67 1 00115 , . .0.01 W10g0o 4i575.^6#316 ;-296,36 •OeM 4«45 "°, 3r f ' •: ^^$.?9,.
Q+^ 't^9 ;«^C•..$1;` Q?4i' : 320. X30 6^P, 3. OK . 6 a4aJ ..2.48 25"b0t4 ` 3"'58 a >k.5^. , x 11W Ai r — A: At .?^^ ► ws ; i i M L _. ^.^^t° ner n. r+la Y.
:. •.^.T>^._V.
„<,,.oG^a.^ W -^' YVa °"^Ud `_— i.^ cu u _- ► spa.
.. ^i-1=1 _^ 6 w2.Op 0.02, 3.530 5«305 .•22.80 06225 3*73 4 27 . 3.74 J 0.00 . 0 *.01 2.858 5 658 -1 9 . 26 (x •.2,29 4.53 . # , 2x 2 2g8 00 0.01 44.52 90,15 8 5# 42 ^ jk Q g _.IZ*- ^3_:.wq 4*00 rQ O 5 77 ^0 1:53 9.•' l34 ^ '^ fiO3 b>t 43..
4.
: 6400 i1> z.0 A sa2r -x3=0 0^:. 2:^ ^a ,2s^r ^,^ 8sa ,zX ^0:'45^ Y ' i2. t, ^h +'$'4!5 +'J41.2 .7:• 0 '^ ^ '78 :^ --- 1.0,•00 ^^- 12 . 001 x•2 q :31 7-tll 41522 w 10 CkS'31 R1K69 Oa i 0v01 Q : -126-73 2«35 13 563 4 # 372 0 06198 wools -..
._^ ^- ...
- .-_ 0000 e —0000 — ^ n a uVL-^'ti '-u^u x.
:^R12M i.ae ^4^f31trL^'Il^ 1-.303 ' Y1A29 j81 " 4UPPO RT^_DA:TA fiKFB b^T CORRECTED `AMES - ^D T TEt^ " 3TKQL ` A*COKREC .
BFI lLi ' , : t' Pmt `^M/8 L:Ibt^ " . 01Q pM/^ ` SF-/Q . Q fRS'3 :. " Ri^T AL? A 201= A3 6r14 13870 t00 01,00 ; 5.920 . ,a*25*2* -o 1.281 -12 6.6i 15176 '"23.78 -i.2i2 "10 1, 00 0«00 1;521 3075 .
16:ii9l^.
.; ,O a^00 ` 1 "x7 , 46 " (x.45$ 3 r9^ ` 3 • 8Ua . i 0'1,7 ,^92 '.w >t75^.: i'r/^2 :t7>^77C' • ' .Oi? ' .`. b^$63:.'26.72 6+Oa ^: 3"x'01 _ la. ^c9 *-^0 ."'.Q'400:.. 72 X785`" 2 11+X73 . . *v46 •00 . 0 •0+30.48 0o879 6 2+00 00 938 5+623 w 4.08 101,50 -OOL36 9.687 :-23s65 Lr529 7 -0000 — 0.00 `r89.po 7IK98 0.399 •0. ? d0 3.75 *00. 0(7 50336 8 2.00 • 5 '.
;`, sOf'S3,irz49:: " • A FB: Q198 S^r188 w'^:OQ " ?3X 1,05 9 ?.QOM; 'is ` : B rQ0 P , s '*4471 :`'i t0:' .k" 'GkQp'' •,Q^ ;^' 8"R^^ •• "ti' .,^,_ 7%78 ^0.86 0700 ..01778 4.805 :21012 0.040 10900 10.00 •8*61 •0«00 • 46 07855 0 18«59 -0.342 0 2.20 +709 13 12+Od 4 000 0 ... -... 0000 A-245 4 V!!tJ(k+T' , L0*'SPEEi3 *:N .D TUNNEL. TESTT' 630 .DELTA DATA f RAM 1aci^fltiN _G 1 ran - Y1/23/81 r INQ .AXE8 C14TA .
t_' N ' 6LE. zsuPRoRr DATA . .
: r .XL'PHA '=P9x L/Q,. ^i/il R. rP "` Phi T' 9F/Q RFi/ M'/ t^" 1 *12400 . OR04 M A4486 6.883 39,60 6.21 .-11.64 563.36 -O+i75 2' wi0;00 " A 0401 6#857 04"90 13.62 *1207 5.530 Sr3.4; .g00 y .
Q4Q Q9Sg :; t 3 7^•Ot2a = ^2k..37 ,'x..383.
Ys2Da.:.
J 00 .', :*!Q'4rQ 8.805:. 931kr93 .;5:.t76 Rt) ' .5 .. 60 ' , OrC1` 0;«6$6 840#' .'
3Qw86 x.103". 17#1 2S` -2400 , 0 6 0.01 -0*361 202 12*35 6.299 .-21,90 44081 7 -0*486 1,23 0 0 40 0- 0 0401 5+984 w 23s-34 3+504 13 52 .^ o 11 nt% , -n_nn —nano. -WzA _„.. ., 05 a$ 4 •:AO f° « i3 f 0,'x 3, 1!0d00 g ' q Q; f •Q' ^bQ7':': 5:1692 , 28 2. t^'9T .
44 ;.
! ' a^y7t # 6 1 1 6«OED :^t1^4a 0 s : l 2°9;+^'° 1a8'ss 9130 h ^ 5'^s43 2 C ! 4 $ - , ..'
339'. <`^^2$ k76 0 10 ► 00 w 0«00 .-1+099 +2c62 13;61 12 5+104 .229'90 1;4347 13 52400 . s 1 378 4 0 991 6 36. 1,3 12x32 00;00 .-21«43 0.658 or POOR Qt3IAMY A-24 ^'^L^i^4H^F 1,0* 'SPEED ',^.1VD TUNNEL : ftS.T 6.30 .DELTA DATA n i ; ^^tls.^(Cs% 1.01~ 69^lt s.^oc^ ui ; t RVN X .
,23/81
r3uPP^R CaNg T o a I,GL >Q^T i A t K R'.DA.Tk-CoR TE wiKa A14E$' ^ YhiEQ.: A" ti^^jt^ 3F :: R MC1l^ ^,^PHA PT4/ /D Pte, ^s s.62 --47 *8* 2.244 .12.00 ' 7#277 3061 9.636 0 0 01 , 15921 i-33•c15 13.35 8 .5 ► 3 7.368 2 -10+00 0*01 ^ 20434 j ^:-3^ 0c ; o :..a^o+^ e¢ ^«^ sE;^ r a QZ'^ ^ A T ^"-9 :9i07 y^ yu^ .} ^ y aa h^•K f'i3 s6;000i {. q 3`Q "'^. I^V •'6F'..r'^^7 r i^1.•. ."
^^.«T .°•. 6' /'.
'^^, ,; .: 6 r 29'.
; ::,... § 26 i0 ^ 08• ^0 . r : 0- ' 2•° •^s.. E6^83'f' '.-29 ^4 X83 6 * 482 : x +21 *65 5# 904 ^y15 6 "2000 •0101 i P5 70 n 64 1 R4 r4K rn° V T o V i^7ysi 7 0501 0e00 L el a3 v'OC. '^ :4 +Oi 7 '5:+6*} -i8R33 =0 9 0^ d 346Q7° , r ^`r : iQrQ(1 t^'.Oi Qo$ r1r5 3.401.'
^^10 - 1~7 " • f .` i5'9' ^: a.QQ `.. 3^^rQ2 `a3`.6+K' >04:Qi *17:17"- .Q 6 13 *60 10#00 o 3.1,51 70 a •.01 5 1+05 - 179 , 34 1.11 Ic .0 654 2.359 -3@,08 10*9 0.'Q0 d19*,54 12000 5 9 014 >jY A-247 t 3•w89 10 * 029 12&61 —48057 *1 200 0 - 00 00 2 - 4 16 .- 7 ,2 54 2' - 10 ; 00 -0 0. 00 2;524 7*244 -iQ*3' 7 8t555 12&51 — 3206 0 0 %7W 7 9 9*4411 . 07^: -,;' w 29457 3i 0: 2%t , 5 444C 0 .0 000' a462 &.533 4 * 8-0 11 33 6 - 2*00 -0,00 1#818 5015 - 4%68 6#400 . - 1-99 , 86 5.603 ocoo 1 * 500 7 0*00 3*,75 16,89 6#124 "14920 4.810 9 20,00 •0v00 .,liog?
5 ,80 -17-Z O 3*.06 6069 *, 0 27- 9. + o ' aw lsi 50606 t il I 3 ,722 5.,3.81:: ii. AiWo 6A.
M 5.23 -wi&ill .4 '3 * L , 4, 70
~^ ie 10*00 11 5 le d + r2 $ + Ow OQ 0. 274 5 # 1,20 -17*30 3 9 17 *•14 13 12. 9 00 Ow00 -0 0'415 44-929 *3 *,35 12o7i -18,06 2 * 427 OF PCOR QUALITY A-248 YOUGH ,. iLCIW SP eED b1 INa ' F UNNEL ' F UNNEL * TES7 630 .DEL,TA DATA *to . * Not j03 I Ruw tas-Rum My DATA SFZQ . RM•.Q 'yM/G 0x00 69344 6r5 9*434 16 109 •-41*05 i _iz 0 00 0.547 •45 1 7 %38 •0000 0;389 6.293 2 , -10 ; 00 ao,,94 jo -39 3 "627.41 6 0: Z74, 9 - 1 1 . . ISO 7*1 ..
0 .
:r, ": 9:.
g w l C) 1 5 5 ill X 16130 6 x:96 -6 6,61 + 3 7 2,55 60269 -2 2 .8 6 -2 60 0 - 06 00 V - 1 4 5 0 7 OOOQ 21,19 1-0J* 00939 5,777 0 18f-03 7 0*00 200() 1;078 , 1.90 6«70 .695 9 4,016 9 0600 5 ^ -20.8 .
'g - Q ' o a.
Cro. 4ilm 6 6 l t , rROQ E «Gtr i l Q 1'13 - - a" . 0 00, .
i i., 9 ; - —.,i S: 59 ® r E L, a 7 - I .
1 L 2 1*099 0 4 , 943 000() 1 0*5 Losoo *0920 -15w39 3.208 ia - o 6035 11087 w0+-352 2.597 0 12 i 00 -0 0 00 4*941 -17f05 11/23/81 1303 a^ . r ,y Nr.Ha ^x^,s ^r ' r ^: sxNoLE uP^CRT , DAr,, : MES ;a^T^ - ^c^R e L/Q; t/d PNT AL'HA.' =^`g= ' 'f^^it^1 Slrfti^ RM/G ''" s,^a ^ s^'^^ 1 -12000 OVOO : 20160 60Y07 o & O S 15..44 ^: ^ ^'^ ? b 0 • 828 2 -10.00 .00 5.886 V94 164136 ; ..^:.^^2 ^•e•o0' ::^ -t ^o^9or ^ ^"*ass > .00:: y .
a oa « bf .: oa a ^, oo r .
54: .z ry of Eli «r'^O 6 -2000 0&00 50795 e5a^• 5 1 1.912 t,^^^ AMU ^ £! ^c "'c 0000 0000 50614 7 148181 -.63 4r13 10J}4,0 sn 8 2000 5#424 t? ` s" 978 2"V40 z jo- ...
' . wrL -r « 9 ,.
4 . 00 •OQ ;.1 8b, 38^F R4 4f•^77 N Y tog '64015 5'w -18 +37 YI 2.95 46 .6051 -3&33 -18r62 10206
Or ' .101N I AL Pn I M — B
QUALITY OF POOR A-250 • vauai4rlf1W.'SPEEo,.Wrf4G TUNNEL:TESr 63.0 DE LTA DATA 'MW 103 m RUN :11)1. 1*69 11/23/81 1303 , : , ./jXESi DATA. CaRREI=Ea AMfS SINGLE 1SUPPORT',UTA a, : ,0A.TA m CaRR'S,CTE I *psl, , I .
^ 1 1C,17 1 ' VP Llg n/a,^- -Plc^a' -ftrj#f3. Rmta y MY a 1 14 L X 1 V512000 0.00 : 2.567 5*887 'j-33o,88 1 * 639 w oq , 80 2Ue*1 2 •0 x00 'xlo i oo 1 ; 979 51822 1.21 16 x22 • 3 ' 1#, 35 i W *36 w-1;* i; Q3 2844, ..
dr 2. z 440 , 0 00 1 276 0 0 , 0 0 7 ; 0 6 -2 0 00 1.870 :-28s21 1@038 -0# - 1* 2*li63 0000 5 4 772 5#584 :-25489 0,65 214,64 7 0 9 00 -0"00 1 0 879 0 * 838 2,00 . 0,00 1i5a5 is 15*485 — 22 * 64 00828 0,14 ii4s io 0 0*04 *w! .. . *' * 23 0!'9.18: , ^k w:L 64 14 7r 4 2,, tai j f* 4^'s 3Z, 7 7* ^ mi M 3, 19 10 0 00 3%46 0*00 . Q i 248 4*535 -307 -179.23 1;9501 0@326 13 12000 040 4*315 2* 4, 99 -14961 0*871 -0*, 9 5 a A^2S1,.
S2 ^^ ^^` ^?
J OF FC . ^ SUGHr L.OW S P EE' p wI:No TUNNEL *TEST' 63 0 p -.
.DELTA DATA ' ^:O b 4 ^Z1 s N ID'"r ; iFitflB^RUμ ?63 3p/ 11/23/81 1303 A3 ES Q'ATA ` .0 > sUPP43RT:4 'T^ 4(IND aft=Ea AME3 DAXA-CBRRE.C.TEG'" SIVILE w . .. _, ,^:... ^..
..
.PSI ! .. L''1Q..<'` PNT' .ALPI+ a1Q, Ah!/4." t SF'/d. R'MtGf. Y'M/Q.
3+661 -0624:-28«00 144665 *+67@97. 36+26 34.54 -56556 3;329 2- -04024:% 6 264000 '16732 -634055 -56527 30&32 5-21 , 13'40 w : $'iii?; F. ..Q.23 w24:C^4 ^::' 57'r4+^8,. '::Q4.5 a8:i 31 5^t8'L': ' A - -0:x27 ;-2s ' i `« .0 . $55,. 52.373 °; *^s1 X26. • '-3.;8'.8+ 3,478; , = : s^5 x15 4 , .,.4g ^.. ,.Q..34 :2D.«Qp.,..sB25
'ifia979 as : ° -S.52 . ,24x:1"7 9.19
0+8.04 11 *463 -0+26 .-18e0Q 22#85 5%68 6 •-44+14 w 2e3Q1 7 -0624 -16x00 0.995 4%43 -40#10 -140670 17.94 11+071 tAL v7_.01 .A 1x.76 1.rS_.65 7. 514 2L rrvv o y?G7. vv1 ,' x -^^a4.^!Sa«pQ ;8.096';, =-52 : ;82.437 9«43 15.;448; ,9 S'1.+891 «37 '^0.24':> < 10 R¢8 2r?610.52. •3.r2'S ; 10 -55tQ7 -^1r4Q6 13sQ4; •0`^ 24 y B : 2: #SA.. °.12 ^304k < . «7A' IF ' QO 7'i95 v o t X59 3:20 .17 i; : -0624'.-6.00 2.094 -59647 181%58 -124376 -19549 2987 -0623 • '-4 40 121f87 13 00 Z ^ 8 02 12%274 -57680 -0.755 1w49 -0623' • -2.00 130,96 14 li879 • 12!321 -60o , 24 -1,335 2x16 -.
fi., 2 . ,, ., ^ 0.
: " ^0rR240 ..C;C ^^56 ' e LE" .^3 r^23 164' 15 k :3.7`' .',SQ.260 sQ;Q . 3153. . .
. x :, x$98.' '1 c^ i 34'1' '': a3 *'G8 •._;:. 1:2:3 in +7 ► Q.. <:'2493 ' 0 • ^4` : ^ s5`Er 3... +4'v83>' ^S:+tJ1 °:T ti •24.' `2.x488. 2 99 64000 157 499 -56137 3,6618 -5f18 -12x52 18 - 002 4 26 12 .
86,00 -04024 2%494, m9.70 19 1240312 -569 4.187 -6..62 2 65 -0 24. 10x00 126652 -56611 5.474 A 1U;27 :-20sr99 20 40 46 , i rQQ. 1; 53 '-2.5 1 37 12«763: ; =5-245 Q5..1:4 w13 .a - F _^ «pp 2 x5 a•2 -^s:.23 ,r#^.as k=a^0.
34 ,a'ss7 &.bra .
2'3 `2r,1gp; +Qu24 « 1,6.Q`0 " 37,6b- = d 21w77 t l i i U 0.1..
402.:;. ' 56868 is -0.25. 10808 •31-079 18 «00 •-38073 6.296 .-22.36 24 126890, 25 -0625 20x00 •-38x'78 1*320 126995 56575 :-24r46 .-28&19 -062 . 5: 22«00 06 890 x94 .-22+20 26 13eT47 -4 .4,.08 5,000 -26 . :.640J ^ -(2,. % S ;,'$ :^40.' :13 , ^ ► '1 ` er38. 22r0.?
-27 -7Qli: '6,i7;. rS1 p:.4$Q .
1•p5T " r -0: • 23xd26. « QQ >2'«3.9 28 ^ ► :sZ6^ r^l6 + 40+89 >: 4t?53 51~;!4r l '9'4 -Q'•.23 _'}' 1$i:L1Q t'Qrd ' : A :4 w764 : ,.48:«44. i^.iL97 .• k7 TSB iy ak•.Qlfc ,- .. ..: '..
:. '' ..
.^H'.4u'Ci'FC.11i..T^Fiai••^.-`.. 3:Y'!.al4r.-.M.p-f-. ^:..^..
of POOR QUALITY yauoHT ,LOW SPEED wrNa TUNNIES.„TEST 630: .DELTA DATA f lo,oNC.r. 07 Y4.8 i,^^a ^ tR^N raT•gUN Y I .^.;_..,,,.. :^^:,^.,. ^,^w.,:.: x /23/ g i 1303 ; , sUPF0RT ^0AT/ OkTA : BATA-CORRECTED S1NGL9 ^, a:'^ 4t R EC'^EQ ,.AM 3 , .
s'' 0..
Y"t1/G . F'S,t RK/a ALPHA L/Q «7a -J2000-• OS01 go 6x529 w3 2*590 2 06 w4a604 a tti#.39 2;34o -i0a00 . ,.0 # 01 6*466 .-27* -Ss58l 0 17717 92'42 1 2' ^KS'S .!M iO 0 36 '• ► 8 00 ^ ^a, 0 6#66.1. moR6 s Q7" a•O wSSR” 3 "« a:3g 78 26 ► 6t.6^4b. ^a2 ^ti2 •3.29.7 - 3 13 ^a0 ^ a lQ'^O 4. ^i 4ai&$ .
5 •4 00 =: Or . .-i9.06 • 3' ? 1^ 88 ,* - 58 0-,223 + t•^33i' «56 : 28,26 '-3 6 -2,+00 - -O Qi -Q O 144 69122 :-22 o,98 !2.286 i*o*9 X 26,.26 w i9494 -1.56 7 0000 - -0•.01 -0 0 *i6 5 6 841 O . SAa 2.Onn.na - o30 6}90 8 7455 27042 59 a.8 .
r •0.._ •^^^ ^= •o,^^a ^• 7s _'; ^^is^ {^az+1s 0-2.73, t oo.. Qt SO.
6,40 -cas =a:7 $a ;•28.:57' 4.132 . f X20 «i3 .,.
2.8' "0, 71' *44'17 11423,.
4,00'' wool; w0:4j-9, ^1 *478 1i . •O+Oi -Q.863 "4.37 1*48 12 10900 0#6 4 11 541 0028a,88 71 4x53 1 3 12 0 00 "0 4t "1-009 ooJ39 x 807 01 0417 8 2907
Ai?pBNpxx a - inn schedules
This, appendix presents the xnn schedules from Low Speed Wind
Tunnel Test 550 conducted in November 1977 and the 40- by 80-foot
Wind Tunnel Test also conducted in November 1977.
B-I
Table B•-T. Run Schedule for Low weed Wind Tunnel Test 550 MODEL CONDITIONS TUNNEL CONDITIONS PT.
RUN a TUFTS TAT1C T&I ALM( TUFT COHF TEST TEMP DARO 1P ENGR DATE ^3[I REMARKS NO. NO. CONFIGURATION RANGE RANGE PICS PICS TAPE PRESS e 11"I (OCCI loci) (! n mixo) ('!) (II[•HC) Is71 E C ( N1 P1 It TLV . F1S1 TS)1 -15/1 0 29 .
"10.1 0 ON X 11.94 64 26 26 81439 8 / 439 Sail oa,includes partial lip fairing T2I0 1112 Z X 6y 29.21 27 Add fuselage atterbcdy
— LL
+2 x 28 wing orr 2 u2 N 1 _ X 27 Thin.ving, S2 66 29 .27 27 Att control & -fairing 3 X 60 29.43 Thin vingb . repeat of 29 31 _ 2 7 J3
Q
H 29.49 ^_ - 2F _ X 64 32 Wing trailing edge Pairing G I -6 6 X 66 Fillet n at vbeal pod 33 _ K 3F 32 td ' v J2 IS 1 x 34 Float kit i k 3 70 N I' + c c^ li _ J2_ faired float kit + 35 x 34 w F X Change wing incidence fro g 71 2 9. 1 19 34 't5' to 0' T a w IF` Thick wing T.E. fairings X 34 W, A I x 23 Stroubls &trakea 'lip ' x 3 23 Thick wing; T.E. fairing W31, 66 29.70., A — 40 Thin wing vith T.E. fairing 114 Cear to-wing f airing .& - Il0 f_ 41 K _ OfF X 71 'Ca iri still on 1 42 F2 81 29.',x2 . 40 x Fair over exhanst ducts 4 x1 x 110 Alternate'T R e ► rhox fairing _ _ - 1$/2 X 40 RMOVa slat on tell H 4 1 x2 1 X 24,71 40 _ N A It/A' Faired model strut FB6 *46 x 29.65 46 II 43 8 439 q
i
t X• INDICATES STATIC TARE TAKEN wing angle incorrect on Runs 29 +Ind 30 110TE 1 - Left
Table B-I. (Continued)
MODEL CONDITIONS TUNNEL COVOITIOHS RUN PT.
Al q TUFTS TUFT CONF STAaI ATSGH TEST TEMP HARD ENGR CATE ^SE7 N0. REMARKS N0. t ^i ` FIGURATION RANGE RANG E PIGS PICS PREW, TAtiE focal to[ q taccl tPsrl Uhxyot t41 DWHII D 0 W1 K2 N2 H t T E V G R *I "It p 1 P 2 I O 0 11.94 15 OFF % 75 .93 9.81 1 /439 439 0 9 _ RHO X0, grit add to AoaelcanopyixinglYart S.
I J x 9.29 1 SinH.T endplstei k tDIII.Grit oatil _.
- t t farther 7 3 0 1.94 x/A 0 fS .O 90 -35psf in 5` Incr; 3775 in 10' iecr.
— - I
R j ao'
0 -10 X 75 .94 1 -^H - I x _ 9.28 Stub blades off 6 / 6 n 6 t R i 1 x s 91 z D -2) -U H l 93 9.21 1 _ 1 1 I X 1 Mein rotor off ru r 9 -6^ 06 y^ 2 i 1 Stub tLdea oa } X HL _ Lill LJ H 1 1 81 9.26 ' 1 Flt.teat m protrusions oved
r
12 1 Prod .dpr^ 79 - 1 -9.26 truaions remove d _ tO * 1 3 _ x '}fain rotor oft 1.4 - Y. _ 81 9.30 13 fail rotor Off _ hH^ I - 21— 15 ?C R9.26 13 Land. gear door s as 16 _ -- - x _ 13 Utnga oft _ x _ Fk? Endplate[ oft T ' *18 — X_ 84 9.27 18 HOriz, tails afr 1 _ _ _ X 18 T P. guard. ant enn a off r 20 20 alert, x_in off a H-, O M I k H I E Y G x _ — - 2I TCs 1 62 19.30 1 Flas vi soaltzation 11-2 — tYt x G8 22 Stub b lades u-C 2 L, _1 15127 & *2 + . 65 F]tb aust tair 1rg Fl _ 1 ._ 23 9.3 0 69 24 U/43 Stability rtt.
0 - 1 2130 _ x 69 L.
c^ 26 23 8/43 -6/6 O _ L Fa7r over m zl S3; 25 _ * INDICATES STATIC TARE TAKEN Table &-IT. Run Sch yule for Full-Scale M222 Test in 40- by 80-Foot Wind Tunnel..
tl T CONFIGVK^1^•t0N °^ t ^ ^Er/}9RK'S •+ HGLICo Pr cx St/rroxT S7rRvG7-rv4C wocit • Dvm y 7 6' DI/yr FTVC ST . tv.; 1ST C.Z No IRTr FE.I.SNCEr /Sj'1G Eurt T^ V ( ^ F}/ 7{iRE =0 e ^ Nct- U tT..^.. •N^ n 7t F^ilRtxb tnJIT • iLLEO / 3or C c ^^ n / i6.6 IMIRD O,; iasE Q.+x 0 D / + 7 o Aa .
i TA4r. Run Ta G6T ba aF JH YA`^t C^ JO'/30° 33 WIND C. ( ARE Rwi Q e 3 to-46.-_ / E C Fflr.ctr/6' AND j--)' PrAwr Fnlnmi- / NI Ti1L L ^E'O .f if ,Pi7N /$ • f+)S O i/GAL C 4'•S ' 1t111MD rA^aE P-M 0 3 O N C^ 0 -Is/w DDA•-Y rT II •l7 P./rD/rt !'A/+t7NL 9--So $ O YsI0.Tlr/S c. FAtJI/rJF S37tr: O N J LIs:eGEC C2 ? '' _ 65 WINO on -15 a Ta.zE R u N / f /s x D Li C R 1 /Sl+/S Faa. I 1 9 E `1z H A G F9 3 . NL A P'L TW! K I 7 7 b O t X Z P Y ^ StAvic. T Ar r- MMAL. CaYF15U"Tf-ff v UP T4 3n 1 0 tt1!/ 5 ft>y TRIf AFOe TED DLIE T- 5R xF- co yA- £G — ANt3 Fr<F.IARY A On ^/ { I+1S o gCYA £ f'StY RIT—ED, YD-L ? a W-;7N Svy)a..- + FntRtaG Cco-tF ds^^S^L . r^ji des 1 A761.YL: f°AfA ^' $ 6 O Hy-I'D ` ff.- _ Vx N Er.7my t ,j jlc c Zxf_-r_D Kz P I-14 /+)S r Am';6C OFF, ,F71rL • fo r S 7 -6 /+( o watt AxAr G,icr CxF 5, 6 -b /+4 O Sur-a7 1•.ia r= ) v4;. ,•rD Y Ao 9xri Er+ owrr I pDRSr CEKTFt Pl A in Az- -10 Ar.
S C Sgj;) 4EAC Ce—f- 3 'CXor.r TMLa FA(ar • ,ts Xmic C:.A p Zz iE FA;C' y GS O FF, ,j; zxdt- jK,j tQ T LiGH FLOAT r;-t TC9 C2 5 !(i ( ,T i T L -.c/+Ej C fg wr YLaAT 2e.a• Mi r A FI A .sAr ;;o a1 O oFF ! i -LItL srm L eomn6 GEAit D S Z - G /+ ;Z-stj£ H OtsT JAIP.1rlG QFF s ] Ti4E Wirer- rLaAT 7"lpr S 13 .T - L/t6 'D ADD 4SELG _. - S}1APED AFTE zBoDticS To 1.144 O - om- 5 14 FH T! tE - F LO AT rw r 4 lr I +fAQ - O F{W vfo SrDS 'To 'YC`H^tj17uTN 6/+E 1r^Alrt ^%TcC YrLACEt,. $ ET kr -6/*6 Q R4"', { 'SPW L} ;kwir 2EEH 4o, Q /G s'7Zf.av7 j CHAxGG3 T s Rio .t o -6/t& o t o° E^c Dotirt w,z.i ATO^C Tvkmmi; G e 407 * , G Dcarts 9STjcACTizD !4 RtE 1/I S N -•`^/+C 0 ^• 3 4 Zo ,'/D /i/$ 0 '9AITZ C£AR AND Q.ETrA CZ• Vacwt t 0 le 6e a Cr%•1/ARE t - m{ jp Tmz rilcxui4 4 Zt .-6 /tb AZV•1vrg, T Ri' O :_e. Frt rrnety kc.^o+6D, CRt6rNAL • 7NS=ALGES 4 ZZ ^-G/*6 YA,L t?G 771','- L FAK2DX FA1R1ns kt p Zo6- FuFL $urn , p Z7 a D T`fp[ i=urEL1GE AFi ELBA /jCf. CoYec7 $c'[Frrft /0/*IO P, O Coyc «D By 4% Rwro, AF cc000Y ]zEMOS as ZQ -te Fv EL Sun- REce;wEr ZS IOJ+10 is 7kAt..las EvcF. FAIXINCS Cr{ THE STAHM I D WIxG 7 wiF • O O r Q T 'IF 1rr 4ACE Ar THE D JUNG TF, 7. t. F^Jlth.'r - :7 i.t t.
2b -/ !t 6 AOF S^lAm_ rx . " wmr " tu ma TrANDA • 7 WIC -/0 7t jo O g6 MoYE MAim GEae T,00cS ] 27 j'AZ t a Dowuz /o +b Nose GEir- + I / 7 28 NL ! Rr-OYL.
y r A 5QLh _ r t,tr.•4 „r, T.C. IA/S I NG, PrTALL LLA<^: tr y•^•L•.'•HhL+ W " TIPS 27 /0 /d6 h's 3 C Altc, FLO:AJD.Nr, At 7 N I Wl ^aT{.
^ .i'C.lrr.!< Rog, g ^r^cL 1'AItPoTOC As r ; •' a.+icG ,? 3D :6.6 Op X3 O - 3a^+7a YAw Ctoce , Act, J = rK / Y, Ao^ Fin Ex Etif:a^,^•z<r.*r VA 7• ^ Su at }(L *JS O jc Fin L-%=s Att w, S TA • ,:6>a WI .r off- Pr'.,tr -ZAvy F.ImmC t Ou 65 Y^ !4 / yi & L / •nD1r1 r ;w ° r, Sj,^ATE ► IAA1ii ZCY<nc7'L'^ (.4 /f W"EE" Pat !^1L Lf• ; 3F. /= a TH.wwo; ;nTB U K.
JD tS I " It -)2 /4) 7.
}. _ D AtD FUneLA6c Ar QZDOUY jD 33 -/Z AIL E F. -was T 'Thr. U•)lntt 34 0 icA1LI4c DC F - w3F ADO k t ro"...
D C—^ l %-Y:o' IK Ehfc Arc Eo AA+rr E.-c , i C4olInL rn 1j 35 OL -6 / *6 SGCrGH N rvctr R r i cs. F . LC ?LeECxt -.
- t p . Ar:rctrt . JT A r.t.A g ,KC ^+ Ct6RTYbLZ a-L Scaes 36 Ot6i (I/+b A tY r R g7 -Jy/+)L O 9'r Tv.rN 1nF AT 9a7. 17^ `lrfi7 -33E Rr'n) _ C STAmACO ^:.rurc.
Rt .hr. Lip C.- X-T-a 7- ', 1t 321 L •'/L /+/Z I jilt, FA,.N, !a Cevrr — MTHL 1QM+rM1Il1. Y mr.
.
Lij, FAlalxc, orc. w i I XPA-er ETECrbc,, l ^sr ^P y a f D1f -) Z /+/ Z RI;AOvc 0__ 4 1NLFr 39 o I!
/ 7/L O Awl 7 j, fC llrr .e-f °f .^Ay ^)Z 2rFLAT •.
Y •.
1l '^ ....
l.i i iii• C) Table B--II (continuca) TfF.^ ILK f R^Id:S^K3 ^{ CQ1jF ► CzWRATION s j _ ) Q C E t r y 1-} ^ M 1 P y ^ l ^ 'iz J f 1 p O iHS7ALL FL1 G8T Tsir 1=xHAVtr E-zcror [' / IIRFN^S, t'J{ILtS,'. ? O ZC1-';' JI:yHF .'.C • F^[SM:.
^i S^ P j ^, T 1x:v ^^XL.
4[ [[ ,tt +z WE -b/+b a gFroYC EKK: VST &-SEt>4C FA4ti-4,3, QC_- .= Bxoxvt =ExT Wtsr;, :244 : w f.Axxi F:SO;z iI IZ,Gtt-t WII TAA16mr F-9:E FA I XW+ crf A; O p fJ A.
E XRAV,Y ^JECTeR 1'HUINGr, [( A'.f -Jz /fIz O FskL SAtt. [RtTnnttL.
Jl r^ [i 4; j 'SZ ^Jx 1412 O BAp$r fx%; 6. pp Ar- ^OTATHF i0.j RCG = F111 CIH4 ca C 1t r o p - tz, An Fix AAtx £cznK. A - 60` Axrnur+t RF,n( p v_- /A, - ,rZ w%ww' C=iTx ;.s F'tertD D JI 47 Qia A X ,nrr°F.stetry tz 1+tz rE EHAr4 S% It -Rs ve C-"QHF c FAIrW44, zo-cam rxs "^aF YC B! .
IJ .4 8 ..
.. .. .. :, 47 - ,a /fiz o i*r srEK" jj YX /+A a •, - & •• - ^xa" rrx" " Y.
IJ -12 /fjt O LA2Gq' FILLrc'S nr WHEEL Fc RaA,C Fat<, j Wimr, 50 p YEV Trtltr !( SJ ^'>tt J'J TAIL SLA': F_'-_ .VF0 [1 -Jz A-m O HCPj ZoKTtt SL ? AC, ' Fax F 7.A+t•7 + -4/44 O TAIL RcrcG G u A t t9 fvxAVYEa tALJO ClL ) A-.reCf SOCKa3 ' S a i' F£^=^F?
ArmJia WK o y oJt STUB &Avti, AZLivr Fas:r.#x GurSret:pW-rr t h P a C FAg--n 3 j! 59 rS -b /+b a Axv%,rrt Ratan r4 gyp ° .
5:5 1j Rca n r• +• zc' rQuar-a-IBLE} -fa,db O !t n «t n O° -L AL C foatrc AmznzO VIA R^ PIS i[ ^ t / er •t n 67.9 (Ssov u FEr- W1^ N RA ;r 1:15-Auzj, Z /3IZ L 14AVE F m xro FLrAr tS'c I" ^x/{1z {^ SWITCHES. At.t47[ED FI A T SwAi SF I StSt 947- ^J;ZA'ZIZA ft[S7ACa nCA • t IRPLAT n rz - jJ 59 J[ /So -jz Puz O F_YPPLnTEL JCaMZVGp ^ , J[Ct:'F^`K711L STABFLTtF2 .
1. ♦.
f l z /u ^l•M9Y EA' 6j C, . I" , q z i H rx ^vIHG s rt J2 All Fl Ar ExTeNrtonr Lwncr Cn * f,.
fJ ^fsr:r r4AtH R OTOti Aximurn Posirma To 'en, 63 R. -A 1 0 ,6 O s i[ .r .• Ecxstsc r, •• CF 3a' ^^^^ q'l -b/t6 A Rte` R' 6 iI TO 5,KCErlJ r =r raja, d O A:-D -j . ?„rjZCnIA A ,:ry,, L ` :LT, 9? y ^51f6 O Dtj ABLa _.c V• .N' VE . :, Q4 t it 1555 M W r p FL-AT 9959 BArs AAO S— 1t.99 9. 9 1 -6/*(.
$r.
if C t'ttrELAGE AFI FB oI Y g s+ oew& [ 17.1!4 O 47 } jJ n W W4T Altar/7 r ct 1 CL D FE^e , E LxFatdc ritlY, j . SE A Coorws SCeSFItS. f] pr ^K:,EY'^"rXFtj+.i: j=^G7 r1[ b8 a QE ^i z ilfn ACjr9*rPWA ^^ t I.” S-rmoARp WiNo BAcx D,1, A74m VrcAx. D" GFAC 14rtAcrzp 14 JL 0 o cr Ot wt b GENERAT:CS b1sr, Lt ^ p C19 SUIC C-C ,r4VfZ-.1dC 1. +, 70 - 1 A -4 !+ O YCtTEx ^ + y 13 71 `( . }. 0 LANG iCAR7ti r, E p ar- F..4txtrt6s ArrAmep5 r c m c rivNtXATOt-_,Orr `Y^ ^.Zf 7 . e '70 rfn IV, , ^Je /Z fr/z 1) )Z=-IKSrAtL. MAIM J:oToR Vuicu CY[v :N.ET T ^7ttrl ► tr PttfL 7z A-Y, 13 ^et ^ y - s /.6 p tED Futt. S AR A.-.;) IS 73 - s ` QXWAAZ Ft; v rL COatt.IC :%10E9t(2 U)CUERE1i fad ... AFr To CF r -4 s 's' $,^ ^^ /f.G O +=;tFrr7G- REAaiE CAI;., INS-zitt. hltaa-Fzru +Rrr Ca4re-s f IT 1iuY, ro txrHa rtr 307 Hs R, Y } -^ l+^ F:^txtn ltlnt i Rp:er.
in O 13 71.
^s CoaPC^rS^ r tn