Wind tunnel test data for wing trailing vortex flow survey

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NASA TECHNICAL NASA TM X-62,148

MEMORANDUM

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N7 TEST DATA 6 2 1 4 8 ) WIND TUNNEL (NASA-TM-X- SURVEY N.-A.

FOR WING TRAILING VORTEX FLOW p CSCL (NASA) May 1972 94 Chigier, et al Unclas .01A 28200 _ G3/01 .

TEST DATA FOR WING TRAILING WIND-TUNNEL VORTEX FLOW SURVEY N. A. Chigier and V. R. Corsiglia Ames Research Center Moffett Field, Calif. 94035 May 1972 Reproduced by TECHNICAL NATIONAL SERVICE INFORMATION U S Department of Commerce Springfield VA 22151 WIND-TUNNEL TEST DATA FOR WING TRAILING VORTEX FLOW SURVEY N. A. Chigier* and V. R. Corsiglia** Ames Research Center ABSTRACT Data are presented on velocity measurements made with hot wire anemometers in the wake of a model of the CV-990 aircraft and a rectangular wing in the NASA-Ames 2.14x3.05 meter (7- by 10-foot) wind tunnels. Variables included angle of attack, tunnel speed and axial distance up to 12 chord lengths downstream from the wing trailing edge. Effects of deflecting trailing edge flaps and small spoiler panels are shown.

*National Research Council Senior Associate 1970-71.

Present address: Department of Chemical Engineering, University of Sheffield, England.

**Research Scientist lIl I NOTATION A,B,C constants in the polynomial fit to the calibration data, eqn 1 a core radius b wing span drag coefficient CD lift coefficient CL E,2 rms of the fluctuating component of anemometer voltage anemometer voltage corrected for tunnel temperature Ecor Em measured average anemometer voltage TI turbulence intensity, eqn 2 Tm measured tunnel temperature reference temperature for correcting anemometer Tref voltage, 30°C hot wire temperature, 200°C Tw U velocity component normal to each wire radial component of velocity Ur mean velocity components in wind tunnel co-ordinates, UX, uy, U z figure 1

/ Ux' ,\Uy 2 u -2

2 4 rms of fluctuating component of velocity y: UZ value of u at center of vortex x Uxmin swirl component of velocity ue maximum value of ue .

U max VCD free stream value of the velocity trailing edge flap deflection 6f .

INTRODUCTION Trailing vortices from large aircraft are known to persist for several minutes after generation and present a hazard to smaller air- craft which might intersect their path. Also, tip vortices which are shed from helicopter rotor blades present a distorted flow field to the following blade. This interaction between the rotor blade and the tip vortex of the preceding blade is a source of rotoS noise and vibra- tion. For these reasons it is desirable to develop an understanding of the vortex structure and dissipation, so that ultimately a means may be devised for reducing vortex velocities in the wake of wings and rotor blades.

The experiments discussed in the present report are a continuation of earlier work by the authors on the measurement of trailing vortices.

Reference 1 reports the effect (on the vortex wake) of a small spoiler on the tip of a rectangular wing and a Convair 990 aircraft. Reference 2 reports the results of detailed measurement of velocity with a three- wire hot wire probe in the wake of a rectangular wing model. The axial distance for this survey was varied from 4 chord lengths downstream of the trailing edge to the origin of the trailing vortex on the wing sur- face. In the present report the range of the variables for this same rectangular wing planform is extended to include axial stations up to 12 chord lengths and variations of angle of attack and tunnel speed.

Listings of the data presented in reference 2 are included in the present report.

In addition to the rectangular wing model a semi-span model of the Convair 990 aircraft was also tested. This model included wing, engine nacelles, anti-shock bodies, and a fuselage. The data for this model include variations of axial distance, angle of attack, tunnel speed and trailing edge flap deflection. The effect of a small spoiler panel, similar to that reported in reference 1 was also investigated.

Discussion of some of the results is given in reference 3. This report presents the complete test results without discussion.

i MODEL, APPARATUS AND INSTRUMENTATION The pertinent dimensions of the rectangular planform wing are given in table 1. A sketch of the CV-990 semispan model appears on figure 1; a detailed planform drawing appears on figure 2, and ad- ditional details are listed in table 1.

The tests were conducted in the Army and the NASA 2.14x3.05 meter (7- by 10-ft) wind tunnels at Ames with the semispan models mounted vertically from the tunnel floor. Surveys were obtained by attaching the hot wire probe to a survey apparatus permanently installed in the wind tunnel which allows the probe position to be varied remotely over the width and height of the tunnel and over about 3 meters (118 in) of test section length. The accuracy of the positioner is + 0.3 mm (0.01 in).

Force and moment data were obtained using a mechanical balance system. Tunnel speed was set with the aid of a pitot static tube mounted in the test section away from the flow field of the model. The vortex wake was surveyed with a triple sensor hot wire probe consisting of three wires placed in a three axis array. This array was operated by three separate constant temperature anemometers. Measurements were effectively averaged over a region 2 mm (x 0.08 in) in diameter. The frequency response of the hot wire anemometer system was well in excess of 30 kHz which was sufficient to measure the fluctuations which were encountered.

Calibration of the hot wire was accomplished by placing a small pitot static tube on the survey apparatus in the vicinity of the hot wire sensor. The hot wire data were corrected for tunnel temperature variations by use of a platinum resistance thermometer sensor placed in the test section.

TEST PROCEDURE AND CONDITIONS Traverses with the hot wire sensor were made through the vortex center both parallel to and normal to the spanwise direction at fixed axial stations downstream of the wing. An index of the test conditions at which the traverses were made appears in table 2.

Location of vortex center.- The vortex center was located by selecting the one of the three anemometers that was most sensitive to swirl velocity and recording this signal as well as the position of the survey apparatus on an X-Y recorder. A plot of swirl velocity vs traverse position could be generated by moving the survey apparatus while recording the signals. At a fixed axial station and normal posi- tion a spanwise traverse was made. From the resulting signal trace an the vortex center was made. Then, estimate of the spanwise position of made at this fixed spanwise center location to a normal traverse was the vortex center. The pro- determine a corrected normal position of further corrections to the spanwise and cedure was continued until no normal position of the vortex center were required.

Traverses.- After the location of the vortex center was determined each of the survey the traverse was performed by locating the probe at points across the vortex. The D.C. average and rms of the voltage signal was recorded with the averaging time as high as about 30 seconds in the vicinity of the vortex core where the turbulent fluctuations were large.

Calibration.- A calibration of the hot wire was made several times each day. For the calibration, the angle of attack was set to 00, the probe was moved away from the disturbance of the model, and a series of tunnel speeds were set. At each tunnel speed the output of the anemome- of the pressure difference on the pitot static tube, and ter, the value the tunnel temperature were recorded.

DATA REDUCTION AND CORRECTION The mean voltages read from the anemome- Temperature correction.- the following ter were corrected for the tunnel temperature according to expression: Ecor = Em2 T Tref Tw TM The wire temperature and reference temperature were 200 C and 30°C respectively.

Calibration.- The anemometer was calibrated by recording tunnel velocity and anemometer voltage for a series of tunnel velocity settings.

The following polynomial was used as a least-square fit to the data Ecor = A + B (u2) + C ( )2 (1) the known for each of the three anemometers. For the calibration, u is component of the tunnel velocity normal to the wire.

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Mean velocity.- The mean velocities in wing co-ordinates (figure 1) were obtained from the velocities relative to co-ordinates fixed to the probe using a transformation of co-ordinates and the known orien- tation of the probe relative to the wing. These velocities in the probe co-ordinates were, in turn, obtained from the velocities normal to each wire and the known geometry of the three wire array. The velocity normal to each wire was obtained from the corrected wire voltage and the inver- sion of equation 1, as follows: U -B + /B2 _ 4C (A - Ecor 2 ) = 2C It is assumed by use of this expression that the component of velocity parallel to the wire results in no contribution to the wire voltage.

Data published by the manufacturer of the anemometer indicates that this is a realistic assumption.

Turbulence intensity.- The turbulence intensity is defined as TI = Uy +U 2 (2) (2 + u 2 + u 2) 2 The rms of the velocity component fluctuations was obtained from the rms of the fluctuating voltage signals that were measured. The rms of the velocity normal to each wire is (u ½ = u (E )½ DE The factor au/3E is the slope of the calibration curve evaluated at the measured mean voltage. The rms of the velocity components in wing co- ordinates was obtained from the rms of the velocity normal to each wire using the same transformation as was used for the mean velocities.

RESULTS A list of traverses is given in Table 2 with the following column headings: Traverse Number Type of Traverse - Normal (Horizontal) of Spanwise (Vertical) a angle of attack of wing in degrees x axial distance in inches from trailing edge at wing tip x/c axial distance normalized by mean wing chord V wind tunnel velocity in ft/sec The 'remarks' column shows the type of model used and whether flaps or the panel was fitted to the model.

Location of the hot wire sensor is given in terms of counter readings.

The location of the wing trailing edge at the wing tip, which is chosen as the origin of the co-ordinate system, and the wind tunnel centerline was determined by placing the sensor at these positions and recording the counter readings. These measurements are shown in Table 3. It should be noted that the location of the wing trailing edge at the wing tip is changed when the angle of attack of the model is changed. These counter readings (Table 3) are used in order to give the position of the vortex centerline and velocity distributions relative to the wing and wind tunnel walls.

The normal, spanwise and axial velocity components and turbulence intensity at each measuring point are tabulated in Table 4 and Table 5 gives the key to the traverse and column headings.

Figures 3-7 show the variation of the principal parameters, uemax, a, Uxmin and TImax as a function of variation of angle of attack, a, for both the CV-990 model and the rectangular wing.

Discussion of these results is given in reference 3.

Force Data Force data as measured on the wind tunnel mechanical balance system are presented in figures 8-9. These show the variation of lift coefficient as a function of angle of attack and the drag vs lift coefficient curves for the CV-990 model.

REFERENCES 1. Corsiglia, V. R., Jacobsen, R.

A., and Chigier, N. A.: An Experimental Investigation of Trailing Vortices Behind a Wing With a Vortex Dissipator.

Aircraft Wake Turbulence and its Detection by J. H. Olsen and A. Goldburg, Plenum Press, New York-London, 1971, pp.

229-242.

2. Chigier, N. A., and Corsiglia, V. R.: Tip Vortices - Velocity Distributions, 27th Annual National V/STOL Forum of the American Helicopter Society, Washington, D.C., May 1971, paper 552.

Reprinted as NASA TM X-62,087, September 1971, pp. 1-13.

3. Chigier, N. A., and Corsiglia, V. R.: Wind Tunnel Studies of Wing Wake Turbulence, AIAA 10th Aerospace Sciences Meeting, San Diego, California, January 17-19, 1972. Paper 72-41.

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TABLE 1 - MODEL GEOMETRY CV-990 wing 91.5 cm (36 in) Semispan Reference chord, c = S/b 31.5 cm (12.4 in) 6.2 Aspect ratio Incidence root 40 2 ° tip Section root NACA 0011-64 NACA 0008-64 tip Trailing edge flap type, plain deflection 270 Rectangular wing 121.8 cm (48 in) Semispan Reference chord 45.7 cm (18 in) Aspect ratio 5.33 Twist Section NACA 0015 TRAVERSE INDEX TABLE 2 - ca x VV.

Remarks x/c ft/sec degrees inches Traverse Type CV-990 Model 147.0 11.85 100 4 3 Norm C = 12.4 in 147.0 11.85 100 4 4 Span 147.0 11.85 100 12 N 147.0 11.85 100 12 S 11.85 100 16 147.0 7 N 11.85 100 16 147.0 S 11.85 49 8 147.0 9 N 11.85 49 8 147.0 S 11.85 138 8 147.0 11 N 11.85 138 8 147.0 12 S 147.0 11.85 184 8 N 147.0 11.85 184 8 14 S 2.54 100 8 31.5 15 N 2.54 100 8 31.5 16 S 78.2 3.89 100 8 N 48.2 3.89 100 8 S 5.91 100 73.2 8 N 73.2 5.91 100 8 S 98.2 7.92 100 8 N 7.92 100 8 98.2 22 S 123.2 9.94 100 23 N 9.94 100 8 123.2 24 S 11.85 100 8 147.0 25 N 11.85 100 8 147.0 26 S 11.85 100 8 147.0 Panel on N 11t.85 100 - .

147.0 8 28 S 100 Flaps, 147.0 11.85 panel off 8 29 N 11.85 100 8 147.0 30 S 11.85 4 147.0 31 N

11.85 100 )1

4 147.0 32 S

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TABLE 2 - Concluded.

x.

V.

inches x/c Remarks Traverse Type degrees ft/sec ° 147.0 11.85 100 Flaps 0 , panel on 4 33 N 147.0 100 11.85 34 S 4 100 Rectangular plan- 162.0 9.0 35 N 12 form wing 162.0 9.0 100 36 S 12 C = 18 inches 9.0 162.0 100 37 N 8 162.0 9.0 100 38 S 8 162.0 9.0 100 39 N 4 162.0 9.0 40 S 4 3.76 159 -41 N 67.7 8 67.7 3.76 42 S 8 72.0 4.0 100 Rectangular plan- 101 N form wing 72.0 4.0 100 102 S 12 C = 18 inches 36.0 2.0 100 103 N 12 36.0 2.0 100 104 S 12 0 100 105 N 12 0 100 0 106 S 12 -4.5 -0.25 100 107 N 12 -4.5 100 -0.25 108 S 12 -9.0 -0.50 100 109 N 12 -9.0 100 -0.50 110 S 12 -13.5 -0.75 100 111 N 12 I - -13.5 -0.75 100 112 S 12 lo TABLE 3 - COUNTER READINGS FOR WING TRAILING EDGE AT THE WING TIP AND FOR WIND TUNNEL CENTERLINE (Scale: 1.0 count = 2.54 cm (1.0 in)) CV-990 Model (Trav 1 to 34) Normal Survey Tunnel centerline 45.95 Wing trailing edge at tip a deg position 4 47.76 8 46.14 12 44.45 16 42.95 Spanwise Survey Tunnel centerline 45.63 52.30 Wing trailing edge at the wing tip Rectangular Wing Model (Trav 35 to 42) Normal Survey Wing trailing edge at the wing tip a deg position 4 45.30 8 44.75 12 44.12 16 43.56 Spanwise Survey Wing trailing edge at the wing tip 64.51 Traverses 1 to 42 correspond to measurements made in the Army-Ames wind tunnel. Traverses 101-112 correspond to measurements made in the NASA-Ames wind tunnel. This explains the difference in the form of the counter readings from xx.xx to 9xxxx.

TABLE 3 - Concluded Rectangular Wing Model (Trav 101 to 112) (Scale: 100 counts = 2.54 cm (1.00 in)) Normal Survey Trav 101 to 108 Tunnel centerline 95411 Wing trailing edge at tip 95073 Trav 109 to 112* Tunnel centerline 91929 Wing trailing edge at tip 91591 Spanwise Survey Trav 101 to 106 Tunnel centerline 95895 Wing trailing edge at tip 95320 Trav 107 to 108 Tunnel centerline 96205 Wing trailing edge at tip 95630 Trav 109 to 110 Tunnel centerline 96180 Wing trailing edge at tip 95605 Trav 111 to 112 Tunnel centerline 96155 Wing trailing edge at tip 95580 *Zero setting on counter was changed to give the values shown.

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TABLE 4 Tabulation of results (Listing of Traverses 3 - 42 101 - 112) KEY TO TABULATED RESULTS Traverse Number TRAV Normal traverse NORM Spanwise traverse SPAN Axial distance in inches from wing trailing edge X Axial distance from wing trailing edge normalised X/C by mean wing chord ALF ALPHA, angle of attack, a Wind tunnel free stream axial velocity in ft/sec, V= V, FPS VORTEX CENTER Location of vortex center for that particular traverse - corresponds to position of zero tangential velocity. The numbers refer to readings in inches on the traversing mechanism counters DIST INCH Readings on traversing mechanism counters in inches (for traverse numbers 101-112 the values are given in hundredths of inches) NORM Normal component of velocity / V, SPAN Spanwise component of velocity / V.

AXIAL Axial component of velocity / V, + y,2 (ux ' + uz' ) TURBUL INTENS Turbulence Intensity (ux2 + Uz2)% + Uy

y'

Note: For NORMAL TRAVERSE = ur/V%, radial component NORM SPAN = us/V(, tangential component axial component AXIAL = ux/V~, For SPANWISE TRAVERSE NORM = ue/V., tangential component = Ur/V., radial component SPAN AXIAL = ux/V., axial component

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:i TRA.V03 ·NORM X=147.0 ALF = 4-. V, FPS=100. I; VORTEX CFNTFR=49.1 0 - v NORMALIZED VELCTTY TU R f lIL DIST NORM S PA I AX I AL T TEFNS INCH 0.9946 0.0096 0.0004 ). 00409 7.50 n.9953 0.00411 0.0092 0.0030 20. 00 0.0086 0.0033 0.9968 0. 00442t 25.00 I ?

0.0090 0.006 5 0.995.- 0.00(42P 30.00 (]. 9y 93 O. 00417 0.0065 0o. 0088 35.00 -0.0016 0,0093 0.9933 0. OO803 40.00 -0.0029 0. 0101 0. 992 0.00763 42.00 -0.0003 0.0094 0,.9909 () 015R I81 44.00 0.0038 0.0109 0.9R88 0.01322 k.,' 45,00 46.00 0.0064 0.0155 (.9905 0.01113 0.0089 0.0203 0.9 930 0. 01398 47.00 n. 985s 0.02940 i,_ 48.00 -0.0019 0.0 257 0.0069 0.0129 0.9746, 0.0015s 49.00 -0.0 184 0.9762 0.()326 50. () 0.0278 0.0207 -0.0268 0.9977 0.018a2 51.00 0.0121 n, 9964 O. 0 1 298 -0.0316 52.00 0.0081 -0. 0301 0.9988 0.00770 '53.(00 0.00 53 -0.02a9 54.00 1. 0119 0.0060 2 0. 0056 -0.0275 1.0 no 11 0.00476 56.00 0.0065 -0.0210 1, 0n .9 0.()00436 58.00 0.0080 -0.01 P6 ] 0n()40n . n456 60.00 0.00 65 -0.0157 1. .01] 0.r046 5 62.00 0.0075 -0. 0146 65.00 1.0027 0.00485 70.00 0.0062 -0.0 127 0.0'042 -0. 0102 1.005 0.004771 .75.00 0.0049 -O.00R2 1.0000 0. 00'604 R4. 50 NOT REPRODUCIBLE --- _ X=147.0 ALF= 4. TRAVO4 SPAN V,FPS=-100.

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\/VORTEX CFNTFR=50.60 ......... _NORMALIZED VELOCITY DIST T R I L INCH NORM SPANl AX JAl_ II'NS 11.00 0.0233 0.0141 O. P899 0.08065 1,5.00 0.0238 0.0218 0.9266 0.06349 0.05(65 2-0 00 0.0242 0.0264 0.9305 25s.00 0.0055 0.0134 0.9746 0.03321 30.00 0.0090 0.0018 0.9875 0.00584 35.00 0.010o -0.0019 0.9951 0. 0 443 40.00 0.0122 -0.0019 0.990R 0.006n0 42.00 0.0071 -0.0053 0.995] k.., 43.00 0.0129 -0.0023 0.9933 0. 005 21 0.0051029 44.00 0.0148 -0.0017 0.0?93 45.00 0.0156 -0.0018 0.9<0o0 _. ,, 46.00 0.0187 -0.0017 0.9R82 0.006568 47.00 0.0258 -0.0027 0.9876 0. 01278 4R.00 0.0337 -0.0048 0.-9P3i, 0.02350 -0.0271 0.9,(69 0.03 952 k,, 49.00 0.0208 50.00 -0.0040 -0.0334 0.9900 0.04693 51.00 -0.0152 -0.0263 0.9994 0. 0358 ( k_ ., 52.00 -0.0393 -0.0233 n.906P ('). 0327° 53.00 -0.0446 -0.0149 1.(07(7 0.0()612 54.00 -0,0368 -0.0112 1.0no4 . ss55.00 -0.0350 -0.0098 1.. o36 0. 007490 57.00 -0.0316 -0.0080 1. o 17 0.00496 60.00 -0.0267 -0.0074 1.0 (29 0 .0 00463 65.00 -0.0238 -0.0035 1.0021 0. 0047 2 72.40 -0.0116 -0.0086 1.0027 0.00474 ................... ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~. .__ .... __... _...

TRAV05 X=147.0 NORM ALF=12. V ,FPS=100.

VORTEX CENITER=51..00 NORMALIZED VELnCITY DIST TUIRBUIL INCH NORM SPAN AXIAL IN TENS 8.00 0.0041 0.0166 0.995) 0.00529 15.00 0.003 6 0.0194 0.9984 0.00510 0.9941.

20.00 0.0015 0.0206 0.00502 25.00 0.9937 0.00532 0.0025 0.0237 0.9944 0.00643 30.00 -0.0084 0.0284 32.00 0.9986 0.0083?2 -0.0141 0.0307 34.00 -0.0157 0.0336 1.0006 0.01514 36.00 0,.9931 -0.0223 0.0399 0.03035 38.00 -0.0309 0.0391 0.985Q 0.04298 40.00 -0,0343 0.9741 0.04844 0.0321 41.00 -0.0343 O.9730 0.0315 0.05421 -0.0361 0.0306 0.9656 kv 42.00 0.05882 43.00 -0,0425 0.9608 0.0293 0.06090 44,00 -0.0418 0.0276 0.9540 0.06646 45.00 -0.0422 0.0322 0.9540 0.06889 46.00 -0.0476 0. 0236 0.945? 0.07284 47.00 -0-.0550 0.0176 0.9300 0.07933 48.00 -0.0556 0.0125 0.9275 0.08249 49.00 -0.0591 0.0056 0.9241 0.08573 0.9244 50.00 -0.0657 -0. 0086 0.08043 51.00 -0.0589 -0.0228 0.9378 0.07563 52.00 -0.0576 -0.0316 0.9466 0.06801 53.00 -0,0446 -0.0395 0.9548 0.05238 -- 54.00 -0.0380 -0.0476 0.9728 0.04714 55,00 -0.0360 -0.0437 0.9820 0.03325 56.00 -0.0340 -0.0421 0.9877 0.02786 57.00 -0.0265 0.9944 -0.0415 0.01921 58.00 -0.0194 -0.0376 0.9977 0.01388 59.00 -0.0145 -0.0355 0.9991 0.01130 60.00 -0.0140 -0.0352 0.9986 0.00863 62.00 -0.0113 -0.0324 0.9972 0.00767 64.00 -0.0113 -0.0289 1.0017 0.00656 66,00 -0.0102 -0.0240 1.0051 0.00546 68.00 -0.0074 -0.02 25 1.0029 0.00560 70.00 -0.0064 -0.0230 1.0011 0.00521 75.00 -0.0020 -0.0188 1.0008 0.00552 84.50 -0 .0010 -0.0144 0.00661 1.0000 j· ·IIIC·UI·LII---L--- __ TRAVO6 X=147.0 ALF=12. V, FPS=- ].O. SPAN VORTEX CFNTER=47.50 NORMALIZED VELncTTY D IST TlIRBIIL INCH NORM SPAN A^X AL TNTEFNS 11.00 0.0622 0.0357 n.R501 0.1.4988 15.00 0.0604 0.0344 n.9088 0.10153 20.00 0.0328 0.0173 n.9452 0.05231 25.00 )0.0162 0.0078 0.9749 p.02819 30.00 0.0325 - 0. 00R6- .9 0 .969 0477n 32.n00 0.0364 -0.0098 0.9594 0. 05949 34.00 0.0367 -0.0083 n.9540 0.06635 36.00 0.0340 -0.0150 0.9448 0.06997 38,00 0.0310 -0.0150 0.9466 n.06952 40.00 0.0307 -0.0112 0.9581 0.06731 41.00 0.0296 -0.0112 0.9575 0.06579 k,.., 42.00 0.0331 -0.0109 0.9534 0.07008 43.00 0.0362 -0.0157 0.9469 0.07311.

44.00 0.0390 -0.0146 0.9409 0.07946 45.00 0.0379 -0.0170 n.9224 N.09059 46.00 0,.0231 -0.0248 0.9(76 .0n9()4n0 47.00 -0.0020 -0.0239 n.896? 0.0!13.

48,00 -0.0178 -0.0262 0.8943 0.09598 49.00 -0.0294 -0.0279 0.9n019 0.09207 50.00 -0.0405 -0.0243 0.9074 0.08637 51.00 -0.0489 -0.0207 0.9190 0.07622 52.00 -0.0603 -0.0184 0.9476 0.06454 53. -- C -05704 ..- (Y.-37 4t. 05, ... 6 54.00 -0.0610 -0.0084 n.9692.

0.04512 55.00 -0.0572 -0.0089 n.9749 0.02938 56.00 -0,0570 -0.0058 0.9745 0.02367 57.00 -0.0483 -0.0086 0.9887 0.01.847 58.00 -0.0439 -0.0067 n.9872 0.01115 59.00 -0.0461 -0.0055 -0.9895 0.0o10.o 60.00 -0.0440 -0.0042 0.9909 0.00726 62.00 -0.0399 -0.0035 0.9957 0.0058.3 64.00 -0.0338 -0.0012 0.9899 0.00565 66.00 -0.0343 -0.0003 0.9893 0.00513 68.00 -0.0333 0.0009 0.9908 0.00548 70.00 -0.0311 0 0016 0.9904 0.00544 72.45 -0.02R5 0.0007 O.9q91 0.00509 - - I I., a "I 1 1 I 11 II . - I i . ., . I I .1 . . _I ^ - I .

X=147.0 ALF=16. V, FPS=100. TRAV07 NORM . .....

VORTEX CENTER=50.50 NORMALIZED VELOCITY n IST TORRIIL AX IAL

!%./ INCH NORM SPAN I NT ENS

8.00 0.0026 0.0227 1.0084 0. 00528 15.00 -0.0011 0.0212 1.0138 0.00515 0. 0241 1.0139 0.00567 20.00 -0.0006 25L 0 _ -0.0043 0.0213 1.0171 0.00606 30.00 -0.0107 0.0226 1.0166 0.00839 0.0247 1.0143 0.01149 32.00 -0.0155 0.01236637 34.00 -0L0218 0. 2h6J__ 1.0151 36.00 -0.0251 0.0253 1.0161 0.02366 .38.00 -0.0276 0. 0268 1.0127 0.03689 40.00 -0.0323 0.0263 1. 0066 0.04744 0.05339 41.00 -0,0353 0.0273 0. 9984 0.9945 0.05659 42.00 -0.0383 0.0252 0.0259 0.9747 0.06872 43.00 -0.0388 0. 9719 0.07656 44.00 -0.0414 0.0218 45.00 -0.0401 0.0221 0.9615 0.07880 46.00 -0.0454 0.0197 0.9537 0. 08626 47.00 -0.0436 0.0168 0.9423 0.09161 0.0062 0.9425 0.09259 48.00 -0.0484 49.00 -0.0471 -0.0051 0.9265 0.09313 -0.0172 0.9197 0.09183 50.00 -0.0482 51.00 -0.0442 -0.0205 0.9178 0.09088 52.00 -0.0460 -0.0311 0.9185 0.08889 53.00 -0.0398 -0.0438 0.9258 0.07657 0.9553 0.06265 54.00 -0.0429 -0.0496 0.9752 55.00 -0.0360 -0. 0496 0.05325 0.9830 56.00 -0.0329 -0.0486 0.04308 _. 57.00 -0.0292 -0.0491 0.9912 0.03363 58.00 -0.0184 0.9976 0.02680 -0.0474 1.0027 59.00 -0.0167 -0.0449 0.02265 60.00 -0.0123 -0.0406 1.0017 0.01486 62.00 -0.0118 1.0042 -0. 0361 0.00995 1.0019 64.00 -0.0091 -0.0327 0.00727 66.00 -0.0085 -0. 0301 1.0064 0.006n8 1,0055 0.00586 68.00 -0.0074 -0.0294 1.0024 70.00 -0.0025 -0.0254 0.00583 1.0024 , 775.00 -0.0009 -0.0226 0.00556 0.002R 1.0000 0.00614 R4. 50 -0.01R86 j . , ; TRAV08 SPAN X=147.0 ALF=16. V FPS=100.

VORTEX CENTER=47.50 NORMALIZED VELOCITY DIST TIJRBUL 4 L. INCH NORM SPAN AXIAL INTENS 11.00 0.1038 0.0602 0,9482 0.0849 7 15.00 0.0609 0.0253 0.9720 0.06807 20.00 0,0359 -0.0022 0.9838 0.06243 25.00 0.0455 -0.0304 0.9327 0.08903 30.00 0.0425 -0.0377 0.9179 0.09072 . R32.00 0.0343 -0.0442 0.9260 0.08827 34.00 0.0280 -0.,0447 0.9380 0.08545 36.00 0.0233 -0,0419 0.9604 0.08025 38.00 0.0228 -0,0376 n.9654 0.07481 40.00 0.0233 -0.0349 0.9660 0.07272 41.00 0,0265 -0.0338 0.9650 0.07546 k.~ 42,00 0.0297 -0,0315 0,.9660 0.07543 43.00 0.0330 -0.0363 0.9531 0.08507 44.00 0.0286 -0.0355 0.9451 0.08744 ,^ r 45.00 0.0245.

-0.0348 0.9308 0.09249 46.00 0.0140 -0.0399 0.9168 0.10111 47.00 0.0057 -0.0311 0.9067 0.10165 . 48.00 -- 0.02.17 -0.0387 0.9131 0.10022 49.00 -0,0257 -0.0364 0.9111 0.09928 50.00 -0.0415 -0.0326 0.9193 0.09413 , s51.00 -0.0465 -0.0281 0.9353 0.08130 52.00 -0.0520 -0.0238 0.9468 0.07539 -t 53,0 -00556-:0--.0 .o99 .9612....

0.07031 54.00 -0.0568 -0.0158 0.9693 0.06358 55,00 -0.0590 -0.0092 0,.9767 0.04736 56,00 -0.0478 -0.0129 1.0007 0.04212 .I 57.00 -0.0469 -0.0123 1.0070 0.03169 5R.00 -0.0436 -0.0104 1.0043 0.02631 59.00 -0.0436 -0.0092 1.0071 0,.01749 60,00 -0.0425 -0.0048 1.0088 0.06186 62.00 -0.0298 -0,0090 1.0213 0.00888 64.00 -0.0292 -0.0080 1.0200 0.00665 66.00 -0.0265 -0.0077 1.0182 0.00561 68.00 -0.0243 -0.0089 1.0172 0.00610 70.00 -0.0215 -0.0054 1.0150 0.00574 72,45 -0.0166 -0.0039 1.0120 0,00562 72,45 -0.0171 -0.0067 1.0107 0.00563 IHC900I EXECUTION TERMINATING DUE Tn ERROR COUNT FOR ERRnR NUIIBFRR ...- ~: -RA.ViNxR±fl/AVORTEX CFNTER=51.70 VORTEX CFNTER=51.70 ITTY NO RMAL17:ED VFCI _- - Il ST TURBUJL INCH NORM : SPANI AXIAL INTENS _4D.on ....... _ 0014_ _0._O_ . l..__.0 50 ...

... 2244 . ....

42.00 0.0161 0.0092 0,9726 0.03794 ~C, 44.00 0.0159 0.0071 0.9689 0.04529 4 -40D_ .. __Q 1i2S Q. 0041 Q_6....

47.00 0.0094'. 0.0017 0.9680 0.05034 k. 48.00 -0.0014 0.0051 0.9612 0.04917 __4_9_ _0 ... .... -0,00 _1 __.L4 00_/__O 2 ........ 19661...... .... 0.0552_..... . .......................

50.00 -0.00(92. -0.0018 0.9689 0.06030 L- 51.00 -0.0160 -0.0258 0.9517 0.06056 !~_._2. .0 0 . 0_ 42._ -0, 0396 0,941_......

. _k_0_q6049. ........

53.00 -0.0043 -0.0416 0.9426 0.06829 , .' 54,00 -0.0095' --0.0525 0,9474 0.05742 _ 5a ) ._.__Q..,,DO__-- oQ562___.2 ....... ........

Q0_37.6 0.......

58.00 0.0191 -0.0648 0.9830 0.02685 j %,, 60. 00. 0.0267 -0.0599 1.0000 0.01396 I - .TBLR ._seQ_ .. .. X.14_7,. ALF= 8,. V,_S- 49. _2-.

VORTEX CENTER=48.00 NORMALIZED VELOCITY DIST TLJRBIJL ~' - INCH NORM SPAN AXIAL I NTE N S I 40,00 0.0664 -0.0246 0.9646 0.06415 42.00 0.0799 -0.0331 0.9737 0.06783 44.00 0,0820 -0.0180 0,9699 0.06815 46.00 0.0896 -0.0327 0.9702 0.069 86 47.00 0.0407 -0.0180 0.9387 0.08044 L- 48.00 0.0270 -0.0128 0.9314 0.08266 49.00 0.0044 -0.0102 0.9481 0.06200 50.00 -0.0130 -0.0202 0.9701 0.06089 _-- 51.00 -0.0173 -0.0180 0.9783 0. 04941 52.00 -0,0149 -0.0232 0.9901 0.03641 53.00 -0.0148 -0.0204 0.9938 0.03144 i .' 54.00 -0.0083 -0.0255 0.9929 0.01610 56.00 0.0096 -0.0250 1.0073 0.01096 58.00 0.0142 -0.0226 1.0054 0.00872 i k. 60.00 0.0161 -0.0259 1.0085 0. 00632 e .s .1I : r , r ·; *1 r;, , TR V l- _-, - QM__X -NRm _ .. _.ALE =- .- 8 ... . .. V. .. ES.-3._8..

VORTEX CENTER=50.00 - _.... _:.E _ __ EDYLQ___C LIY...... .

DIST TUIR13UJL

i i

INGHC. NORM SPAN AXIAL I NTE N S .__4QQOQ .. OQ ,7.' -. .o 2_Q 2.. ... 0, 9.8.01. .. .0..038 .8....

42.00 0.1041' -0.0392 0,9716 0.06096 ,., 44.0..0. 0.1023' -0.0398 0.9673 0.04949 i .-f ,l 001 0 :.10 1' -- , 0366._0.7_76_ 0,o 099'5 47.0 -0.0291 0.9734 0.05524 O i 0o 0923 -0,0365 0.9279 0.07315 49,00 n-fORQ9- -nA n 3 _. 93A ... _C_ .0b8_63 .: 0:.0:824 -0. 0941 0.9023 0.07501 50.00 1 V 0.1052 0.9218 0 .06513 51.00 -0.1180 _0 ,. 11 1: __965-6.

t .i 0.1266 -0.1372 0.9784 0.03813 53.00

54.00 1

0,.1-282 -0*. 1301 0. 9917 0.02 877 '-l' 11 I _ A A :l__ I·Aml ', 0...a.15 74. Q5K.-QOD_ ; r E

7.,.,'

t

i _ v ·I :.

TaAIL~a ~ ALF=. 8" V. .P 138. _ , - *D -i '~i' IZA,, _ " ~.' _S.. ....... PIF.. . -_X -147 C0.,_.. . A 0L F.- . R _ .. .

' '! ' " %11'~ O T r- Vt'" r" I%1 T [ChTD -- / . O n VU I CA .U,,I EC ::-=14H* r '1 L&J .1 V FLQNCTlTY NnRMAL TZFD DIST TUR B IJL I· INCH NORM SPAN AXIAL INTENS

"_35.00 _1L99Q0 0_,03092

__ 0.15.90__ - -0O7_7J8.

40,00 0.1623 -0.0803 0.9888 -0.05126 42 00 0.1638 -0.0782 0.9874 0.04597 - 90, 08:90, 1................0 ....... ...........

46*,00 0.2069 '-0. 0964 0.9877 0.04603 47 .00 0,1995 .- 0.1051 0.9629 0.06592 -0. 1002 20 ,9228, .. _ 0.07312 49.00 0.1203 -0.0988 0.9096 0.07883 0.9259 0.06858 v... 50.00 0.0596 -0.0871 __. 0 .05 89 -0,.0774 0.9384 0.05604

51,00_

52,.,00 0. 0498 -0-.0686 0.9540 0.04399 _, 53:.00 0.0530 -0.0637 0.9734 0.03222 0.984 _ 0.01360247 I 566,00 0.0788 -0.0708 0.9833 0.01360 F . ... ___ ._..

' f i cI · D _ ,, Ii ; I ,.

J i. , V3 M TDAv1 "nl

.. LF .. ......... .FP__ .................. _2. = - -_.5-

_X-.L47._ L.

VORTEX CENTER=50.00 .. 1 - nCTTTY NIIRMAI T7Fn VFI TU(RBUL DIST SPAN AX I AL INTENS NORM INCH ,.053._ .. L.On 37 ...... 1.....10O..42 _ ....

-364.Q _... _... 1.-3 ...

, j 38 00' 0.1429 -0.0509 1.0130 0.02003 ..

40.00 0.1432 -0.0490 0.9980 0.03973 k sW ~~~__4~D1(1_ __~_1o.1 05-: I ~..O........E .......... 981 . ..... _ . .-.. _..._ 0.04914 44.00 0.1394 -0.0662 0.9932 0.04795 ; .' 46.00 0.1357 -0.0539 0.9901 9..7_ .. 979 ..... -- OE.1 .....

.__4. .-. _.__ _ .13Q5.-O.....

0.06507 48.00 0.1053 -0.0345 0.9444 0.07675 49.00 0.0959 -0.0524 0.9080 _50. O0 _Ql£Q.Q __02.,_ Q3_.. _ 0._._96.6. ... Q....... Q7729 .__ _ _.. .....

0.06991 5-1.00 0.1198 -0.1192 0.9119 0.05431 52.00 0.1315 -0.1432 0.9496 _.53_ ._ ..... .. .. __Q._L5__4 -... 1i12 09.... 99.3.6_. ..03.9Q9 _.

0.9996 0.03242 54.00 0.1582 -0.1465 0.02196 56.00 0.1607 -0.1348 1.0049

'. - 58.00 0.1625 -0.1213 1.0000 0.01404

ALF=. ,. V,FPS = .. 1. 84, _. __ _ .- RAi41... SP _ ... .. 147.0, ., VORTEX CENTER=48.50 /l'j __~_ ND.RkALI2ED.VELQUJY. . L-*,_ D IST TURBUL INTENS INCH NORM SPAN AXIAL ':...36_fL__ 0_._199.5 - 0.1O023 __..L._QO39. . O........11975.... ...

i' -0.1064 1.0104 0.04873 38.00 0.20'52,' 1.0101 0.05045 40.00 0.2'64 -0.1076 I- .0Q__ .... __.__9.1Q23,_ tQ. O 6 _,_ ___.0__,. . _. _0.9- ..... _.:_ 9_ ._ ...

!, 0.23'68 -0.1158 1.0242 0.04183 44.00 ?

1.0110 0.05472 46.00 0.2539, -0.1210 'LL0_ .....- __.0.4.2._12, 0..7...' .. ..... 0. ' ,0O6566.

0.08052 48.00 0.1793 -0.1118 0.9069 -0.0975 0.9034 0.07888 49.00 0.1166 500Q____i -0,o 864 Q92 94__ .9Q ..... 0._1 .

0.0776- -0.0834 0.9543 0.05419 51'.00 52.00 0.0773 -0.0847 0.9843 0.04490 i.

5,,,0_ ._, .... 0_920 - i844 0.996,3,_ , , ,0. 0295.4 54.00 0.0990- -'0.0855 0.9993 0.02322 56.00 0.1106 -0.0884 1.0108 0.01412 I .,, :i v

V

Fv

k,,, F· v ·i - ,. . .... - .

- - - - . - -8 - I -. --- - I- . - .

l TRAV1 5

X= 31 .5 ALF= 8. NORM 21

VFPS=00.

VORTEX CENTER=47.50 NORMALIZED VFELFCITV n IST TtJR hI !L Ik\CH NORM SPAN AX I AL IN FITENS 10.00 -0.0050 0.0114 o.9817 0. 00542 15.00 0.0068 0.0059 0.- .9i 2 20.00 0.0044 0.0070 n.9960 n.oonnl 0.00519 25.00 0.0056h 0.0090 0.9959 0.00 577 3n0.00 0.00n.O46 .0.0134 0 .9978 0 C 005q9 35.00 0.0036 0.0152 0.9979 0.o00543 36.00 -0.0014 O.01R1 0.s94f 37.no -0.0024 0.0277 1.Ono0 0. 00 5 A.n00 -0.0048 0.0211 0.998R 39.00 -0.0084 0.021.5 1.on02 0.00562 40.00 -0.0089 0.0247 n.999n 0. Or)663 41.00 -0.0103 n.noo ( l.

0.0253 1.o0n2 n.00661 42.00 -0.0113 0.0324 1. 0058 0. 00857 43. 00 -0.0219 0.0381 .nn0068 0.02043 44.00 -0.0355 0. 0485 1..0014 0.04730 45. 00 -0.0590 0.0 626 0.9675 0.0)7243 46.nn00 -0.071.2 0.0494 0. 9034 0. 10)2 4 47. 00 -0.0774 .0 6lhl1 n.9022 0. 11304t -0.0889 -0. 0195 0.9038 0 O. 098Q n-- . on -0.0619 -0.0h4h 0.9442 0.O8Q0476 90.00 -0.0450 -0. 0807 .95 11 0.0 76h ( l .n00 -0.0251 -0.0751 0. 9776 0. (06044 -'0'0'6 0.9 88 1. 0. 03934 53.00 -0.0159 -0.046 0. 9964L 2 ~.o01 554 94.00 -0.0170 -0.0421 0 . 999n 0. 0072 ' 56.00 -0.0144 0-.9994 -0 .03h9 -. 6-6 540 R .00( -0.0079 -0.0296 O .996-7 An. 00 -0.0067 -0.0264 0.9974 -0.0065 -0n.0238 0. 9972 0.00647 0.00567 h4.

00 -0.0041 -0.0212 0.9980 -0.0031 -0.0193 0.9997 O.00538 64. 00 -0.0031 -0.0169 6. O 00 1. 0015 0). 00524 -0.0016 -0.0161 0. 9985 0. 005 60 75.n00 -0.0o02! -0.o 114 1. 000(, 0. O) 5 &p ~-8. oo -0.0002 -0.0091 1. 000nO 0. 00563

- 01 ?EO DU OD

Cp :7 1 - ?. , ._I .

X= 31.5 ALF= TRAV16 SPAN

R. V,FPS=100. ._

.A; VORTEX CENTER=50.20 I i NORM ALIZED VELOCITY T lJRBI I L DIST NORM INCH SPAN AXIAL INTENS 11.00 0.0637 -0.0031 0.8313 0. 19092 15.00 0.0569 0. 0089 0.7920 0.19854 - , Q 20.00 0,0492 0.0184 0.9642 0.02057 25.00 0.0514 -0o,0074 0. 9433 0. 07537 30.00 0.0325 -0.0085 0.9221 0.08778 0.9538 35.00 0.0462 0.0089 0.07105 0.0515 -_,0_.0096 0.08794 36.00 0. 9521 37.00 0.0550 0. 0014 0.9250 0.10934 -_ , 38.00 0.0443 -0.0048 0.8945 0.12046 0. 8849 39.00 0.0345 -0. 0066 0.12 302 -0.0104 0.9071. 0.11940 40.00 0.0140 0.0048 -0. 0064 0.9196 0.10848 -iv 41,00 -0,0038 0.9354 42.00 -0,0023 0.09755 0.004,8 43.00 -0.0107 0.9597 0.07703 44.00 0.0210 -0.0094 0.9736 0.06114 -0. 0022 0. 04087 45.00 0.0293 0.9831 46.00 0.0501 0.0065 0.9863 0.03231 47.00 0.0641 0.0186 0.9855 0.03754 48.00 0.0835 0.0276 0.9620 0.06605 49.00 0.0808 0.0310 0.9210 0.09972 0.0201 0.0418 0.8536 0.11943 50.00 51.00 -0.0630 0.0339 0.8954 0.10920 0.9640 52.00 -0.0977 0.0279 0.06495 x., 53.00 -0.0905 0.0127 1. 0001 0.03466 -0.0772 0.00101 1.0010 0.01105 54.00 55.00 -0.0617 0. 0006 1. 0057 0.00726 56.00 -0.0492 -0.0028 1. 0039 0.00 561 57.00 -0.0373 -0.0050 1. 0063 0.00540 58,00 -0.0396 -0.0014 1.0092 0.00540 60.00 -0.0360 -0. 0017 1. 0070 0.00530 62,00 -0.0297 -0.0018 1. 0010 0.00528 64.00 -0.0262 -0.0021 0.9996 0.00573 66.00 -0.0267 -0o.0035 1.0034 0.00550 68.00 -0.0228 -0. 0006 1.0007 0.00538 70.00 -0.0148 -0.0072 1.0153 0.00560 72.40 -0.0117 -0. 0082 1.0162 0. 00539 TRAV17 NORM X= 48.2 ALF= 8. VFPS=100.

_ 2

VORTEX CFNTER=47.50 NORMALIZED VELOCITY DIST TURBIJL INCH NORM SPAN AXIAL INTENS 10.00 -0.0029 0.0159 0.9851 0.00483 15.00 -0.0023 0.0182 0.9859 0.00498 ,- t 20.00 0.0008 0.0162 0.9947 0.00510 25.00 0.0056 0.0155 0.9946 0.00509 30.00 0.0028 0.0189 0.9979 0.00498 32.00 0.0021 0.0198 1.0012 0.00519 34,00 0.0009 0.0197 1.0033 0.00537 35.00 -0.0024 0.0215 1.0037 0.00514 . .v 36.00 -0.0013 0.0241 1.0066 0.00520 37.00 -0.0019 0.0241 0.9984 0.00486 38.00 0.0069 0.0189 1.0096 0.00541 39.00 -0.0055 0.0252 1.0034 0.00584 40.00 -0.0072 0.0261 1.0049 0.00609 41.00 -0.0094 0.0290 0.9927 0.00714 ~.~ 42.00 -0.0183 0.0365 1.0143 0.01313 43.00 -0.0146 0.0408 1.0056 0.02884 44.00 -0.0205 0.0491 0. 9968 0.04081 '.

, < 45.00 -0.0254 0.0628 0.9785 0.06310 46.00 -0.0354 0.0618 0.9298 0.08048 47.00 -0.0365 0.0285 0.8569 0.09376 48.00 -0.0347 -0.0264 0.8631 0.09367 49.00 -0.0387 -0.0833 0.9224 0.07225 '50.0 -0029 -770 0.-047 51.00 -0.0239 -0.0748 0.9805 0.03950 52.00 -0.0220 -0.0645 0.9854 0.03823 53.00 -0.0139 -0.0468 0.9844 0.03056 54.00 -0.0125 -0.0413 0.9919 0.01767 55.00 -0.0093 -0.0353 0.9917 0.00686 56.00 -0.0067 -0.03 20 0-.99'10 0. 00-5'9-6 57.00 -0.0067 -0.0284 0.9935 0.00568 58.00 -0.0066 -0.0277 0.9920 0.00519 60.00 -0.0035 -0.0222 0.9921 0.00520 V.~ 65.00 -0.0036 -0.0186 0.9966 0.00516 70.00 0.0007 -0.0137 0.9948 0.00555 75.00 0*0034 -0.0097 0.9907 0.00508 i..- 8'2.50- -0.0015 -0.0050 1.0000 0.00568 N- P. V,FPS=)00.

TRAVIR SPAN X= 48.2 ALF= VnRTEX CFI\ITFR=5n.0(n NnRMALIZEO EL!C I TY TI IR I L Il- .ST NI\ORM SPAM. AX IAL TNT ENS INCH 1.1.00 0.13474 n0.0550 -0.0009 n.0.746 0.13068 15.00 0.0648 0.0140 n.8707 0, 003771 20.00 0.0415 0.0200 0.952c .2.5,0 0 0.0393 0.0060 0.9463 0.06594 3n.00 0.0299 -0.0059 n.9233 0.9431 0.057].8 35.00 0.0368 0.0050 .. 3nhQ_ - 0 4 3 01_ . ... 0..o0045 0n,.9 _,37 7 37.00 0.0459 0.0023 0.924n 0.08196 38.00 0.0406 -0.0005 0.9012 0.09430 0.09942 39.00 0.0372 -0.0054 0.890s9 40.00 0.0290 -0.0073 n.897R 0.09935 41.00n 0.0152 -0.0082 0.9134 0.09109 42.00 0.0101 -0.0041 0.9280 0, 08163 43.00 0.ol24 -O.0032 o.9 368 0. 06650 44.00 0.0262 -0.0041 0.9551 0.05293 0.0 4087 45.00 0.0336 0.0028 0.9590( 0.03435 46.00 ( 0.0405 0.0125 0.9636 47.00 0.0573 0.0250 0.9599 0. 04305 48.00 n.0760 0.0400 0.9427 n.06246 49.00 0.0589 0.0564 0.R891. 0. 07909 50.00 0.0056 0.0612 O.8651 0.0882P 0,08492 51.00 -0.0412 0.0477 O.8740 0.0706 8 '2.00 -0.0821 0.0338 0.91473 53.00 -0.0900 0.0255 0.9521 0.04724 0.02439 54,00 -0.0739 0.0147 0,96774 55.00 -0.0548 0,0059 0.9798 0.01022 0.0056h3 56.00 -0.0463 0.0031 0.9758 57.00 -0.0430 0.0016 0.9744 0.00508 58.00n -0.036 -0.0006 0.9819 0.00516 60.00 -0.0322 0.0004 0.9760 0. 00549 0.00538 65.00 -o.0283 0.0009 .09758 0. 00545 72.40 -0.0200 0.0021 n.9696 X= 73.2 ALF= 8. NORM TRAV19 VFPS=100.

VORTEX CFNTER=48.00 NORMALIZED VELnCITY DIST TURBIJL INCH INTENS NORM SPAN AXIAL .- 00077 0.9725 0.00470 10. 00 0.0113 0.0134 0.9734 0.00461 15,00 -0.0072 20.00 -0,0072 0.0135 0.9763 0.00466 -'-.

25.00 0.9776 0.00440 0.0162 _-0.0077 30.00 -0.0071 0.0184 0.9803 0.00440 32.00 -0.0052 0.0201 0.9809 0.00457 34.00 -0.0091 0.0215 0.9842 0.00460 35.00 -0.0096 0.0200 0.9855 0.00469 36.00 -0.0091 0.0209 0.9855 0.00473 37.00 -0.0115 0.0237 0.9893 0.00489.

38.00 -0.0125 0.0238 0.9923 0.00473 39.00 -0.0150 0.0230 0.9936 0.00523 40.00 -0.0160 0.0225 0.9961 0.00577 41.00 -0.0180 0.0225 .n,9992 0.00765 1.0027 0.01165 42.00 -0.0180 0.0251 43.00 -0.0194 0,0278 1.0029 0.01854 44.00 -0.0238 0.0385 1.0023 0.02718 0.9991 0.03470 45.00 -0.0311 0.0465 46.00 -0.0464 0,0598 0.9768 0.05290 47.00 -0,0539 0.0404 0.9197 0.06761 -0.0423 -0.0044 0.8679 0.07483 48.00 49,00 -0.0420 -0.0517 0.8772 0.06993 50.00 -0.0215 -0.0839 0.9457 0.05359 -0.0801 51.00 -0.0176 0.9812 0.03392 52.00 -0.0123 -0.0670 0.9903 0.01900 53.00 -0.0055 0.9948 0.01581 -0,0543 54.00 -0.0034 -0.0484 0.9925 0.01519 55.00 -0.0024 -0.0421 0.9976 0.01227 56.00 -0.0029 -0.0383 0.9976 0.00788 57.00 0.9965 0.00619 -0.0003 -0.0363 59.00 1.0008 0.00552 -0.0008 -0.0337 60.00 0.0028 -0.0311 0.9970 0.00518 62.00 0.0002 -0.0296 0.9999 0.00539 64,00 0,0023 -0,0243 1.0012 0.00573 66.00 -0.0243 0.9999 0,0033 0.00514 70.00 0.0054 -0.0196 1.0026 0.00500 75.00 0.0063 -0.0 148 1.0004 0.00496 80.00 0.0073 -0.0136 1.0000 0.00517 TRAV20 SPAN X= 73.2 ALF= R. V, FPS= 1 0('0.

.. . ._ VORTEX CFNTFR--49.70 NORMALIZED VELOCITY fDIST TURBR()L INCH NORM SPAN AXIAL INTEN S 11.00 0.0330 -0.0052 0.8770 0.12372 .

15.00 0.0479 0.0175 0.9561 0.07307 20.00 0.0383 0.0153 0.9437 0.05944 25.00 0.0276 0.0062 0.9728 0.03283 _ 30.00 0.0254 -0.0069 0.9586 0.04765 35.00 0.0304 -0.0017 0.9637 0.04593 I,- 40.00 0.0242 -0.0154 0.9310 0.07617 42.00 ]0.0154 -0.0090 0.9328 0.06907 43.00 0.0113 -0.0027 0.9472 0.06213 44.00 0.0297 -0.0045 0.9678 0.05384 45.00 0.0387 0.0007 0.9624 0.04913 46.00 0.0515 0.0139 0.9622 0.04753 _ 46.50 0.0561 0.0141 0.9568 0.04885 47.00 0.0629 0.0146 0.9443 0.05195 47.50 0.0668 0.0121 0.9295 0.05658 I-- r 48.00 0.0556 0.0274 0.9067 0.06558 49.00 0.0242 0.0355 0.8925 0.07124 50.00 -0.0219 0.0476 0.8815 0.07337 1-- 51.00 -0.0658 0.0374 0.9166 0.067R3 52.00 -0.0826 0.0311 0.9382 0.05358 52.50 -0.0865 0.0238 0.9485 0.04444 53.00 -0.0841 0.0206 0.9613 0.04010 53.50 -0.0809 0.0170 0.9621 0.03.411 54.00 -0.0711 0.0119 0.9679 0.03033 54.50 -0.0646 0.0076 0.9723 0.02488 55.00 -0.0628 0.0077 0.9757 0.02236 56.00 -0.0568 0.0037 0.9737 0.01015 57.00 -0.0521 0.0070 0.9703 0.00609 _ 58.00 -0.042R8 0.O045 0.9700 0.00487 60.00 -0.0355 0.0003 0.9752 0.00492 62.00 -0.0305 -0.0014 0.9751 0.00509 64.00 -0.0270 :0.0000 0.974R 0.00531 66.00 -0.0265 -0.0014 0.9756 0.00564 70.00 -0.0260 -0.0017 0.9778 0.00594 - - _... ... .. ;.. . .. ._ _. _ . . .. _. -. .-. .

---- - --- -~- -^- -- ~ TPA L2 1 NORM X= 98.2 ALF= R. VtFPS=-00...

VORTEX CENTER=48.20 NORMALIZED VELnCITY 0DIST T. UR RIJL INCH NORM SPAN AX I AL INTENS 10.00 -0.0074 0.0153 1.0017 0.00505 20.00 -0.0117 0.0250 1.0072 0.00500 25.00 -0.0047 0.0176 1.0033 0.00504 30.00 -0.0031 0.0244 1.0061 0.00521 32.00 -0.0052 0.0258 1.0103 0.00508 34.00 -0.0058 0.0260 1.0066 0.00499 36.00 -0.0063 0.0284 1.0108 O.0o503 38.00 -0.0112 0.0294 1.0142 0.00645 39.00 -0.0166 0.0319 1.0115 0.00832 40.00 -0.0177 0.0313 1.0123 0.01171 41.00 -0.0252 0.0286 1.0112 0.02153 42.00 -0.0289 0.0320 1.0071 0.021_98 43.00 -0.0327 0.0316 1.0077 0.02539 44.00 -0.0332 0.0339 1.0079 0.03084 44.50 -0.0342 0.0371 1.0070 0.03431 45.0n -0.0341 0.0383 1.0052 0.03797 45.50 -0.0377 0.0444 1.0038 0.04377 ,,, 46.00 -0.0497 0.0481 0.9997 0.04844 46.50 -0.0513 0.0508 0.9888 0.05533 47.00 -0.0566 0.0391 0.9588 0.06256 47.50 -0.0592 0.0380 0.9494 0.06495 48.00 -0.0587 0.0294 0.9210 0.071].9 48.50 -0.0599 0.0046 0n.907-9 ... 0.07271 49.00 -0.0610 -0.0150 0.9057 0.07148 49.50 -0.0554 -0.0299 0.9080 0.06906 50.00 -0.0463 -0.0546 0.9204 0.06243 50.50 -0.0319 -0.0628 0.9296 0.05791 51.00 -0.0322 -0.0647 0.9441 0.04901 52.00 -0.0274 -0.0649 0.9745 -0-.-04-156 53.00 -0.0186 -0.0559 0.991A 0.02252 54.00 -0.0158 -0.0478 0.9939 0.01638 55.00 -0.0130 -0.0383 0.9972 0.00926 56.00 -0.0130 -0.0371 0.9980 0.00850 58.00 -0.0102 -0.0312 0.9980 0.00675 60.00 -0-0096 -0,0260 - 150010 000563'-' 62.00 -0.0085 -0.0241 1.0010 0.00568 64.00 -0.0074 -0.0216 1.0014 0.00563 66.00 -0.0068 -0.0207 1.0033 0.00559 70.00 -0.0035 -0.0163 1.0024 0.00534 ->- 0.00506 75.00 -0.0030 -0.0122 1.0019 80.00 -0.0024 -0.0112 1.0000 0.'00541 t,, LI~ P.

O ; · , .

?

': . .

TRAV22 FPS=100 X= 98.2 .. ALF =f, V. SPAN VORTEX CFNTER=49.20 NORMALIZED VELOCITY DIST TURBI!L INCH NORM SPAN AXIAL INTENS 11.00 0.0459 0.0070 0.8816 0.12612 20.00 0.0239 0.0237 0.931].9 0.05657 L. 25.00 0.0157 0.0112 0.9802 0.02937 30.00 0.0141 0.0058 0.9757 0.03640 35.00 0.0172 0.0052 0.9740 0.-04550 40.00 0.0229 -0.0082 0.9562 0.06501 42.00 0.0223 -0.0018 0.9575 0.06238 43.00 0.0193 -0.0005 0.9648 0.05943 44.00 0.0256 0.0069 0.9702 0.05525 45.00 0.0239 0.0146 0.9678 0.05193 46.00 0.0388 0.0138 0.9731 0.05037 46.50 0.0478 0.0152 0.9638 0.04862 47.00 0.0563 0.0182 0.9582 0.05291 47.50 0.0560 0.0163 0.9410 0.05934 .48.00 0.0465 0.0246 0.9293 0.06572 48.50 0.0269 0.0320 0.9181 0.06715 49.00 -0.0060 0.0319 0.9059 0.07291 49.50 -0.0234 0.0433 0.9160 0.07102 50.00 -0.0452 0.0367 0.9137 0.07277 50.50 -0.0608 0.0374 0.9291 0.06611 51.00 -0.0673 0.0445 0.9431 0.06225 51.50 -0.0854 0.0296 0.9536 0.05152 s2;.ff-n -- "-O.....6 0.03 2 .0 .9641 .. 0..0448'0 52.50 -0.0925 0.0335 0.9704 0.03880 53.00 -0.0823 0.0244 0.9814 0.03344 53.50 -0.0795 0.0227 0.9857 0.02978 54.00 -0.0765 0.0179 0.9769 0.02496 55.00 -0.0633 0.0128 0.9950 0.02093 56.00 -0.0508 0.0075 1.0011 0.01180 57.00 -0.0492 0.0053 -1.0015 0.00847 58.00 -0.0448 0.0074 1.0013 0.03419 60.00 -0.0393 0.0061 0.9955 0.00582 62.00 -0.0404 0.0062 0.9990 0.00527 64.00 -0.0371 0.0049 0.9953 0.00654 66.00 -0.0349 0.0062 0.9948 0.00618 70.00 -0.0311 0.0028 0.9916 0.00631 72.40 -0.0278 0.0053 0.9880 0.00614 _ ____ · · TRAV23 NORM ............................ ... FPS=1 00 .

12 3. 2 ALF _ VORTEX CENTER=49.50 NORMALIZED VELOCITY ,DIST. T'RR-iJL INCH NORM SPAN AXIAL INTENS 10.00 0.0053 0.0143 0.9967 0.00536 20.00 0.0058 0.0146 0.9963 0.00523 25.00 0.0042 0.0174 0.9966 0.004O0 30.00 0.0033 0.0201 1. 0033 0..00480 32.00 0.0012 0.0232 1.0037 0.00510 34.00 0.0017 0.0235 1.0033 0.00532 36.00 -0.0024 0.0244 _ 1.0095 0_.00__620 38.00 -0.0044 0.0250 1.0099 0.00933 39.00 -0.0111 0.0296 1.0070 0.01721 40.00 -0.0218 0.0316 1.0023 0.02525 41.00 -0.0265 0.0307 1.0060 0.02917 42.00 -0.0279 0.0275 0.9952 0.04118 43.00 -0.0300 0.0263 0.9975 0.03991 44.00 -0.0315 0.0228 0.997n 0.03726 44.50 -0.0284 0.0272 0.9962 0.03639 45.00 -0.0321 0.0251 0.9992 0.03859 45.50 -0.0294 0.0291 0.9970 0.04294 .6.00 -0.0267 0.0329 0.9911 0.04560 46.50 -0.0372 0.0340 0.9865 0.05227 47.00 -0.0376 0.0348 0.9835 0.04950 47.50 -0.0332 0.0291 0.9640 0.05971 48.00 -0.0372 0.0207 0.9422 0.06346 48.50 -0.0450 0.0115 0.9358 0.06368 49.00 -0.0463 -0.0037 0.9217 0.06856 49.50 -0.0363 -0.0065 0.9074 0.06895 50.00 -0.0403 -0.0331 0.9270 0.05774 50.50 -0.0317 -0.0505 0.9298 0.06134 51.00 -0.0325 -0.0593 0.9360 0.05289 52.00 -0.0243 -0.0687 0.9563 0.04192 53.00 -0.0150 -0.0544 0.9777 0.03018 54.00 -0.0098 -0.0531 0.9960 0.01981 55.00 -0.0034 -0.0453 0.9944 0.01332 56.00 -0.0029 -0.0397 0.9978 0.00858 58.00 0.0008 -0.0352 0.9983 0.00622 60.00 0.0008 -0.0298 0.9995 0.00609 62.00 0.0049 -0.0262 0.9946 0.00536 64.00 0.0024 -0.0247 0.9999 0.00593 66.00 0.0044 -0.0241 0.9973 0.00502 70.00 0.0064 -0.0192 0.9932 0.00506 i~ 75.00 0.0075 -0.0169 0.9991 0.00484....

o0.00 0.0075 -0.0156 1.0000 0.00631 I %.,t .ii 1- I ll' 1· I Iv

TRAV24 SPAN X=123.2 ALF= A. V0FPS=100. 8

VORTEX CENTER=48.70.

NORMALIZED VELOCITY TIRBI IL INCH NORM SPAN AXIAL I NIT E N S 11.00 0.0381 0.0006 0.8375 0.12299 20.00 0.0351 0.0170 0.9366 0.05074 25.00 0.0190 0.0083 0.9926 0.02106 _300 _ , Qo201__ 0.015 __0.99 09 0.0 268 35.00 0.0266 -0.0040 0.9799 0.03592 40.00 0.0302 -0.0096 0.9650 0.05032 42.00 0.0304 -Q06.09 0_.7_ ..... _ ... 4953 43.00 0.0295 -0.0029 0.9765 0.04744 44.00 0.0316 -0.0004 0.9813 0.04382 45.00 0.0468 0.0009 0.9P02 0,04569 46.00 0.0563 0.0039 0.9799 0.04649 46.50 0.0630 0.0001 0.9557 0.05028 47,00 0.0580 0.0033 0,9568 0.04911 47.50 0,0536 0.0057 .0.9318 0.06237 48.00 0.0281 0.0040 0.9225 0.06306 48.50 0.0202 0.0115 0.9181 0.06771 49.00 -0.0--080 0.0125 0.9147 0.06924 49.50 -0.0152 0.0215 0.9165 0.06666 50.00 -0.0418 0.0203 0.9327 0.06215 50.50 -0.0598 0.0190 0,.9455 0.05583 51.00 -0.0648 0.0141 0.9633 0.05043 51.50 -0.0686 0.0077 0.9745 0.04110 52.00 -0.0729 0.0039 0.9856 0.04106 52.50 -0.0725 0.0061 0.9898 0.03201 53.00 -0.0694 0.0125 0.9940 0.02988 53.50 -0.0629 0.0037 0.9998 0.02513 54.00 -0,0584 0.0017 1.0019 0.02090 55.00 -0.0528 0.00i0 1.0036 0.01756 56.00 -0.0485 0.0029 1.0009 0.01163 57.00 -0,0349 -0.0018 1.0116 0.00853 _ 5800 - 312 -0.021 _, 2 .00641 60.00 -0.0313 0.0005 1.0176 0.00563 62.00 -0,0276 0.0027 1.0140 0.00516 64.00 -0.0260 0.0024 1.0131 0.00658 66.00 -0.0203 -0,.0003 1.0169 0.00590 70.00 -0.0203 -0.0003 1.0188 0.00538 72.40 -0.0192 0.0022 1.0136 0.00529 TRP.A\25 X=147.() ALF= NIORM A \I RTEX CFNTER=49.70 NORMAL IZED \/ELnCTTY n I ST TI JR. I! L INCH NORM SPAN AXIAL I NTEF'S 1o.no0 0.0002 0.0152 1.no96h n.00506 20.00 0.0029 0.0168 I .0 112 0. 004e5 25.00 0.0018 0.0174 1.0n11 0.0046h ... 30. 00 0.0003 0.0190 1..nl 32.n00 -0.0007 0.021.5 0. 004520 34.00 -0.0028 0.0234 .01. 25 0.(0599 36.no -0.0034 0.0244 1..

1. 2F 0.00 889 38.00 -0.0116 0.0398 1.0152 0.02400 39.00 -0.0140 0.0364 1.0065 0.02506 40.00 -0.0197 0.0345 1.on22 0.03649 41.00 -0.0225 0.0354 0.9941 0.04152 42.00 -0.0213 0.0281 n.9857 0.05237 43.00 -0.0186 0.9791 0.0252 0.04808 44.00 -0.0240 0.0228 0.9870 0.04508 44.50 n.9915 -0.0263. 0.0229 0.04259 45.00 -0.0246 0.0257 0.9910 0.04205 .5.50 -0.0252 0.02h6 0. 994 0.04467 46.00 -0.0260 0.9890 0.0291 0.0451.6 46.50 -0.0277 0.0288 0.9927 0.04648 47.00 · -0.0344 0.0333 0.9836 0.04842 47.50 -0.0330 0.031.6 0.9644 0.05359 4R.00 -0.0431 0.0255 0.9620 0.05923 4R.5 . -0.0483 0.018h 0.952n 0.06277 49.00 -0.0342 0.0041 0.9296 0.06458 49.50 -0.0397 -0.0071 0.931 . 0.06.685 50.00 -0.0423 -0.0234 0.9315 0.06994 50.50 -0.0405 -0.0347 0.9276 0.05866 51.00 -0.0366 -0.0463 0.9322 0.05562 52 .n00 -0-.02-60 -- o0.059- 8 0.9564 0. 0448 5 53.00 -0.0259 -0.0631 0.9777 0.03346 54.00 -0.0210 -0.0559 0.983 ? 0.02651 s5.nn -0.0206 -0.0494 0.9917 0.02145 56.00 -0.0166 -0.0412 n.9927 n.n1275 58.00 -0.0144 -0.0334 0.9973- 0.00708 60.00 -. 0127 -0.0318 n.099s5 0.00605 62.00 -0.0100 -0.0273 1.n00? 0.00535.

64.00 -0.0061 -0.0232 0.9983 0.00562 66.00 -0.0028 -0.0214 n0.9975 o.'-0518 70.no00 -0.0040 -0.0190 1.0024 0.n0527 75,.00 rJ20! .O 01. 5 1.o0020 0. 00 523 ?0. 00 -. 0001 -- 0. 0130 .. 0000 0.0 50.5 X..'

L-~~~~~~~~~~~~~~~~~~~~~~~~~~~~........................

-----.--- o.o -o .oz- -. ,-.no n.oo-o L,...

_ TRAV26 SPAN X=147.0 _ ALF= 8. V, PS=100.

.. _ VORTEX CENTER=48.80 NORMALIZED VELOCITY -

- Y D IST

TURBUL INCH NORM SPAN AXIAL INTENS 11.00 0.0362 0.0075 0.8231 0.11630 'ij , 20.00 0.0.284 0.0181 0.9407 0.05216 4, ~ 25.00 0.0082 0.0095 0.9896 0.01930 30.00 o.0108 0.0011 0.9856 0.01860 32.00 0.0124 0.0027 0.9905 0.02107 34.00 0.0218 -0.0036 0.9745 0.03259 36.00 0.0238 -0.,0037 0.9688 0.03706 38.00 00.0233 -0.0058 0.9634 0.04734 ,. t./ 39.00 0.0243 -0.0064 0.9617 0.04546 j 40.00 0.0243 -0.0065 0.9622 0.04565 41.00 0.0238 -0.0049 -0.9639 0.04509 ;v k.J 42.00 0.0249 -0.0049 0.9647 0.04367 43.00 0.0265 -0.0004 0.9722 0.04398 44.00 0.0337 0.0038 0.9690 0.04284 44.50 0.0353 0.0053 0.9720 0.04267 45.00 0.0398 0.0079 0.9670 0.04268 45.50 0.0472 0.0122 0.9610 0.04978 46.00 0.0461 0.0049 0.9545 0.04888 46.50 0.0434 0.0130 0.9540 0.05325 47.00 0.0457 0.0047 0.9419 0.05873 47.50 0.0349 0.0169 0.9347 0.06397 48.00 0.0116 0.0187 0.9196 0.06581 48.50 -0.0065 0.0030 0.9164 0.06563 ql ij 49.00 -0.0201 0.0120 0.9186 0.06219 49.50 -0.0347 0.0133 0.9287 0.06114 50.00 -0.0482 0.0082 0.9365 0.06155

i : 50.50 -0.0657 0.0116 0.9525

0.05203 : 51.00 -0.0727 0.0065 0.9607 0.04650 51.50 -0.0746 0.0082 0.9611 0.04118 52.00 -0.0717 0.0031 0.9714 0.03550 52.50 -0.0708 0.0043 0.9796 0.03061 53.00 -0.0710 -0.0000 0.9799 0.02881 '".! iW" 53.50 -0.0700 0.0000 0.9798 0.02539 54.00 -0.0643 -0.0002 0.9872 0.01995 54.50 -0.0539 -0.0027 0.9863 0.01712 55.00 -0.0550 -0.0021 0.9881 0.01277 56.00 -0.0530 -0.0008 0.9894 0.00978 57.00 -0.0480 0.0015 0.9867 0.00832 :/i4 5l58.00 . -0.0469 0.0009 0.9862 0.00714 -- 4----~~~~ r~ i _ ~

:? i

59.00 0.0011 -0.0436 0.9841. o .0637 . . .......... .....

:,.

60.00 0.0011 0.9867 -0.0438 0. 00509 h !

, di .

62.00 0.002 1 -0.0410 0.9835 0.00545 0.0047 64.00 -0.0378 0.9851 0.00569 66. 00 0.0005 0.9895 -0.0360 '· -68.00 -0. 0035 -0.0269 0.9952 ., 0.00 553 I.

.:· 70.00 -0.0044 -0.0230 0.9898 0.00629 '1' 72.40 -0. 0050 -0. 02110 0.9938 0. 00571 ,;i .~ IHC900I EXECUTION TERMINATING DUE TO ERROR COUNT FOR ERROR NUMBER 217 - - . - _ _ . .- - - - . - -. - ---1------ - .-- - .! _ 7- IHC217I FIOCS - END OF DATA SET ON UNIT 5 S .i TRACEBAE8ACK FOLLOWS- ROUTINE ISN REG. 14 REG. 15 REG. 0 PR IBCOM 0007CB84 00070300 n0000nno0 ( i. L ^,, MAIN z 00002F98 5007AR20 ',( ' 0on0nn 7 l ,NTRY POINf T- 5007A820 I .n, t,t r -~~~~~~ ~ · _ .- .- _- _.-. _.. ..-- __. . _ _..._ I .. .

- - ----.---.... -_.....

I ·,; .!

., , r ' ', ,.

;.. . ..

I.

.'-.'" - -_%f ..

% '.' 1k.2 7 .... J _ -. - .. X=147.0 ALF= .. ?. . v, PS 0 . .. : .

:; _T,. IRAV2 VORTEX CENTER=47.50 .._.... ....L ...

LILE. JL....IY ........... ._.... .... _ ._._._

T TUR B IL ',- INC H NORM SPAN AXIAL . INTENS 0 ... 005.73 - .Q_. .. .. __.0..OQ.7_f_ _0...Q2:13_ . 1._087 · 1.0107 0.00554 32. 0 0 0.0058 0.0221 10 0.0046 0.0221 1.0122 0.00608 -i · 34.0 LO ...... ...... 1.3._1 _22 . . ._._ D 2SL2_. 7 . Q.... ... .0_03_ 1___.

38'.0, 0 -0.0008 0. 0274 1.0132 0.01471 0 -0.0083 0.9999 0.03387 40~ t4'0.0 0.0317 - 0 ..9832 0..0 5.42 .....

42.0h 43.0 0.9733 0.04977 0 -0.0.264 '.-' 44.0 0 -0.0138 0.0178 0.9708 0. 05026 0.... _Q.._..0_L74 .. .__0 ..93.2.7.

; __45._0. _QA._O.Q. .... Q .. 48_3_ 2..... .......

46.0' 0 -0.0193 0.0113 0. 9771 0.04590 47.0 0 -0.0221 0.0061 0.970R 0.04710 0-...... ..... 0..2 52.. _0o Q .. 0 0 9.7146 0...Q 0 _4628.

.-.4.8...0.( 49. 0O 0 -0.0267 -0.-0062 0.9603 0.04628 0 -0.0258 '-0.0201 0.9582 0.04724 :- ._ 50.0( 9._ _ ..... Q._2_:..- : -9O__32. O ... 952_ .... _......0.,_O_7_. _ .... .

52.0( 0) -0.0267 -0.0310 0.9599 0. 04375 , '. _ 53.01 0 -0.0254 -0.0421 0.03878 0.9679 -0 Q1... -oQ 0.Q.441 0 ..9 9839 _ . 0,Q2972 55.0( 0 -0.0157 -0.0422 0.9867 0.02770 i '?., 56.0( 0 -0.0108 -0.0362 0.9888 0.02167 58a0( 0 -0.0096 -0.0303 0.9944 0 .01502 2 0 -0.0090 -0.0240 1.0017 0.00861 60.0( 0 -0.0053 0.00564 62.0( -0.0225 1.0005

0 -0.QQ9 02Q1 _. .0 1.0000 0. 00626

r ._..-_,40(

TRA VZ._ ......SPAf',! X=147,0 ALF= F. VFPS=(O. -- I -I VORTEX CENTER=47.70

Li

0N._LED LT.... J ... r Y ._....................

0 DIST TUIRBUL SPAN AXIAL INiT ENS -. INCH. NORM ___ o 60 -0.... .. 005....7..,.oo'_o_ 57_.__ ., 0973 . 0.03562_ 0.0337 -0.0071 0.9743 0.04108 38.00 40.00 0.0325 -0.0071 0.9771 0.04236 ._4_2..o0 .__ 0.0360 -0._.0030 _ 0. 9772 0.04069 44.00 0.0580 0.0012 0.9703 0.04780 0..0422 0. 0055 0.9499 0.05335 46.00 47.00 0.0101 -0.0041 0.9307 0.05477 48.00 -0.0093 -0.0043 0.9403 0.05290 0.05198 49.00 -0.0212 -0.0051 0.9522 _-.O0_ 00.... -. 0.- _..0___- _ _.0065 0 .. 9635 0.04446 -0.0433 -0.0065 - 0.9789 0.03519 51.00 52.00 -0.0459 -0.0052 0.9846 0.02971 -0.0071 .... 0.9945 0.02003 Q.._5... _.- -0.0392 54.00 -0.0351 -0.0080 0 .9952 0.05565 ,,,_ 56.00 -0.0304 -0.0079 0.9986 0.00718 1.0085 0.00574 58..0 .- 0.0168 -0.0129 -0.0098 1.0099 0.00613 60.00 -0.0150 62.00 -0.0126 -0.0090 1.0119 0.00569 6;4. 00 -0.0132. -0.0087 1.0108 0.00688 ?/ k I--- - - - - -- -f --:- -r-?r~~~~r-P lr· r r -~mmcl--·---r·-- ~ r - -,--^ TRAV29 NORM X=147.0 ALF= P. V FPS=100.

VORTEX CENITER=49.50 NORMALIZED VELOCITY DIST TURBUL INCH NORM SPAN AXIAL INTENS 10.o00 0.0053 0.0129 1.0750 0.00524 20.00 0.0047 0.0174 1.0775 0.00556 25.00 0.0040 0.0187 1.0799 0.00801 30.00 -0.0022 0.0223 1.0749 0._02236 32.00 -0.0088 0.0362 1.0544 - 0.03025 34.00 -0.0096 0.0407 1.0474 0.03863 36.00 -0.0137 0.0362 ]..0352 0.04950 38.00 -0.0145 0.0331 1.0166 0.05680 39.00 -0.0135 0.0307 1.0039 0.05998 40.00 -0,0154 0.0311 1.0057 0.06037 41.00 -0.0158 0.0321 1.0031 0.06195 42.00 -0.0183 0.0279 1.0016 0.06298 43.00 -0.0156 0.0279 0.9982 0.06372 44.00 -0.0191 0.0260 0.9958 0.06324 0.0240 1.0009 0.06367 44.50 -0.0240 45.00 -0.0234 0.0253 1.0025 0.06503 45.50 -0.02 66 0.0215 1.0010 0.06268 46.00 -0.0294 0.0199 1.0038 0.06290 46.50 -0.0114 0.0317 0.9883 0.06354 47.00 -0.0307 0.0119 0.9983 0.06730 , 47.50 -0.0341 0.0085 0.9R76 0.06589 48.00 -0.0355 0.0015 0.9844 0.06973 4..50 9-0.0377 -0.0028 0.9s50 0.06825 - _,, 49.00 -0.0391 -0.0085 0.9707 0.07076 49.50 -0.0421 -0.0158 0.9647 0,.07275 50.00 -0.0447 -0.0240 0.9443 0.07055 50.50 -0.0496 -0.0321 0.9498 0.06665 51.00 -0.0408 -0.0386 0.9434 0.06585 52.00 -0.0478 -0.0466 0.9522 0.06023 53.00 -0..0394 -0.0577 0.9630 0.05317 54.00 -0.0359 -0.0586 0.9702 0.04258 55.00 -0.0246 -0.0575 0.9883 0.02918 56.00 -0.0230 -0.0542 0.9932 0.02196 58.00 -0.0206 -0.0408 1.0038 0.01312 60.00 -0.0168 -0.0343 1..o1q 0.00759 62.00 -0.0132 -0.0299 1.0006 0.00697 64.00 -0.0125 -0.0258 1.0027 0.00621 66.00 -0.0259 -0.0340 1.0165 0.00627 70.00 -0.0068 -0.0202 0.9991 0.00595 kI - i::. ., r .

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-.-. 1.- --...-...-..----- -- .-..-- ..- --- _ TPRAV3 () SPAN VX..=147T ALE_ ... ... C N..TE q4. .

Y,E... -.. .5 VORTEX CENTER:44.50 NORMALIZED VELOCITY . IST TURBUL ',,,.,.

INCH NORM SPAN AXIAL INTENS 11.00 0.0426 0.0045 0.8531 0.11306 20.00 0.0339 0.0303 0.9390 0.05083 x;' 25.00 0.01,88 0.0205 0.9916 0.01743 30.00 0.0261 0.0217 0.9922 0.01672 32.00 0.0298 0.0218 0.9904 0.02055 34.00 0.0353 0.0230 0.9886 0.02701 36.00 0.0466 0.0155 0.9930 0.03115 38.00 0.0514 0.0157 0.9927 0.03070 39.00 0.0513 0.0151 0.9943 0.03588 40.00 0.0620 0.0212 0.9855 0.04266 41.00 0.0622 0.0098 0.9702 0.05623 42.00 0.0594 0.0076 0.9652 0.05528 43.00 0.0470 0.0207 0.9532 0.06155 44.00 0.0281 0.0146 0.9413 0.06827 ~.,,' 44.50 0.0200 0.0237 0.9348 0.07192 45.00 0.0073 0.0179 0.9387 0.07221 45.50 -0.0091 0.0155 0.9352 0.06886 ~,__t 46.00 -0.0186 0.0105 0.9323 0.07031 46.50 -0.0266 0.0089 0.9414 0.06465 47.00 -0.0282 0.0113 0.9406 0.06733 47.50 -0.033t1 0.0110 0.9486 0.06470 48.00 -0,03195 0.0032 0.9479 0.06246 48.50 -0.0397 0.0040 0.9499 0.06264 k,., 49.00 -0.0417 0.0043 0.9527 0.05901 49.50 -0.0462 0.0044 0.9552 0.05742 50.00 -0.0487 0.0003 0.9583 0.05575 50.50 -0.0469 0.0025 0.9547 0.05424 51.00 -0.0492 0.0006 0.9574 0.05344 52.00 -0.0566 -0.0027 0.9672 0.04562 53.00 -0.0559 0.0015 0.9693 0.04302 54.00 -0,0545 0.0022 0.9733 0.03428 56.00 -0.0574 0.0042 0.9846 0.02166 58.00 -0.0548 0.0044 0.9832 0.01039 60.00 -0.0481 0.0044 0.9903 0.00821 65.00 -0.0392 0.0018 0.9917 0.00654 k.7 72.40 -0.0313 0.0014 0.9930 0.00622 0/ 1!

i%,., TRAVIl NIRM Xl147.0 ALf-V 4. VCFPR= SlU.

..y1

VORTEX CENTFR=50.HO NORMALIZFD VELOCITY :"',[ · ) OlIST TIURBIJL t'+ I INCH NORM SPAN AX I AL INTEN!S 10.00 -0.0016 0. 0276 1. 0193 0.00525 20.00 -0.0016 0.0277 1.0216 0.00521 :' .. 25.00 0.,0005 0. 0283 1.0256 0.00564 30'.00 0.0034 0.0317 1..0227 0.00827 32;'00 0.0034 0.0351 1.0234 0.01589 0.03217 . .v 34.00 0.0000 0.0389 1.0223 1 . 003R 0. 03607 36,00 -0.0161 0.0454 -0.0310 0.0489 0.9896 0.04050 38.00 40.00 0.0359 0.9741. 0.04475 -0.0395 -0.0404 0.0190 0.9664 0.04534 41,00 42.00 -0.0381 0.0113 0.04797 0.9567 -0.0356 0.0012 0.9525 43.00 0.04655 0.04487 44,00 -0,0342 -0.0035 0.9496 0.9497 45.00 -0.0335 -0.0015 0.04338 46.00 0. 9640 0.03948 -0.0318 0. 0101 46.50 -0.02 81 0.0095 0.9722 0.03655.

47.00 0.0070 0. 9775 0.03417 -0,0339 vj~ 47.50 -0.,0354 0.0061 0.9787 0.03078 48.00 -0.0333 0.9792 0.03078 0.0058 48.50 -0.0369 0.0094 0.9833 0.03024 0. 9840 '! v 49,00 -0.040'7' 0.0077 0.03254 49.50 -0,0541 0.0041 0.9792 0.03833 50.00 -0,0473 - ._04- 0- 0.9647 0.04449 -0.0472 -0,0165 0.9546 50.50 0.04511 51.00 -0,0442 -0, 0409 0.9434 0.04850 -0.0438 0.9460 0.03458 51.50 -0.0479 ;i,~, 52.00 -0.0323 -0.0558 0.9567 0.03418 -002 -0.0630 0.9669 52.50 88 0.02939 53.00 -0.0220 -0.0700 0.9721 0.02387 -0 0275 -0.0659 0.9839 0.02016 53.50 54.00 -0.0136 -0.0637 0.9855 0.01658 55.00 -0.0136 -0.0599 0.9859 0.01321 56,00 -0.0100 -0.0537 0.9957 0. 00765 -0.0077 -0.0461 57.00 0.9959 0.00615 58.00 -0.0092 -0.0423 0.9987 0.00570 ~i., -0.0077 -0.0392 1. 0013 0.00560 59.00 60.00 -0.0055 -0.0355 1 .0012 0.00543 62.00 -0 .0040 -0.0339 1.0005 0.00544 -0.0032 -0.0327 1. 0004 0.00558 64.00 :!?F: I';% 66.00 -0.0025 -0.0307 1.0032 . 005P5 68.00 -0.0025 -0.0291 1.0021 0.00599 70 0', 0 -0.0010 -0.0283 1.0031 0.00566 i- A5.00 000208 -0.0213 1..OOOn 0.00768 ii i, . · · ··· L.../-.~_:_._. _~. _~_....._. .... .

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.'; ; .I -1 - :-A 12 X=147.0 ALF= 4. V,FPS=100. ,, II ,,,TRAV32 SPAN ±11 ..

VORTEX CENTER=46.20 . , . x NORMALIZED VELOCITY TUR BIIL DIST ,,.a..

. . ,- . I TNCH

NORM SPAN AXIAL INTENS 11.00 -0.0073 0.0080 0.8620 0.09118 ,. ., 20.00 0..0193 0.0215 0.9163 0.05802 ': ' , 25.00 0.0038 0.0086 0.9661 0.03014 30.00 0.0098 0.0044 0.9765 0.00750 32.00 *0.0188 -0.0016 0.9833 0.00658 '. ~634.00 0.0209 -0.0028 0.9833 0.00629 0,.0266 -0.0061 0.9867 0.00604 38.00 0.0300 -0.0105 0.9839 0.00616 1' -/ 39.00 0.032 8 -0.0121 0.9828 0.00639 40.00 0,0329 -0.0122 0.9850 0.00674 41.00 0.0377 -0.0118 0.9794 0.00825 .PV 42.00 0.0425 -0.0098 0.9750 0.01232 43.00 0.0472 -0.0158 0.9667 0.02721 ,' ,, ':43.50 0,0480 -0.0123 n.9705 0.O2152 44 00 0.0572 -0.0061 0.9619 0.03132 44.50 0.0636 -0.0247 0.9391 0.0 3234 45.00 0.0580 -0.0267 0.9313 0.04572 v , L 45.50 0.0261 -0.0135 0.9158 0.05368 46.00 0.0070 -0.0184 0.9173 0.05701 46.50 -0.0218 -0.0208 0.9214 0.04943 -0 0436 -0.0232 0.9289 ~: ~ 47,00 0.04113 47.50 -0.0561 -0.0176 0.9470 0. 03971 48,00 -0.0613 -0.0175 0. 9535 - 44. 4.50 -0.0695 -0.0200 0.9586 0. 02 814 49.00 -0,0695 -0.0185 0.9602 0.02564 49.50 -0.0737 -0.0177 0.9690 0.0 2112 *: 50.00 -0.0725 -0.0192 0.9700 0.01909 50.50 -0.0720 -0.0204 0.9716 0.01458 51.00 -0.0707 -0.0211 0.9727 0. 0147 7 51. 50 -0.0682 -0.0218 0.9758 0.01125 52.00 -0 .0617 -0.0247 0.9799 0.00972 * 53.00 -0.0535 -0.0259 0.9838 0. 00647 ,j -0.0513 54.00 -0.0262 0.9825 0.005R5 55.00 -0.0473 -0.0223 0.9787 0.00544 56.00 -0.0458 -0.0199 0.9786 0.00 5 42 57.00 -0.0446 -0.0215 0.9814 0.00586 58,)00 -0.0438 -0.0202 0.9813 0.00568 60.00 -0.0424 -0.0210 0.9806 0.00562 62.00 -0.0425 -0.0202 0.9R34 0.00567 i: , -0. 0198 0. 9P45 0.00667~ 64. 00 -0.0419 0.9R62 0.00o713 -0.0206. 66,00 -0.0420 -0.0190 0.9851 0.00611 68.00 -0,0419 0.00697 -0.0206 0.9840 70.00 -0.0419 -0.0214 0.9857 0.00728 72.00 -0.0420' ...... ~- ~ ~ d........... ·..........

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II X=147.0 ALF= 4. _V I FI)S= 1 ( 10. TRAV33 NnRM VORTEX .CFNTER=50¢.40 i I NORMALIZED VELnCTTY DIST TUJR IJL NORM· INCH SPA N AXIAL INTENS _ 20.00 -0.0000 0.0000 1.0308 0.0 30.00 -0.0000 0.0038 1.0335 , .J 335.00 0.0009 0.0081 1.0288 _40,00 -0.0083 0,0095 1.0309 0.0 44.00 0.0001 -0.0007 1.0194 0.0 0.0 v <> 45.00 0.0009 -0.0013 1,0233 46.00 -0.0007 -0.0022 1._ 0186 0.0 47.00 0.0 -0.0022 -0.0009 0.9973 0.0 ~,..~ 48.00 -0.0030 -0.0086 0.9929 49.00 -0.0046 -0.0173 0.9828 0.0 50.00 -0.0013 -0.0171 0.9769 0.0 51.00 0.0 -0.0046 -0.0269 0.9780 52.00 -0.0079 -0.0296 n.9796 54.00 -0.0190 -0.0326 0.9929 -0.0224 -0.0285 1.0000 0.0 56.00 %_ TRAV34 SPAN X=147.0 ALF= 4. V. FPS=100 VORTEX CENTFR=47.00 NORMAL .IZED V\/ELOCITY DIST TOJRBIJL L: INCH NORM SPAN AX I AL INTENS 11.00 0.0047 -0.0026 0.9478 0.08550 20.00 0.0151 0.0191 0.9915 0.071R3 25.00 0.0071 0.0161 ].0677 0.03944 30.00 0.0036 0.0079 1.0821 0.00825 32.00 - 0.0090 0.0038 1.0836 0.00718 .34.00 0.0090 0.0 03 8 1.0808 0.00691 36.00 0.0090 0.0018 1.0794 0.01067 37.00 0.0090 -0.0031 1.0759 0.01221 38.00 0.0098 -0. 0016 1.0752 0.016R1 39.00 0.0125 -0.0059 1.0689 0.01820 40.00 0.0108 -0.0051 ].0745 0.11182 41.00 0.0161 -0.0039 1.0666 0.03449 42.00 0.0196 -0.0019 1.0638 0.02671 42.50 0.0204 -0.0013 1.0603 0.02797 43.00 0.0196 0.0010 1.0658 0.03027 43.50 0.0221 0.0016 1.0609 0.02969 44.00 0.0211 0.0022 1.053 0.03219 k..,' 44.50 0.0140 0.0093 1.0453 0.032.14 45.00 0.0236 0.0009 1.0470 0.03417 45.50 0.0237 0.0018 1.0503 0.03289 46.00 0.0194 -0.0007 1.053S 0.03364 46.50 0.0133 0.0018 1.0544 0.03114 47.00

-0.0025 -0.0012 .-056- 0.02876

47.50 -0.0052 -0.0017 1.0568 0.02879 48,00 -'0.0123 -0.0019 1.0617 0.02675 4. 50 -0.0169 -0.0045 1.0654 0.02378 49.00 -0.0205 -0.0037 1.0683 0.02100 49.50 -0.0223 -0.0057 1.0692 0.01370 50.00 -0.0159 -0.0030 1.0660 0.01225 51.00 -0.0233 -0.0073 1.0714 0.00993 52.00 -0.0233 -0.0092 1.0700 0.00801 53.00 -0.0242 -0.0106 1.0673 0.00746 54.00 -0.0224 -0.0117 1.0693 0.00661 55.00 -0.0216 -0.0112 1.0713 0.00679 56.00 -0.0179 -0.0121 1.0684 0.00619 58.00 -0.0161 -0.0110 1.0669 0.00691 62.00 -0.0134 -0.0007 1.0758 0.00754 68.00 -0.0097 -0.0112 1.06ll 0.00717

Ii I TRAV35

X=162.0 ALF=12. V, FPS=100. NORM I .

VORTEX CENTER=44.70 1; NORMALIZED VELOCITY -' --- - - _ __ .. ... . . _. .. .. _. ..-..- D IST T URB UL INCH NORM SPAN AXIAL INTENS 10.00 -0.0077 0,0260 0.9806 0.00718 15.00 -0.0047 0.0279 0.9805 0.00677 ,~ , 20.00 -0.0093 0.0292 0.9870 0.00692 25.00 -0.0123 0.0363 0.9940 . 0.00685 30.00 -0.0101 0.0418 0.9973 0.00677 32.00 -0.0101 0.0501 1.0036 0.01406 34,00 -0.0070 0.0434 0.9929 0.02538 36.00 -0.0046 0.0567 0.9964 0.01235 37.00 -0.0017 0.0665 1.0054 0.00979 38.00 -0.0055 0.0716 1.0114 0.00898 39.00 -0.0033 0.0743 1.0127 0.00898 ~v. 40.00 -0.0009 0.0908 1.019R 0.01311 41.00 0.0035 0.1163 1.0324 0.02168 41.50 0.0180 0.1314 1.0292 0.02656 42.00 0.0363 0.1430 1.0254 0.04654 42.50 0.0455 0.1539 1.0360 0.04276 43.00 0.0160 0.1710 1.0450 0.06187 43.50 0.1186 0.1667 1.0510 0.09466 44.00 0.1205 0.0599 1.0718 0.11790 - . . .- I. . ... . ...

44.50 0.1521 0.1362 1.0741 0.11229 45.00 0.1490 -0.0292 1.0499 0.13627 45.50 0.1480 -0.0749 1.0165 0.10579 46.00 0.1239 -0.1117 1.0342 0.09185 ;R. 46.50 0.0932 -0.1833 1..0031 0.05562 47.00 0.0489 -0.1707 1.0425 0.04108 47.50 0.0383 -0.1714 1.0354 0.04655 48.00 0.0356 -0.1754 1.0122 0.02740 48.50 0.0313 -0.1637 1.0264 0.02636 49.00 0.0507 -0.1385 1.0051 0.02202 50.00 0.0271 -0.1326 1.0241 0.01579 51.00 0.0231 -0.1203 1.0051 0.01309 52.00 0.0193 -0.1021 0.9948 0.00974 53.00 0.0143 -0.0966 1.0028 0.00777 54.00 0.0098 -0.0874 0.9912 0.00759 55.00 0.0097 -0.0756 1.0020 0.00717 56.00 0.0097 -0.0724 1.0073 0.00717 58.00 0.0155 -0.0636 1.000o 0.00755 60.00 0.0124 -0.0583 1.0024 0.00700 65.00 0.0093 -0.0502 1.0000 0.00853 v 70,00 0.0085 -0.0361 1,01.14 0.00802 '~ . 75.00 0,0081 -0.0257 1.0006 0.00753 80. .00 0.0074 -0.0225 1.0000 0.00732 \.

i.

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_ ~~~~~~ " ' -- x------·-----u ------- ---- ·-·a -7c·-- rr -- -- --- ·-- --- -- ·-·I TRAV36 SPAN X=162.0 ALF=12. V. FPS=l()o.

VORTEX CFNTER=60.20

NORMAL IZED VELnCITY

I.ST .... TU RB .. L INCH NORM SPAN AXIAL TINTENS 11.00 -0.0234 -0.0373 0.9562 0.()602 15000 -0.0100 -0.0357 n.937R 0.'06439 20.00 0.0004 -0.0260 n.9402 0.05616 25.00 0.0082 -0.0181 0.9576 0.03753 30.00 0.0149 -0.0157 0.9~66.19 . 0.02093 35.00 0.0193 -0.0021 0.9683 0.01235 40.00 0.0208 0.0008 0.9699 0.00919 42.00 0.0267 -0.0001 0.9715 0.00807 44.00 0.0401 -0.0047 0.9721 0.00852 46,00 0.0499 -0.0031 0.9794 0.00824 48.00 0.0510 -0.0078 n.99-o 0.00775 49.00 0.0589 -0.0089 0.9780 0.00817 50.00 0.0605 -0.0050 .0.9845 0.00831 51.00 0.0669 -0.0060 0.9759 0.00752 52.00 0.0677 -0.0046 0.9779 0.00879 53.00 0.0739 -0.0028 0.9837 0.00904 54.00 0.0924 -0.0144 0.9862 0.01112 55.00 0.1092 -0.0086 0.9844 0.01447 55.50 0.1028 -0.0161 0.9930 0.01899 56.00 0.1082 -0.0344 0.9817 0.01955 56.50 0.1117 -0.0533 1.0107 0.02145 57.00 0.1283 -0.0556 0.9951. 0.01950 57.50 0.0908 -0.1021 1.0261 0.03956 58.00 0.1141 -0.1060 0.9942 0.04055 58.50 0.1137 -0.1146 1.0125 0.05892 59.00 0.0507 -0.1823 1.0235 0.08658 59.50 0.0621 -0.1999 1.0520 0.10687 60.00 -0.0060 -0.2036 1.0573 0.06269 60.50 -0.0723 -0.1738 1.0493 0.06041.

61.00 -0.1085 -0.1605 1.0622 0.07922 61.50 -0.1327 -0.1597 1.0631 0.05610 62.00 -0.1506 -0.1081 .. 0251. 0.03826 62.50 -0.1219 -0.0838 1.0274 0.02951 63.00 -0.1179 -0.0706 1.0204 0.02521 64,00 -0.1224 -0.0609 1.0139 0.01708 65,00 -0.1030 -0.0519 1.0057 0.01512 66.n00 -0.0998 -0.0470 n.9965 0.01393 67.00 -0.0938 -0.0374 0.9926 0.01306 68.00 -0.0875 -0.0338 0,98.75 0.01083 ,j 69.00 -0.0871 -0.0315 0.9923 0.0089_ 70.00 -0.0847 -0.0286 0.9874 0.00744 72.00 -0.0713 -0.0205 0.9807 0.00726 k..'I I w. I t k.J I ,,..'

',,_.

k.,, I I- -----c- --- I- ' - I - ---------- --------- --- --------- -- ---- -··----- ----- · ::~~~~~~~~~~~~------ -- -- . ...... , -- . .--- TRAV37 NORM X=162.0 V.

TRAV37·~ ~·~u·~· I-1L L-. MOR _ _.0 .L ALF= FPS=00=44.70 -_... .. __.......................................

VORTEX CENTER=44.70 NORMALIZED VELOCITY n IST TURB IIL ',*,~ IINCH NORM SPAN AXIAL INTEN S 10.00 -0.0024 0.0134 0.9944 0.00728 -, ~15.00 -0,0076 0.0389 1. 0124 0.0075 4 20.00 -0.0085 0.9947 0.0094 0.00713 25.00 -0.0023 0.0151 0.9933 0.00696 30.00 0,0017 0.0153 0.9864 0.00722 *.j 32.00 0,0017 0.9927 0.0242 0.00713 34.00 0.0043 0.0289 0.9865 0.00716 ____ 36.00 0.0039 0.9781 0.0277 0.01627 37.00 0.0054 0.0277 0.9781 0.01942 38.00 0.0031 0.0304 0.9832 0.01288 39.00 0.0076 0.0350 0.9809 0.00985 40.00 0.0069 0.0457 0.9894 0.01072 40.50 0,0030 0.0489 0.9985 0.01274 41.00 0.0105 0.0554 0.993R 0.01385 0.0127 41.50 0.0611 0.9969 0.01673 42.00 0.0187 0.0664 0.9921 0.01596 42.50 0.0166 0.0676 0.9904 0.022 66hh 43.00 -0.0039 0.0928 0.9943 0.04812 43.50 0.0061 0.0826 0.9994 0.05008 44.00 0,0470 0.0345 0.9560 0.08974 44.50 0.0154 -0.0176 0.99 15 0.07785 45.00 0,0636 -0.0 189 0.9934 0.09860 45.50 0.0636 0.08583 46,00 0.0697 -0.0 130 1.0052 0. 08566 46.50 0.0531 -0.0964 0.9818 0.04892 47.00 0.0451 -0.0912 0.9977 0.02944 47.50 0.0255 -0. 1006 1.0074 0.02444 48.00 0.0247 -0.1037 1. 0068 0.02325 48.50 0.0315 -0.0919 1.0005 0.02056 49.n0 0.0299 -0.0886 1.0034 0.02025 50.00 0.0203 -0.0930 0.9988 001244 51.00 0.0206 -0.0740 1,0054 0.01057 0.0130 52.00 -0. 0669 1. 0007 0.00805 53.00 0,0044 -0.0605 1. 0048 0.00813 54.00 0.0079 -0.0559 1. 0001 0.00780 55.00 0.0029 -0.0524 1.0087 0.00814 56.00 0.0069 -0.0473 1.0096 0.00844 I 58.00 0.0046 -0.0414 1.0130 0.00791 ~. ~ .. 60.00 0.0046 -0.0339 1.0183 0.00911

!ii ; i

65..O0 0.0091 -0.0261 ] .0112 .())H - 51 70.00 0.0060 -0.0252 1.0120 0.o0053 75.00 0.0057 -0.0195 1.0043 0.00722 80.00 0.0075 -0.0168 1.0000 0.00694 ii ,:I ; ,: - _ 7 ~ ~ ~ ~ -. _ _ _ _ _ _ . ___ , .

'1: ..

X=162.0 ALF= A. V FPS=1_00. _ TRAV38 SPAN VORTEX CENTER=59.70 :.

NORMAl LIZED VELOCITY

nTST TURBOL

.:.

.: INCH NORM SPAN AXIAL INTENS %.-, ..

1.1.00 -0.0291 -0.0252 0.9575 0.05460 I 15.00 -0.0233 -0.0241 0.9694 0.04741.

,.I 20.00 -0.0036 -0.0235 0.9762 0.03744 ·i 4L 25.00 -0.0110 .0.9883 0.02756 0.0007 30.00 0.0097 -0.018 0.9879 0.01616 35.00 0.0167 -0.0133 0.9780 0.01066 40,00 -O007 4 0.9761 0.00777 ___0,0221 42.00 0.0252 -0.0067 0.9706 . 00759 44.00 -0.0076 0.9722 0.00825 0.0251 46.00 0.0267 -0.0067 n.9706 0.00858 -0.0027 0.9774 0.00847 48.00 0.0266 49.00 0. 0266 0.0020 0.9812 0.00856 50.00 0.980O 0.00924 0.0280 0.0021 51.00 0.0382 -0.0030 0.9878 0.00948 0.0375 -0.0025 0.9868 0.00808 52.00 53.00 0.0434 -0.0025 0.9872 0.00981 54.00 0.0486 -0.0014 0.9811 0.01211 55.00 0.0604 0.0078 0.9833 0.01213 55.50 0.0721 0.0064 0.9795 0.01445 56.00 0.0755 0.0132 0.9777 0.01697 56.50 0.0807 -0.0043 0.9696 0.03037 57.00 0.0951 -0.0007 0.9851 0.03028 57.50 0.1005 -0.0254--- 2 0 5 0 .0563 58.00 0.0962 -0.0224 0.9779 0.06658 58.50 0.0821 -0.0036 0.9913 0.08227 59.00 0.0205 -0.0302 0.9889 0.08764 59,50 0.0027 -0.0011 0.9852 0.08188 60.00 -0.0166 0.0005 0.9628 0.08971 60.50 -0 .0991 0.0093 0.9910 0.07152 61.00 -0.0865 -0.0124 0.9911 0.05941 61.50 -0.1067 -0.0018 1.0043 0.04788 62.00 -0. 1043 0.0059 1.0038 0.04554 62.50 -0.0967 -0.0076 0.9880 0.03433 63.00 -0.0953 -0.0070 0.9786 0.01915 64.00 -0.0860 -0.0075 0 9853 0.0151.?

65.00 -0.0833 -0.0135 0.9779 0.01396 66.00 -0.0749 -0.0147 0.9931 0.01150 67.00 -0.0714 -0.0113 1.0033 0.01095 -0.0676 68.00 -0.0193 1.0044 0.00667 69.00 -0,0607 -0.0151 1.0001 0.00810 to_ .

',,..

70.00 -0.0553 -0.0131 0.992P 0.007R2 72.00 -0.0533 -0.0140 0.9877 0.00728 k..

L',.

v N..

4., \/I)RTFPX CFNI fi:l4/t..f l.

I ,.II . I NORMALIZED VFLOCITY I IlST T R B IL INCH NORM INT EN S SPAN AXIAL 10.00 -0.0024 0.0080 1.026.3 0.008 26 15.00 -0.0041 0.0124 1.0 290 0.00782 1.0354 0.00787 ' v 20.00 -0.0044 0.0106 -0.0060 1.0342 0.00785 25.00 .0.0094 I '30. 00 -0.0015 0.0105 1. 0260 0.007 56 -0.0033 0.0084 1.0267 0.00749 32.00 _ 34.o00 -0.0040 0,0122 1.. 0273 0.01158 36.00 -0.0112 0.0139 1.0397 0. o009n5 0.008P4 ._- 37.00 -0.0058 0.0191 1.O343 0. 00905.

3 .00 -0.0047 0.0202 1.0274 o. oosa4 0.01167 39.00 -0.0094 0.0161 1.0391 .j 1. 0301 0.01567 ; 40.00 -0.0090 0.0187 40.50 -0.0019 0.0179 1.0170 0.01564 41.00 -0.0134 0.0150 1.()334 0.01644 1.0310 0.01604 41.50 -0.0108 0.0154 1.035n0 0.01706 42.00 -0.0134 0.0172 -0.0135 0.0231 1.0417 0.01563 42.50 -0.0122 0.0206 1.0302 0.01633 43.00 1.0391 0 .02212 43.50 -0.0151 0.0228 44.00 -0.0203 0.0151 1.0381 0.03069 44.50 -0.0279 0.0186 1.0123 0.03566 0.04010 45.00 -0.0300 0.0136 1. 0170 45.50 -0.0042 0.0092 0.9827 0.05276 0.9916 0.04956 · _., 46,00 -0.0300 -0.0222 46.50 -0.0233 -0,0210 0.9899 0.0 05589 '"5 47.00 -0.0148 -0.0512 0.9980 0.05124 -0.0111 -0.0471 0.9955 0.023 50 47.50 48.00 -0.0063 -0.0471 1.0004 0;02311 0.9942 0.01652 48.50 -0.0052 -0.0485 49.00 -0.0149 -0.0462 1. 0042 0. 04059 -0.0141 -0.0457 1. 0060 0.01260 50.00 51.00 -0.0050 -0.0315 1. 0000 0,00747 52.00 -0,0036 -0.0295 1. 0096 0.00823 53.00 -0.0037 -0.0285 1.0130 0.00774 .00. .. 83 ..

54.00 -0.0036 -0.0274 1.0111 1. 0118 -0.0019 -0.0233 0.00837 55.00'

56.. 00 0.0016 -0.0234 1.0075 0.00763

58.00 -0.0018 -0.0213 1.0112 0.00783 -0.0008 -0.0158 1. 0099 60.00 0.00798 , i , - ~. ~--- _......

65.00 -0.0016 -0.0143 1.0105 0.00795 70.00 -0.0014 -0.0133 1.0061 0.00734 1..0045 0.00722 75.00 0.0028 -0.0088 1,000 1 00.00799.

80o.00 0.0088 -0,.0084 -------------- ·-- ------------- ------------- ·- --- · ·------ ---- -- -.... _.. ._._..____ __.._: . -- --------.

'v- i- --- --·-·------ ---~ - ~ -~ ~ -~ -- ------- ~ ^~~--~~~ .`-' ~`~ - ~ , .

=

(6

TR. A\/1(40) SPANt X 162.Q_ AL -I 4, V., FP'. =1(0.

VORTEX CFNl'F!R=60. 50 NORMALIZED VELOCITY TUiRBL D IST NORM SPA N AXI AL INTENS .. ,...,~ INCH ?1:?';. ' 1 1.00 -0.0331 -0.0174 0.9 285 0.00741 ]i 5.00 -0.0336 -0.0 142 0.9379 0.00 652 20.00) -0.0121 -0.0078 0.9682 0.00475 25.00 0.9784 .0.024 5 9 0.0012 -0.0056 n.9844 30.00 -0.0006 -0.0083 0.01258 35.00 0.0009 -0.0072 0.9R76 0.00846 40.00 0.0027 -0.0032 n.9859 0.07605 0.9803 42.00 0.0109 -0.0023 0.07854 · ... 44.00 0.0075 -0.0009 0. 9R93 0.08077 46,00 0.0083 0.0017 0.9901 0.08202 0.9863 48.00 0.0100 -0.0016 0.06595 k..' 49.00 0.9845 0.011'6 -0.0006 0.08243 0. 9868 0.07222 50.00 0.0091 -0.0050 51.00 0,0116 -0.0036 0.9848 0.07938 0.9919 ,,~' 52.00 0.0099 0.0008 0.07793 0.0132 0.0015 0. 9859 0.079?22 __ 5__3._00 0.9884 54.00 0.0140 0.0001 0.11066 0.9862 ,4_, 55.00 0.0140 -0.0030 0.01138 56.00 0.0318 0 0024 0.9918 0.0 1102 0.9858 56.50 0.0351 -0.0089 0.01393 0.0399 0.0043 0.9892 0.011].1 57.00 0.0375 -0.0057 0.9811 0.01901 57. 50 58.00 0.0516 -0.0026 0.9660 0.03071 0.0524 0.0051 0.9724 0.04403 58.50 : ..

59.00 0.0294 -0.0125 0.9852. 0.05350 59.50 0.0076 -0.0044 0.98 19 0.04137 0.9720 60.00 0.0119 0.0026 0.07248 60.50 0.0081 0.0205 0.9775 0.064 54 0.9764 61 00 -0.0228 -0.0035 -0.0286 -0.0062 0.9779 0.03841 61.50 0.9649 62.00 -0.0274 0.0031 0._ 05 005 63.00 -0.0428 -0.0080 0.9736 0.01962 -0.0456 -0.0125 0.9649 0.01594 64.00 65.00 -0.0449 -0.0069 0.9703 0.01185 0.9755 66.00 -0.0435 -0.0026 0.10338 -0.0433 -0.0017 0.9738 0. 08960 67.00 68.00 -0.0362 -0.0047 0.9846 0.05981 0,9885 69. 00 -0.0286 -0.0102 0.06190 -0.0264 -0.0094 0.9939 0.00728 70.00 t rr i , , ., ·. ..

., · ,..: ,...

t!.'

7. 00 -0.0206 -0 19 (* Ac)4 _. 00 7 7 NIIuP'FR 21.7 IHC900! EXECUTION TERMINATIN; U)(JF TO ERROR CO[UNT F('IR F-RRfR F:I-OC-S --- END-'"-OF '-D-/T-A--SE'T .ONF'"i'JIT - 5 IHC217I REG. 0 PE( TRACEBACK FOLLOWS- ROUTINE ISN REG. 14 REG. 15 00C55RDO OOOn00000000n ( IRCOM 00055384 .

50053020 00000074 " MAIN 00002F98 ENTRY POINT= 50053020 .

:: '; - ----·-------'7---- - - ---- I ... NQ.1M .7Xe:,O7, V , P S 159.

tBAV_4=1 .- - ALFP 8.

ID5

VORTEX CENTER-46, i.

i ... ____. NORMAIZE _V..LOUc TY . -- TURBUL DIST i, INCH NORM SPAN AXIAL INTENS o, .

0,01026

0522__ _ t,,_ _00Q6_ 0 . 9845

34,00 0.0513 0.0125 0.9783 0.01102 0.01073 36.00 0.0540 0.0150 0.9811 37.00 0,.0525 0.9778 0.01214 0.0192 0.9907 38.00 0.0521 0.0246 0.01228

i /

0.9911 0,01265 39;.00 0.0521 0.0281 40, 00 0.0504 0.0360 0.9846 0,02425 41.00 0.0508 0.0321 0.9725 0.03067 0.9769 0.01907 42.00 0.0500 0.0474 42.50 0o0 546. 0. 0494 0.9995 0.02222 0.9923 43.00 0,0605 0.0617 0.01802 43.50 0.06.78 0,0762 0.9915 0.01962 ; %'"" 0.9869 0.,026.15 .......... _ o_768._.

_,_ 8_53

i, 0.9756 0.03210 44.50 0.0968 0.1083 45.00 0.9833 0.05771 0.1109 0.1204 445. 50 2___Q,_2._Q 5 086 0.9903 0.08509 0.2039 0.0066 ,~ 46.00 0.9667 0.06853 r-_ 46.50 0.1730 -0.1307 ,.9811 0.05255 0... :... .15.Q .. _.__ 89. ..

V- 47.50 0.1143 -0.1675 0.9932 0 .03290 0.9960 0.02492 ,: , s 48.00 0.1022 -0.1569 48.50 Q___,9874 .. _....Q_,22..2. 9L.

.. 1..._,1 _02 ___1___L

0.9833 0.01907 49.00 0.1015 -0.1405 0.01577 ' _- 49.50 0,0917 -0'.1262 0.9890 Q.,01435 __0..9906 0.0771 -0.,1059 0.9984 0.01150 51.00 0,0700 -0.0977 0.9891 0.01048 52.00 0,01145 53,00 .. _0 636 -O 00797 0.0632 -0.0758 0.9923 0.01332 54.00 55.00 0.0630 -0 .0750 0.9878 0.01279 0.0611 -0.0667 1.0001 0.01355 56.00 58.00 0.0633 -0.0624 1.0046 0.01258 _. 60.00 0.0608 -0.0599 0.9959 0.01274 ._,.__OQ00 Q 0..o. 01271 ! 62.o00 ._. _.0 5 94 -0. 0545 .;.,?,f','I

: I

i t V ,FPS=1.59.

JB LAV42 .... __.... X= 67.7 ALF= 8.

!

VORTEX CENTER=61.60 1 .

..- .. ' NORMA'LIZED VEALI-TY TURBUL - ' ' DIST AXIAL INTENS INCH NORM ' SPAN 44.Q0Q __._ .o6_. -OQj332 ..0.9679 0.01128 0.01074 46.00 0.0823 -0,0321 0.9700 0.01159 - -. ' 48.00 0.0811 -0.0312 0.9722 0,01223 50oo00 0.0814 -0.0300 0.9681 0.01268 51.00 0.0844 -0.0300 0.9720 52.00 0.0851' -0.0296 0.9732 0.01185 .0.9631 0.01243 j 53.00 _ 0.0878 -0.0294 0.01219 -0.0263 0.9728 54.00 0.0910 0.01168 '~. 55.00 0.0966 -0.0231 0.9678 0.01292

=56.00 0_ 1063.' -0:0216 _0.9658

56.50 0. 11'.4 -0-.0197 0.9723 0.01239 0.12i3 '--0.0221 0.9814 0.01193 , 57.00 0.01275 -5750 7 .... .L_ . 2_-0- 0202 0. 9867 .

Q 1 58.00 0.1389 -0.0169 0.9777 0.01591 0.01843 .. ;' 58.50 0.1527 -0.0100 0.9768 -0.0037__0.9815 0..02090 59.00 . .. 0.1860 59.50 0.1996 0.0053 0.9694 0.02'645 60.00 0.2201 0.0059 0.9679 0.04170 I, L_ 0.07067 - __65_ _ _,__.... 0Z2438 _.,,q.00192 0.9940 61.00 0.1834 -0.0500 0.9721 0.11416 ' . 61.50 0.0289 0.0110 0.9837 0.13834 -0.0024 1.0216 0Q.,1353 62.00 _-0Q1243 62.50 -0.1113 0.0179 0.9858 0.04216 63.00 -0.1261 0.0046 0.9927 0,05858 63.50 -0.1096 -0.0051 0.9766 0.03989 -0.0855. -0.0075 0.9822 64.00 0.02983 -0.0075 0.9677 0.02046 65.00 -0.0688 66.00 -0.045:8 -0.0175 0.9768 0. 01595 67,00 -0,0378 -0.0179 0.9809 0.01219 . 68.00 -0.0294 -0.0160 0.9761 0.00923 69.00 -0.0170 -0.0216 0.9862 0.01081 -0.0387 0.9999 70.00 0.0172 0.01038 72.00 0.0011 -0.0198 0.9761 0.01020 TO ERROR COUNT FOR ERROR NUMBER 2i7 IHC900I EXECUTION TERMINATING DUE - END OF DATA SET ON UNIT 5 IHC217I FIOCS REG. 14 TRACEBACK FOLLOWS- ROUTINE ISN REG. 15 REG. O REG.

. : 1, i . t.,, L 1 NRM Y/C= 4.00 AF=1 ,F n ____IEI 2- TR AV I 0 .... .-.. - . I VORT'EX CENTER=9,1685 ,i : ij NnARMAI T7Fn VFLncTTY _ ___ 0DIST , ; ,-' TURBUL .I INCH NORM SPAN AXIAL- INTENS 88500 . i O!OnQ6 -n,0141 Q, QAR . n ,.nnnnn_ _......

'' ' -} . 0.9-923 -0.0001 -0.0139 0.001000 89500 .

-O.000 1 -0.0195 1.0005 0.00000 90000 -0.0266 90200 0-0-00QopO -0.0000 -0.0312 0.9968 0. 00000 90400 I I 0.,0042 -0,0433 1.0041 0. 00000 90600 A A11 _n -ncs A A1 nln n nnnnn _an Qnn 7; 0 Ai O* - X .*U _W _ .L La' LI IID4 s-1 I- U- I - . I ii 91000 0.0048 -0.0532 0.9925 '.0.00000 91200 -0.0114 -0.0634 1.0183 0.00000 --- 9-3.-- -..... -00 !&. ....- QO L1 . L._9._9 .3.....0 ......- _.. 00 91350 -0.0108 -0.1099 1.0209 0.00000 91400 -0.0248 -0.1360 1.0327 0.00000 914.05 -_ 0 02. . . -024' -16 1___.04 DD.0D0 L........

-:; 91500 -0.,0312 -0.2020 1.0757 0.00000 7I 91550 -0.0469 -0.2315 1.0972 0.00000 --160-. -_ 0_ 3 .- n,-.1 7__--22 6__1 . . ... 1_1382-..... __.0, 0.000 00 91650 -0.0981 -0.1291 1.1862 0.00000 91700 -0.1061 0.0686 1.1718 0.00000 9!s75n -n n A N I I - 1 .1 1.

____l_410llQ 0. n...

' _,.

91800 -0.0879 0.1499 1.0988 0.00000 91850 -0.0334 0.1339 1.0869 0.00000 __919Q.._ .0.0142 0.1217 1.0547__ QOQ 00....

v 91950 -0.0175 0.1124 1.0455 0.00000 92000 -0.0116 0.1058 1.0152 0.00000 i 921Q__ _-onn-82 O. nq72 1. nn24 n On nonQ aGAa0 n nnnnn 0n77 n n _-A -nnI :) r) Aro. n -U .*UUL U.0U C U.. V Ue. UUUUUo 9"ouu ......

-0.0067 0.0767 1,0026 0.00000 92300 -- Od039 __0&096 1.0016 nn _ 00. 0 0 _924n00 i· -0.0029 0.0567 0.9972 ,0.00000 92600 -0 .0001 0.0555 92800 0.9957 0.00000 -0o.0007 0.0479 99 0 .00000... ... --930-An -0.0023 0.0397 0.9917 93500 0.00000 94000 -0.0046 0.0333 0.9899 0.00000 .0.__ .... 0.00000_ 95800 -0.0052 0.0191 1.0000 0.00000 YIr-. . _Fn/ AI r-12 AVl eFS.=.1Q.O ,_. - .--.-.. ZRAUIZZ-1 VORTEX CFNTFR=94793 _NIRMALJZF_ VE.LOCI TY_ ;. ~ .

TURBUL n1ST SPAN AXIAL INTENS INCH NORM n oonl nnn/n n ns2o n 978G 0.0308 1.0016 0.00000 97000 -0'.0296 .0.0313 1.0010 0.00000 96000 -' -00446 AI /'1/'1/'/' -- O. 9-9-9- - -..- 342- 0.0350 1.0037 0.00000 95600: :, -0O0603 -- 0.0955 0.0322 1 ·0044 0.00000 95300 1.0014 0o-00000 . ..- -...

- 0 1Z 229 0.9911 0.00000 95150 -0.1418 0.0385 :,· 0.0345 1.0004 0.00000 95100 -0.1584 (V-A 2O 1 ' A7 i n nnnnn n ---9-50504 -0. 1778 0.00000 95000 -0.2055 0.0432 1.0233 94950 -0.2168 0.0146 1.0562 0.00000 _ 0.0.0. ...- 94900.- --0_ 1e 0 QAQ I-......l...

94850 -0. 1535 -0.0792 1.1544 0.00000 94800 -0.0171 -0.1538 1.1659 0.00000 -9-75 50 0.-1075 0:1610 .49 __00O0 94700 -0.1758 -0.1008 1.1100 0.00000 94650 0.2178 -0.0516 1.0811 0.00000 94600 Q0 029 -0_n - 3 nfi ' n O , nonoQ__ 94500 0.1-745 0.0034 1.0259 0.00000 0.0103 1.0133 0.00000 94400 0.1471 .9_4200___ 0,1194 ._... nn_ .. 1 _ 5 . 001 __ 0 m.0000 .

94000 0.0978 0.0085 1.0027 0.00000 93800 0.0825' 0.0085 0.9994 0.000000 93600 _0iA.0660 0_0089 L l - 0n4 , onnnn 93400 0.0552 0.0119 0.9945 0.00000 TRIAVln _I NRM XL..... . . ALf .=_.. 4 .. ES.L .

VORTEX CFNTER=95200 .. NRM AI T7EDF VFLOClIY__ ._ _ DIST TURBKJL INCH NORM SPAN AXIAL INTENS _ .qq9331. al. n 'q 0 i 36_ -.. _8_ . _ 0. - S..

98500 0.0077 0.0188 0.9889 0.10472 98000 0,0070 0.0236 0.9834 0.10468 -. 750__9-1 0D..59_S- _...0.J253 ..... _0.9859.. _ _...0. 10447 97000 0.0075 0.0328 0.9892 0.10430 96500 0.0077 0.0455 0.9931 0.10413 96000 n 0066_ A 0_062 3 Q 3_-- .. I9 1_6...

95800 0.0027 0.0804 1.0010 0.10312 95600 0.0008 0.1152 1.0101 0.10169 ... 95 5 0 02 L..___1 J7 ... ._ O 126____1_0722 8 ___ LQ2.5_..53 95400 0.0074 0.1557 1.0640 0.10563 95300 -0.0022 0.1886 1.1298 0.11337 _q.250 - 00nnF 7 l0 1949_.1.146 .__.281_.____ .2 95200 -0.0473 ·0.0326 1.1776 0;18001 -0.2103 1.1532 0.13672 '., 95150 -0,0414 __-Q2. 8R0 .__. 1042 _ Q ... 12094 95050 -0.0001 -0.2740 1.0799 0.11763 ., 95000 -0.0018 -0.2274 1.0662 0.11684 -0.1508 1.042.5 0.11252 _.n_ 0 .0nR03 94800 0.0043 -0.1055 1.0302 0.11275 ., 94700 -0.0003 -0.1031 0.9963 0.11533 _9_46_i D_. - 00039. -0. 101Q _ 1.Ol2._ O._1042 94400 -0.0001' -0.0772 1.0106 0.10960 94000 0.0063 -0.0563 1.0085 0.10761 _9,3.O .nn R84 -08.0343 0.9998 0 . 1072-_.

-0.0236 1.0000 0.10731 92000 0.0093 V.F P -= 1 nn TQ A11 4 .1..

L X/C=- 2.nn ._. Al F=1 2 SPAN VORTEX CENTER=95500 ____ NORMAL ZE VELCITY_ DIST TURBUL -) , i<Sk INCH NORM SPAN AXIAL INTENS n0-157A3 9900nn0 0.422 -n-n009 n9899 0.10720 98500 0.0501 -0.0132 1.0389 9800'0 0.0495 -0.0043 1.0275 0.10652 - 0 -0 0006 ----- 035-3---- 0.--06672 7500-- 0,0 519 97000 0-.0559 0.00'43 1.0366 0.10686 0.0595 0.0087 1.0478 0.10712 96800 00645 0 0162 .- L 0427 o0n7 1 _ .7 .

-96600 96400 -0.0690 0.0182 1.0386 0.10769 96200 0.0855 0.0241 1.0414 0.10897 96100---0 0.0994 0 0268 --1.0571 -_ .lQ98_.......

0.11294 96000 0.1139 0.0316 1.0533 95-950 0.1219 0.0332 1.0539 0.11442 95900 0A:i37 ' 3 .0o34 1:0551 pn -15 1 95850 0.l-1.566 0,0440 1.0719 0.11882 95800 0.1797 0.0458 1.0709 0.12353 --- 9 750 2117 0.076 -- L Q9 0 05 127927 .. .

1.1059 0.13142 95700 0.2369 0.0697 0.:.2751 0.0858 1.1246 0.13729 95650 1.1A11_ N014241 95600 0.2981 n0n:076 0.2508 0.0784 1.2054 0.17599 95550 -0.0076 0.0128 1.2475 0.22802 9.5500 -- 9-5450-_ -n 2294 -n, 1 ,_ n9 _ _.0__3. .......

95400 -0.2866 0.0462 1.1515 0.09797 95350 -0.2647 0.0463 1.1198 0.08408 n-....

_5300 -0.2298 04! 0 110 n67 n, -0.1651 0.0322 1.0665 0.08849 95200 -0.1355 0.0232 1.0416 0.08972 95100 955000 -0. 1122 0I02.2_1. n4Q _ N0499L66.---..

-0.0931 0.0198 1.0402 0.09420 94900 94800 -0.0813 ' 0.0092 1.0420 0.09593 94600 -n 0617 0 0084 -061 0 2 3 ... _ _....

-- 0.0501 0.0094 1.0412 0.10058 94400 94130 -0.0406 0.0085 1.0519 0.10181 I i --U--h l. ·,.. lo·-pl*-- *U·_i .·.-· n. I- . _r--.. --.- _I-_r_· _.i*.

KInDm TX)I= 0.0 fi TRAV1Dr n AlF f=12.

11 ._+..P.S .-.1.Q0. ...

VORTEX CFNTFR=95210 _N - R.._ .__Z F D V_ LELOLLTTY ...

DIST TIJRBUL INCH NORM SPAN AXIAL INTENS OO3Q ' -f-D,_lCA D -. -nn7A - I n0446 f'11l3AR 98500 -0 0'005 0.0047 1.0333 0.11315 98oo00 01.0017 0.0100 1.0391 0.11325 .. , 9Q75 00 _ ... __=-' ]"~-/'~l. rO, 01%8_ .i.1_03_81. U0.1139_1.

97000 0.0071 0.0242 1.0473 0.11332 96500 0.0093 0.0383 1.0435 0.11452 q^nDn D012 3 0. nO30 17 ........ l3.

95800 0,0047 0.0836 1.0425 0.11136 95600 -0.0048 0.1173 1.0613 0.11055 s -__90 ' lO_,J12_IZLA____Q ,_! _65_ 1.J .. 4 0.,_10_6_95..

95400 -0,0867 0.1793 1.1282 0.10095 95350 -0.2073 0.2082 1.2020 0.10019 S953DDn -0.3007 0.2?147 1.338 0LL.. ....

95250 -0.1934 0.1312 1.2068 0.16509 95200 -0.1447 -0.0405 1.3327 0.11988 _.9515_ . ... ... 46 - 0 26_ .. ._. L9QO_ 44L.6.12.5 95100 -0,0182 -0.3912 1.0994 0.13591 95050 -0,0292 -0.2069 1.1051 0.12223 ,50f) ... -n,0n3Qc7 -0.17A5 1 A31 n.l 1 83....

949'00 -0.0322 -0.1302 1.0380 0.11821 94800 -0.0241 -0.1051 1.0185 0.11806 .__94_70_0.. -0 .0155 -0.084 10142 __ 011949 94600 -0,0081 -0.0722 1.0095 0.11924 94400 -0,0021 -0.0552 0.9968 0.11945 9A4jnOQ. n.An o -n. 03gl .q9974 1 982 .* , 93000 0.0119 -0.0165 0.9974 0.11995 92000 0,0131 -0.0107 1.0000 0.12054 k-.

i, .. ' ITRAVl06 SPAN Xr/C= onno Al F=12. v.FEp=lnn... .

~. .. ..1

VORTEX CENTER=95400 : I __ ____O1RAJ.-LZ-ED V EL-n I T-Y . _ _ r.

DIST TURBUL i NORM SPAN AXIAL I NCH INTENS n-aQQ7 -anA21 aOann n RA1 nA -nn47 : ) 98200 0.1058 -0.0139 0.8269 0.19386 98000 0.1.085 -0.0096 0.8309 0.18419 -9-800--_- 0.,1032 0 0016 -- i___n--3 - . -9-62-6- i 97600 0,I006 0.0051 0.7764 0.19455 * ,t 97400 0.1005 0.0083 0.7846 0.19481 97200 01a023 0.0124 -_-0.7992 __ 1 87 A7 Iii.

97000 0.1056 0.0181 0.7899 0.18924 - l.

96800 0.1088 0.0234 0.7965 0.18491 96600- 01130 0 -0332 _.n .0795 0,17871 _.....

96400 0.1184 0.0411 0.8242 0.16960 l' 96200 0,1234 0.0522 0.8439 0.15656 ni -1:aQQ n, R63 n. 4R49 0. 0567 .96000 0.1382 0.8814 0.14318 ' L 95900 0.0633 0.8982 0.1462 0.13778 nrn na -- 95-800- _.L364-7.

0; 0647- 95750 '0.1557 0.0614 0.9307 0.13621 ~J 95700 0.1631 0.0563 0.9349 0.13681 An 17 2 n tn ./.") 1 V1Ac1 a -n n Y "_--:'U '_ -- I_ If' I'" (I I It I '_ 95600 0.1870 0.0289 0.9558 0.14091 95550 0.2014 -0.0107 0.9846 0.14402 ., . j -&9 5-Q0-0 0 1781 -0= 7Aln - lnn __ n0 , 5760_ . ..... .

95450 0.1180 -0.1916 1.0161 0.17468 95400 -0.0092 -0.4534 1.0850 0.16988 !1 070 n-141q - 95350 -0.1209 -0n.3206- 95300 -0.0762 -0.1820 1.0632 0.14163 I 95250 -0.0954 -0,1001. 0.6918 0.20170 .. I _-95200.-- -0 -2Q41 -Q_ 03zn.. 1,0429 nl,_022_4 ......

95150 -0.1687 -0.0122 1.0284 0.10557 95100 -0.1377 -0.0032 1.0172 0.10867 95000 -01 '04 3 00055 O1Oq 012^3 --- 1..

94900 -0.0790 0.0090 1.0089 0.11584 94800 -0.0608 0.0075 1.0126 0.11764

n, nln n . 9QQ

4An60Q .19b_1 q 94400 -0.0294 0.0080 0.9959 0.12094 94127 -0.0231 0.0090 0.9945 0.12231 TRAV In 7 _NnBM , XLC- =Q_, 2 s A1 F= 2 _V, FP=1 Q.__ .

VORTEX CENTER=95310 nrC Tv NnRMAI T 7Fn VFI . 1 L _s _ __ _ _~~~~. I DI ST TURBUL .%-J INCH NORM SPAN AX TIAL INTENS n 1 41Q -n,_1 qaw s5240 1 .42nl . 140572 __o __ 95250 0.1480 -0. 1921 1.4162 0.14085 '%.' 95260 -0.1914 0,Q 1463 1.4187 0.14067 -n. lI9Q 1 -416L .13648 95280 o.0984 -0.1986 1.4271 0.13448 - 95290 o .05 87 -0. 1894 1.4191 0.13135 -n.MQ44 95300 1 .4A41 0n. 1 246 n 95310 -0.0327 -0. 0765 1.3957 0.12391 95320 -0 .0901 0.0465 1.3929 0.11780 __95331 -Oo 1£586 -L. 3925 : I 95340 - -0.1579 0.2500 1.3825 0.10642 k..; 95350 -0.1376 0.2913 1.3764 0.10973 I1, 3n7n6 [ln. 2 Re C 1 eq24R n0,11492 .... .

95370 -0.0636 0.2584 1.2565 0.11787 .: 95380 -0'.0438 0.2468 1.2421 0.11326 _-95390 -002!11 0-243 5 -1.244 L;12.1Z28 ......

95400 0,00'89 0.2345 1.2201 0.11133 "-' 95450 0.0532 0.2025 1.1511 0.11351 95500 0_'600 0.1666 11 ncOn . 1 579.

95550 0,;0597 0.1478 1.08.23 0.11668 95600 0.,0574 0.1287 1.0701 0.11740 95700_ o0.0l11 0.0946 _ .0537 _ . 11842..

95800 0';0483 0.0841 1.0513 0.11863 'v 95900 0.0454 - 0.0712 1.0472 0.11817 , 96000 0.0Q4 2 4 0,0544 1.n^ n7 .1.187.

96500 0.0358 0.0338 1.0263 0.11908 98000 0.0253 0.0088 1.0105 0.11926 qq30A 0,_F I ,n240 -A) flC) 1R 1, I0000 0. _ 1 9_. _7. . ...

, . .

,., i j.

F=-1 0 /Cr =-n ?I ^ 1 Al TRAV/1 O C DPANi nn V',EP-=l VORTEX CENTER=95420 Nn RM AL T ZEILE.SEL 0 CI.TY__ i DIST T U RB U L t

r

INCH NORM SPAN AXIAL INTENS Q 17Qn 0.752 0:0!_ L12- 1. n! 0q n _-.9 1 4 .........

.. '1 96690 0.1778 0.0360 0.9998 0.13856 96190 0.1765 0.0536 0.9825 0.13789 -- 96090--- h.!744 ...... _--, -. 1-37.08.- -.- - ....- 9----0 --. 9683- -

95990 i

0.1704 0.0669 0.9638 0.13701 95890 0.1739 0.0749 0.9603 0.13698 9 570 - 0.1805 - - £X-0.07 0-7-!a 0-1 3-5-8-- .. ...--.

I 95690 0.1886 0.0883 0.9736 0.13785 . I \-' 95640 0.2005 0.0909 0.9780 0.13959 --- -- 9-55-90 4 - 2238 2--- 0- 092 -497/-9s8- -.- 01-425.7:-- I 95570 0.2430 0.0948 0.9959 0.143 R6 I 95550 0.2630 0.0950 0.9972 0.14645 I - n_ 1 R7 0.2880 0.0969 0 997a 95510 0.3231 I 0.1157 1.0124 0.15196 iL 95490 I 0.3339 0.1022 1.0454 0.15529 n 1- &77n -- 547-0- --A 0.3680 -0. 0887 !1322 95450 I 0.3818 0.0460 1.2208 0.17268 95430 0.2198 -0.1643' I 1.3989 0.18792 7 RA -1 _l0 1 _1 -- L h I na 1 2a 95390 -'0.1147 0.0151 1.2639 0.12091 _,- 95370 -0.0611 0.0524 1.2130 0.13005 nL 1 RRR 9553 50.

. 1n53 1L.a69 95330 -0.0283 0.1330 1.0290 0.16661 95310 -0.1013 0.1629 1.0561 0.15709 O952n '-n '171Q n_ 1 7'7 1 nQA7 n 1 R7 E 95270 -0.2462 0.1807 1.1078 0.106'16 95250 -0.2641 0.1841 1.1172 0.09522 nA. 172 2 _aQaI - 523 -0.2591 1.0995 95210 -0.2486 0.1486 1.0859 0.09051 95190 -0.2300 0.1367 1.0863 0.09256 95140 -0.1862 ' 0098 1 073 3 0,09729 ....

95090 -0.1586 0.0775 1.0591 0.09991 94990 -0.1157 0.0523 1.0540 0.10609 -489Q4 _ 9.0-- . - 87 03-74 1.0A43 ._ n.10_0..S7_.

94790 -0.0711 0.0252 1.0329 0.11269 94690 -0.0582 0.0200 1.0177 0.11348 941 90- __ -0 .031 3 nln1A 1n 18&..........

93810 -0.0212 0.0097 1.0044 0.12013 i MR M ALEk1a 2_._ .M..E P...M 1 ]0f .... .i I . -tRA ula9o - X/r.Cm-A Q-_ 1 5f ..

.

.I VORTEX CENTFR=95400 t -; l :Li n. I TT lNnIRMAI T7Fn V:FI DIST TURBUL L!

NORM SPAN AXIAL INTENS ~ INCH 9538Z n. 1 A70 -0.1251 1.2431 01Q337. .... ....... " .i .I, 95392 0.2245 -0.0895 1. 2600 0.13286 ii I <k.. 95402 0.2908 -0.0257 1.2477 0.13545 t 0,0976 _ 13709.....

-- 9-5412 _1.22_422 i.

0.2098 1.1804 0.13809 95422 0.4583 .. 95432 0,47.91 0.2782 1.1683 0.13610 n-2685 n 13 1.34 95442 0.2449 0,12828 95452 0.3422 1.1719 k.l 95462 0.2256 0.12375 0.2770 1.1589 95472 Q.22&56 ___.A21 52 -. 1.548. _0L1.202-4 ....

95482 0.1831 0.2068 1.1469 0. 11730 K.-i 95492 0.1574 0.1917 1.1360 0.11640 n 1 R1 4_ nc 1 l1 2 ..

955fl2 0 1- 3'38R 95512 0.1173 0.1772 1.1273 0.11527 <.. 95522 0.1081 0.1734 1.1288 0.11390 _ 95 542 n0.0892 O+ 1548 _L 1 1 25 -0.11350..

95562 0.0804 0,1448 1.1158 0.11339 K<, 95582 0.1319 0.11337 0.0692 1.0929 9.s560 n-Ola1 .1 209 1.099R _, 11324 ..... : ............

., i 95622 0.0578 0.1129 1. 0947 0.11341 , K-J 95642 0.1052 1.0893 0.11284 0.0466 · 95 662- 0,0425 _ 112.5_6 ....... ..........

1.0_8_42- 95682 0.0418 0.1004 0.11277 1.0801 '--' 95732 0.03.82 0.0914 1.0792 0.11303 q57_82 1 .n7n8 95832 0.0278 0.0689 1.0678 0.11320 v.- 95882 0.0237 0.0664 1.0611 0.11305 1 .0456 n.]1.289.t.

-95982- , -05 96.. .

96082 0.0153 0.0462 1.0468 0.11347 ..- 96182 0.0119 0.0443 1.0430 0.11332 96482 0 .073 0 0333 !03 1 1 0 1!3L5-1_ . ............

97482 0.0113 1.0141 0.11427 0.0015 '-i 98482 0.0028 0.0073 1.0000 0.11481 CDAMI -n TA'11 1 nI AIl F=l--17 V.:FPS=:1

X/rJ-n )-..-... . ....... q I

VORTEX CFNTER=95350 . .~I,. ._, TT nIADMAI T7lFl IllFnr C t! i TURBUL DIST NORM SPAN- AXIAL INTENS INCH 1 7AAA n _ I_291 ...

0 -17?6 .00!25 i 0.0272 1.2398 0.13195 : 96715' 0.1877 . :1 0.1-875 0,0442 1.2177' 0.13147 96215 -.. -- 1-a3-26 96415 0.0475 .s !o 860 1.2065 0.13096 96015 Q.1870 0.0593 i 0.0651 1.2172 0.13110 95915 :0.1906 1 .

0 nl 1 I OI q. l '7"7 7nnq A 12RnA A 1 w - U-i-C B@w -WI 06 .Uf· ; -- - 0.0859 1.1878 0.13063 95715 0.1869 95665 0.19116 0.0896 1.1846 0.13090 2--1-4 357-3..

-O.1679 ' ___O1l -1J - 0.13578 0.1712 0.1094 1.1186 95615 0.13566 '->' 95595 0.1679 0.1098 1.1206 0, 1 12 1. I I 3- 95575 0Q1 34422 1.1254 0.13622 955555 0.1745 0.1140 0.1202 1.1227 0.13639 ! k. 95535 0.1786 -- -0-4.I 221 -L.4-3.09 ..... .13683.

--- 95-51-5-- O: 18238 0.1300 1.1322 0.13703 95495 0.1880 0.1318 1.1304 0.13861 :, ~ 95475 0.2022 A_33 n_ 1 11 71 _11 n_l QAQ -95455- 0.2531 0.1553 1.1312 0.14139 95435 0.1910 1.1272 0.14251 ~-;' 95415 0.2857 1..1l403 0_.1470L

0o3751 I.2277

95375 0.4211 0.3224 1.2323 0.15438 0.14762 L-' 95355 0.1344 0. 3138 1.3418 I 95~375- --- 03861 0.3l284 1.33 0. 155 7 5 95355 0.1545 0.3165 1.3380 0.14872 95335 -0.1574 0.2963 1.2929 0.12772 -- 0.2339 026733 12617 - 0_-0O384............

95315 95295 -0.1947 0.2207 1.2079 0.10467 95275 -0.1723 0.1924 1.1806 0.10427 95255 -0,1599 0 1751 l1561 156 I 04-4- -1 95235 -0.1482 0.1558 1.1280 0.10536 95215 -0.1339 0.1412 1.1144 0.10584 ----- ....- 1 176 -- 0 1 16 1 7_...3.... - 95115 -0.1082 0.0965 1.0701 0.10767 1.0355 0.11020 - 95015 -0.0855 0. 0682 1 - n- 32 1 n. 11215-- - ----------- 94915 .0..072 3 0.0375 1.0130 0.11271 94815 -0.0645 -0.0494 0.0269 1.0037 0.11463 ~.~ 94715 -n -n9tA n nl ln _9A4215- _....

.0_,_11_802 N.

' -- 00165 0.0075 0.9843

o. 118 87 .... .... . .1I

'I i' .I 'd i ,!

'I ' . _- . - . .

Is i L i!

I .

.. --- .

.... _ _ .. .

I _ ' I ' k, _ . . . _ .

VY r I n,,--/5 79 A 1 1 l 91 10nn TDAV1 InDMa AQrl V.I FC=- .... I. . 1 I VORTEX CENTER=95500 i TTV AlnDMAI T71Fln Il nr DIST TURBUL INCH NORM SPAN AXIAL INTENS i i N' *or. O' n nflgA A 1 2Q 012-667- 95492 0.1056 0.1129 1. 1088 0.12667 1.1177 0.12535 95502 0.0954 0.1156 0 .1114 --- 012388.

0.12041 95522 0.0717 0. 1138 1.1383 0.0589 0.1054 1.1357 0.11903 95532 95542 0.0501 a: 1036 1.1340 95552 0,0451 O. 1040 0.1040 0.11629 Ci 95562 0.0383 0.1034 1.1349 0.11569 · : 9-5572- Q0955_ 1 397 0.0311 95582 0.0276 0. 0933 1.1338 0.11542 - ., 95602 0.0185 0. 0943 1.1234 0.11476 1 1147 -956222 0_ '0!57 n: Ra6 7 95642 00.0150 0.0765 1.1082 0.11544 0.0793 0. 11486 'i' 995662 0.0088 1.1043 -- 956482- 0.0061 1:0974 0_. II.4B 2_ 0.11458 95702 0.0013 0.0627 1.0968 v- . 95722 0.0006 0.0591 1.0951 0.11469 n .1 1514 n0 QA7 1 .nR17 0 .0020 1.0806 0.11516 95762 0.0575 ' .. 95782 0.0508 1.0717 0.11550 0.0014 -. ..-0 0020 _1.nh73 0._11553Z -9-5-832 - 95882 0.0008 0.04'58 1.0575 0.11588 ,-,' 95982 -0.0005 0.0367 1.0429 0.11606 0 - 0342 . 0289Q 0-1163-7 96282 -0.0024 0.0276 1.0163 0.11677 -~ 96482 0.0271 1.0000 0.11731 -0.0010 c, · , . ,..

nn -IQ .. L4.2. SP'N V.IsFP=l XY/ C =--DO =I 7 VORTEX CENTER=95320 A I T 7 r" ', WC - nr T TV hi f)Oa c DISTN-- ·- L, I - !I.VLU.L.. L.._.. t.u J.L.. Y~ DIST TIURB UL k,, I-NC H NORM SPAN AX I AL INTENS _-,22-A_ Q..04a5o -L 1J 6_L5.

95690 0.0891 0.0469 1.2218 0.11727 : 95640 0.0945 0.0590 .1.2178 0.11745 __0_.5029_ _1 .212 - _...0_11774 95600 0.0918 0,0545 1.2140 0.11766 ~.J 95580 0.0930 0.0591 1. 2022 0.11778 n .9g4? 0.0592 1.2046 n.

11802 . ..

95540 0`0906. 0.0635 1.1967 0.11688 i- 95520 0.0906 0,0671 1. 2068 0.11673 __9550.Q_ 0. 0729_ _1 · L9_49 _0_,11_662 ..

95480 0.0747 1.1924 0.11734 * - * I 0 ~ 0 95460 d.085-9 0.0834 1.1954 0.11693 1.1911 95 q440 0.0864 ° - 1 L53&6, 95420 . 0oi799 0,0914 1. 1822 0.11553

i< 9d 5400 0o .0759

0.0982 1,1881 0.11503 O.1080 _._1.7_1761 . 11L5_75- 95360 0.-0726' 0.1195 1.1524 0.11782 -. i 95340 0.0593 0.1492 1.1771 0.11359 0. I 654 1 .1504 95300 -0.0613 0.1418 1.1347 0.10139 "; 95280 -0.0740 0.1252 1.1233 0.10102 -'0 · 0 0802 0.1091 0,10084 l_.__ 45 95240 .0'826 0,0963 1.1024 0.10117 :',J 95220 1.0958 ::.4-0794 0.0862 0.10193 rI : -, - qr nn . .n L:n.r n7i1 1 n7fl n 1 nvo7 --- o eL Zg!: t-sg{|'- .. *,--w - . . =llrl -t II t11/ .. . ------ 95180 072:8 ,0.0691 1.0741 0.10339 95160 -0-.0695 0.0651 1.0613 0.10397 95140 -0091 0.0620 1.0526 0.131 _ .........

95090 -- 00634 0.0492 1.0466 0.10438 95040 -0.0568 0.0416 1.0287 0.10556 Q4QQn -"nAn. ? ' 2 nfnAR I 01R4 n 163 __ ., 94940 -0-.0443 0.0282 0.9993 0.10775 94740 -0.0:344 0.0217 0.9872 0.10920 i. 45494_5 -0'.n0771 ol06i 0973 . 1 10 3_9...

94340 -0.0205 0.0122 0.9620 0.'11146 i .

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