Ice Accretions and Icing Effects for Modern Airfoils

Appendix A Model Coordinates NASA/TP--2000-210031 27 A1 .--BUSINESS JET AIRFOIL COORDINATES X/C Z/C X/C Z/C 1.0000_ -0.00033 i 0.00000 i _-0.00392 ....

0.82500 _ -0.01321 - ! 0.00050! -0.00006 0.80000 -0.01506 ' 0.00100 0.00137 --0177500 LL -0.01691 i 0.00150 0.00246 0_0-0.01876 _- - _.002_0337 0.00300 0.00471 0.72500 i -0.02061 0.7_0000] :o_ .... 0;00400' 0.00594.

0.67500 -0.02427 [ o oo5o6_ dio6691

0.650001-0.02610_ 0.00750 0.0087(

_6250o_:o.62788, old16ooi_ .... 0.00999

0.60000 -0.02953 i 0.01250! 0.01108 0.57500i-0.03108 0.01500 0.01212 0.52500 -0.03383 I 0.02500 ! 0.01547 0.50000i-0.03501i 0_03000_ 0101694

o_7_O_-bSJ3597_ - o.o4ooo i 0.o1956

0.45000 -0.03666 !0.05000! 0.02184 0.42500 -0.03706 0.06000 0.02388 0.40000! -0.03718, :0.075001 0.02670 0.37500 -0.03709 - _ .j 0.10000! 0.03066 0.350001-0.03681i _0.12500 0.03404 0.325001 -0.03643 i &.15000J 0.03698 0.30000 -0.03598'-- .I0.17500L0.03951 0.27500i -0.035451 0.20000 0.0416!

-0.03482_ i0.2250_ 0.04359 0.22500 -0.03410 i0:250000.0_04520 -0.03322i 0.27500 0.04654 o.2oooo i 0.175001 -0.03218L_ _ 0.30000 i 0.04771 0.15000 -0.03094! L0.32500! 0.04862 0.12500 i -0.02969_ .... _ 0.35000:0.04924 0.10000_ -0.02833 i 0.37500 0.04951 0.07500_ -0.02672i _00 T- 0.04956 0.06000 -0.02551, _0.425001 0.04942 0.05000 -0.02455i 0.45000 0.04915 0.04000 -0.02338' _0.47500_ 0.04863 0.03000 -0.02185 |O_50000 Oib478-9 ----1 o.o25ool-o.o2o9o i 0.52500 0.0468_ 0.02000i-0.01977+___0.55000 i 0.04555 0.01500 -0.01833 _ 10.57500! 0.04404 0.01250i-0.01748 _0.60000 0.04233 0.01000!-0.01656 i 0.62500 0.04042 0100750-01015471_ _di6gO00_ 0.03837 10.67500! 0.00500 -0.01386 0.0362: 0.00400-0.01299T 0.70000 0.033_)-7 0.00300 -0.01192i 0.72500i 0.03154 0.00200-0.01054 L0.750()0 _ 0.02901 !0.77500 0.02629 0.00150 !:0__0_0_9671 0.00100[-0.008621 0.80000; 0.0234( 0.00050 -0.007231 0.82500' 0.02058 !1-000004 0.00033 0.00000i-0.003921 28 NASA/TP--2000-210031 A2.--COMMERCIAL TRANSPORT AIRFOIL COORDINATES x/c ; z/c yac I z/c X/C Z/C _ 4 X/C i Z/C t 0.035223 0.029423 0.635551' 0.043928 _1.00000010.008649 - 0.349370-0.033927 0.041185 0.031511 0.648984i 0.042839 0.990740! 0.007881 . 0.335871 _ -0.033921 0.047581 0.033515- 0.662418-01041710: 0.980977- 0.007064 0.322380L -0.033840 0.054426 0.035429 _0.675855_0.040544 0.9707240.006200: 0.3089101-0.033732 0.9600030.005287: 0.2954-6_585 0.061730 0.037255 0.689294 0.039347 ........... I 0.069503 0.038992 0.702733 0.038120 0.948844 0.004332 0.2820571 -0.033411 _ . f + 0040642 !0.716173 O.036867 0.937286 0.0033331 0.2686951 -0.033220 0.077750 • _ _.___ 2 0.925373 0.002286! 0.255396 i -0.033018 0.086474 0.042203 i 0.729612_ 0.03559 0_131-500.001195! 0.2_0-0.032802 0_095671_ii_43677_ _ 0.743047_ 0.034298 0.900662 0.000006_ 0.2290701-0.032567 i0.105330 0.0450661 _0.7564760.032989 0.887952 -0.001095! 0.216091!-0.032306 i0.1154360.046372:0.76989510.031670 -0.032010_ I 0.1259640.047594! _01783298] -61030345 0:875058.0.862015 -0.003489:0'002281 0.1906420"203272-0_1-6691 _013688Y_ 0_48731_ " 0.796_ 6_029018 %1848852 -0.004715, 0.178234 -0.031278! 101i4817ii 0.0_- -0_1062710_027689 0.835594 -0.005957, 0.166084 -0.030817! 0.159781_0.050754' 0.823333 0.026365 .......... ± - 0.171677! 0.051649 _ 10.836583 0.025048 -0.030289 .0.822262-0.007211_ + 0.154228i -0.029705 0.808873-0.008473 0.142703 0.183822i 0.052471" _ 0.849759_ 0.023742 0.795441-0.009737 0.1315471 -0.029071 0.196182_ 0.052321 _0.862842 0.022453 -0.0283881 0.2087221 0.053863 10.875806 0.021182 0.781977 i -0.011000 0.1207951 0.768490 -0.012261 0.1104771-0.0276581 0.221416i 0.054424 i 0.888621" 01019933 0-754987 --0.013517 .... b 100617_ -0.026881i 0.2342370.054900 T 0.90i25410.018711 0.7_,1-474 -(3J314_3! - _09123_-63_Q_:_471"76 0._276 !0.913667_0..()1Y521 %.:f27956- '0.015cj94! -0_082-328 -0.025204 i 01260202- 0.055525" _ 0.9:_5817_0..-0_0 017144,3_4-01017206_ .... O_6!-0.024309 q O.2_2,_. O..055658_i O.93,7660'.-0-015266 0.7009121-0.018395 0.065958 0.949149 i 0.014211 -0.023373! i0.286525 0.0557191 i0.299796_ 0.055754i 0.960241i -01013201 0.687390 ! -0.019556 0.058473 -0.022407 0.673870-0.020686 0.051434 -0.021387 0.31312310.055776_ .0.970898 _ 0.012236 -0.020314 0326492i 0.055788' , 0.981090_ 0.011321 0.660352 _ -0.021783 0.044823 -0.019194 0.339889i 0.055780 _0.990794 _ 0.010457 0.646836_ -0.022843_ _ 0.038616i -0.0180271 0.353305 _ 0.055740 i0.999998, 0.009644 0.633332-0.023862 _ 0.0327921 -00167971 i0.366733! 0.055654 i -- .....

0.619810 -0.024838 0.027333 I -010154671 I0.380170 0_55512 ! !----- O_60630-0_ -0.025769; 0.022232!

-0.0140011 -_--0.393614_01055318_--- -- 0.59-2791- :0_26652i _ 0.0174901 0_57928f '0.027486i i 6.0_07_ -0.010609 0A20517 0.0548i9 T - - _ ....

-0:0-28267'i 0009 90

0.552262-0.028998 _ 0.005522i -0.0085581 ; 51011 1111ji iiii

0.538750:-0.029676 0.002576 -0.006619 _ 0.447428 i 0.054154 i -0.003357 _0.460880i 0.053752 0.525237 ! -0.030300 0.000617 i 0.0000021 0.511720 -0.030871 -0.0002781 0.474331i 0.053300_ _ ....

0.002726! i0.487778 0.052799 i 0.498201 -0.031389 0.000330 i 0.484678-0.031856 0.000330!

0.002726_ ..... _O.0.501_2210..052248 0.471153 -0.032270 0.001411!

o.0057231 10.514662 0.0516451 i 0.457624 -0.032635 0.0031231 0.008853 _ -_0.528100 0.050990!

0.005434 0.444092 -0.032952 0.01_07 _ i0.541535 0.050282i _ -__.

0.0_-781 _ 10.554968 0.430558i -0.033221 0.0083211 0.049523 ........

0.4170261 -0.033445 0 011711i 0.017531 0.568399i 0.048712. _ .......

0.047851 i 0.4304871-0.033624 0.015544i 0.020162 0.581829 • _ 0.046940 0.022656 0.595259 0.389952 -0.033760 0.019824 i 0.608689 0.045981 i 0.376420. -0.033855 0.024542 i 0.025013 0.622119 0.0449771 0.362894 -0.033910i 0.029678! 0.027260 NASA/TP--2000-210031 29 A3.--GENERAL AVIATION AIRFOIL COORDINATES x/c i z/c i I x/c ! z/c i x/c i z/c i i x/c z/c -1-.0OO00_-0_2-751: [0.47869i-0._985 r 0._86, 0.01082, _ 0.548380.0781:/' 0.9947"I -0.02723 0.46171_ 41 ' " -_ -O,0596 ! i 0.00653_ 6_ ! 0156558, 0_-_0 0.98894 _ -0.026951 _ 0.44476! -0 ,0_5 93 5-" l 0.0-1154! ().-020_66 i 0,5826_ 0.0752---a, 0.98271-0.02669 0.42788 -0.0589ZL L 0.0176_ _7_21 i 0.599671 0.97602-0.02645 10.41107 -0.05851i ; 002450_ 0.02836- 10._3 _ 0.96886 -0.02624 i 0.39435 _ .0.05796i I 0_-,03202! 0.()-3177_ 0.63322_ 0.06926 0.96123 -0.02604 _-0,37775 -0_.05732_ i 0.04009_ 0.03506! 0,_41 ().06682 0.95316:-o.o25871 i 0.36128 -0.05661 _ 0,048-691 _38:23_ 0_-6605 -0,06414 0.94463 i --0..0_ ,--C)-134495 ; ..... _ i- - + --'-- -:--- -0.05583 _-0.05782 0.04127 i 0.68211i 0.06115 0.93565_-0.02562' i0.32-879" _ __0.0674_5 0.04418_-_ 6-_ 0-[6_-77 _31 _- /0.312821 -0.05405! 0.0775_ 0_4_6 _ O_ -0-_05394 0.91638 -0,02_! 0.29704! _ _i{38816 _ 0.049_- _ 01=72845i 0.04963 -(_.90611 -0.02565 ! 0.28148i' -0.05203 i _9-921- &052181-- _- 0;64;,_)1

0.89542!-o.o2586 i (_2_ -0.050941 i 0_1107()i _-_ 0_

088432 -0.0262110.25108 _ 0.87283 -0.04980' L0.1226i-! ():_J_ 0.7714910.034-84 -0.02671 i0.236274 -0.04860_ !£)-:'1349_ 0.0592-6 - ()_:78_ 0-.02979 0_6_696-0.02739 i /0.221_ / -0._:_6! _54766T 0106_,Y W 0179_6d-&02488 0.84872 -0.02825 i !0.20751!-0.0_07 ! i 0.16076__0-:0636_ _ 0.81__20;16

o8361_3 L -0.02930 i 0.19358 -()_ _ 0_-7_3 ()_06-566_ ' 0.824611 0_01-567

0.823191 -0.03053 0.17998 -0.04335! 0.18805! 0.06763 i 0.83719i 0.01142 0.80993 -0.03196 0.16672 -0.04193! 0.20221! __ 0.849470.00744 0.79635 -0.03359i 0.15381 -0.04047 0.21671 o.o712810.8614_ 0.00372 -0.03548 014126 -0.03896_ 0.23151 0.07294 0.87308! 0.00027 0.78249 I ! [ .....

0.76838-0,03772! 0.12909!-0.03742! i 0.24661 0.07449 0.88438-0.00293 _o.754o4 i -0.04036 , 0.11730: I -0.03584+ _ 0.26198 0.07591 ! 0.89533i-0.00587 0._-0.04333 0,105921 -0,03422 i 0.27762 0.07720 0.90591:-0,00859 0.078_ 0.91611 i -0.0110{ 0.72468,-0.04641 _:00_4493_-0.03255, 0.29351 0.70959[ -0.04929 -0.03084 0.30962 0_7 _)-< (3_ 92591_ -0.01337 0.694181 -0.05170 i 0.07426i -0.02909 i 0.32594_ 0.0803-0! _-(316:3530 i -0_ -0.02731!

0.678491 -0.05357 i 0.06457 I 0.34245_ 0.08107 i 0.94426 -0_.0173-7 -0.02549; 0.66255 -0.055011 I 0.055331

-0 59130.o8169

I 0.952801 -0.01912 -0.646411 -()_05617 [ 0_4655, -0.02363 i ! 0.96090[ -0.02070 -_ 0.37597 0.08216!

06 o,o! -0.02169L -

0.3929410.08248 _ 0.96856:-0.02211 -0.01966!

0.41002! 0.08265:_ 0.97577i -0.02338

-005865 !

0,59703 -0-,05798 ! .... !0030431 -0.01749 0.42720: 0.08267 i 0:98252_F -0.02451 i -0.01515i 0.580311 -005917 - i O_016-35 0.44445 i 0.08252 . 0.98881 z -0.02550 -0.012571 0.56350 -0.059551 0.01016 0.46175_ 0.08221 i 0.99464 -0.02636 0.54661 -0.0598210.00475!

-0.00949 I

c)_ ,79o91 0.08175

-0.00516i 0.49645 0.08112 0.52967 -0.05997 i 0.00104i I 0.51379i 0.08032 0.51269, -O.._ _ 0.00000 0.000000 ().49569i -0_,5998! - 0.00069 o.o6_3_ i 0.53111! 0.07934 30 NAS A/TP--2000-210031

Appendix B Pressure Tap and Thermocouple Coordinates NAS A/TP--2000- 210031 31 B1 .--BUSINESS JET PRESSURE TAP LOCATIONS [Y measured from tunnel centerline] No. X/C Y/C Z/C X,_)_ Y (in_ Z _in) r - i I I - _ ....

1 ! 0.9700 -0.08331-0.0026 i 34.920, -3.0001 -0.094

3 0.9000'-0.0833-0.0077, 32.400 -3.65_2-77 28.800 I -3.000 -0.544

--_-_ _.7_33 _-0102_25200 -3.000i-0.806

6 i 0.6000-0.0833i-0.0295 i 21.600 -3.000 -1.062 7 0-_-0 08331 -0 03501 1_00_ -3.0.000] -1.260 -- I , .... "_+ "- _---'_4 ----_ .......

8 0.4000 -0.0833,-0.0372 14.400 -3.000! -1.339 9 0.3000-0.08331-0.0360 10.800 -3.000, -1.2961

__0001 -0.0833 -0.0_-_ -3.000 -11951

- 11 _. 0.10-00! -0.0833:70.028_4_13--6()011 i3._ ii--_ 12 0.0800, -0 0833, -0 0271 2.880 -3 000 -0.9761

___ 3 ! 0.06001 -0.o8#3_ -0 0255--__21_..60_ :3 00_.__0, -019i81

l 14 _ 0.0400 -0.0833,-0.0233__1.440 --3.000 ! -0.839 / 15_..i 0.0200, -0 0833 -0.0197 i _0.720_ -3.0oo_ -o:z09 [ 16 +oo_-0.08331 -o.o165 o.360_-3.oo0 i -0.594 0.0040:0.0833:0_o128--o_4 -3.oo6! -o.461 -()_0005_ _-0.0833_ -013073_ - 0_18_0-'- _3 [ 21 0.0100 -0.0833 0.010_0_60 -3.#0-- O_:J60

:00833! 0.0121 00 0.436

23 0.0200 -0.0833 0,0138 0.720 -3,000 0,497 24 0.0300i -0.0833i 0.0170 1,080_ -3 000, 0 612-

2_-6_ -O.O_3:_t 0.019_F- 14_5t -3-000_ -0-706 -

26 0105001-0.0833 o_i_o + -3.000 _ O:_ss

2.160 -3.000 0-86£}1 27 0.0600' -0.08333 0.0239'

2520_%.00d -&_51

28_io_.o833 616257 i

2:88 -- iooot-

30 0.0900'-0.0833 0.0290 3.246 -3.000 _ ! 3_ 0.1000!-_ 0.0307!

3.6001 -3.000_ 1.105 "32 -_0.1500_ -0.0833 0.0370 5.400 -3.(]00___ "11332 33 0.2000 -0.08331 0.0417i 7.200 -3.000 1.501

34___2500i -0.0833_45_2 9.000_ -3_00_.627

35 I 0,30001 -0.0833_ 0.0476 10.800 -3.000 1,714 36 0.4000' -0.0833 0.0496 14,400: -3.000 1.786 38-I 0.6000 -0.O_3i 0_4_' 39 -! 0.7000 _0_08-_ 0.0340 ,_ '! [X-0! lj2-2-4 40 0.8000,-0.0833! 0.0234i 28.80_ -3.000 0.842

41 -I o_ooo_ -o.o_o-o-1_9_32._6L -_.o6Qi_.4_

42 0.93001-0.0833 0.0090 33.480-3.0001 0.324 43_ 0.9700 -0.0833 0.0038i 34.920 -3.000' 0.137 0 r 1 .......

44 11 000_ -0.0833] .0000_3_6.000_ -_3:000+ ...... 0.000 -- ! .... I Thermocouple Locations 0_ Y/C Z/C i X, i(in) Y, (in) Z, (i_ --1 0-()_-0_. 600_ 3.000 -1.-022 2 0.0500 _ :0.0241 1.80-6 ] 3.000 ---0.868 _O.lOOOi 0.08331 0.0307! 3.60043__3.000 1.104

4 , o.o2 sW oZ o, 6

oloooo iooo÷ o

32 NASA/TP--2000-210031 B2.--COMMERCIAL TRANSPORT PRESSURE TAP LOCATIONS No. i X/C . Y/C _ Z/C . X,(in.) i Y, (in.) i Z, (in.)

1 0.9700 -0.0833 0.0061 34.920 -3.000. 0.221 2 _ 0.9278-0.08334 0.0027 33.400 -3.000 _ 0.097 3 0.9000 -0.0833 0.0000 32.400 -3.000 0.000 + .... ---- - 4 ;0.8000 -0.0833 -0.0093 28.800 -3.000 -0.335 5 0.7000 -0.0833 -0.0185 25.200 -3.000 -0.665 + .... -- 6 0.6000 -0.0833 -0.0262 21.600 -3.000 -0.943 7_ 0.5000- -0.0833 -(}))313 _ 18.000 -3.000 -1.128 -8 , 0.4000_-0_0833-0.0337 L 14.4007--3.000 _ -1.212 9 0.3000-0.0833-0.0336 10.800:-3.000 -1.211 100.2000 -0.0833 -0.0319 7.200 -3.000 -1.149 11 0.1000 -0.0833 -0.0268 3.600 -3.000' -0.966 12 0.0800 -0.0833 -0.0250 2.880 -3.000 -0.898 13 " 0.0600-0.0833 -0.0226- 2.160 _ -3.000" -0.814 14 0.0400 -0.0833 -0.0194 1.440 -3.000 -0.700 15 0.0200 -0.0833 -0.0148 0.720 -3.000: -0.532 16 + 0.0i00 -0.0833 --010110 0.360 -3.000:-0.396 17 - 0.0-000- -0.()833 -0.0003 0.000; -3.000 -0.010 t .....

18 0.0050-0.0833 0.0113 * 0.180--_ 0.408 19 0.0100 -0.0_8.33 0.0161 0.360 -3.000i 0.581 20 0.0150+-0.0833 0.0198 0.540_ __-3000_-+__0.712 21 . 0.0200-0.0833 0.0227 L 0.720 -3.000i 0.819 22 0.0300,-0.0833 0.0274 1_.0801 -3_0()! 0.986 23 0_0400 -0.0833 0.0311_ 1 440 -3.000 1.120 24 0.0500_-_0.0833 0.0342 1.800 -3.000_i 1.231 25 0.0600-0.0833 0.0368 2.1601-3.000; 1.326 26 .... (3.0--700 -0.0833 0.039i 2.520_--3.000. 1.407 27 _ 0.0_.800 --0.0833- 0.0410_ ....2.880_ -3.000 _ 1.478 28 0.0900-0.0833 0.0428 3.240 -3.000 1.540 29 0.100011-0.08331 0.0443-- 3.600 _ -3D.O()OT 1.595 30 0.1250 -0.0833 0.0475 4.500 -3.000 1.709 31 0.1500 -0.0833- 0.0499 5.400 -3.000 _ 1.798 32 0.1750 -0.0833 0.0519 6.300 -3.000 1.867 33 0.2000 -0.0833- 0.0534- 7.200- -3.0-00- 1.923 34 0.2500 -0.0833 0.0553 9.000 -3.000 1.992 35 0.3000 -0.0833 0.0558 10.800 -3.000 2.007 36 0.4000 -0.0833 0.0552 14.400 -3.000 1.988 37 0.5000 -0.0833 0.0523 18.000 -3.000 1.883 38 0.6000 -0.0833 0.0466 21.600 -3.000 1.678 39 0.7000- -0.0833 0.0384 25.200 -3.000 1.381 40 0.8000 -0.0833 0.0287 28.800 -3.000 1.033 ....... t 41 0.9000-0.0833 0.0188 32.400 -3.000 0.678, ,_,2 - 0.9300" -0.0833_ 0.0160" 33.480 -3.000 0.575' 43 0.9700-0.0833- 0.0123 34.920 -3D00-- 0.443 44 " 1.0000--0.0833 0.0087-- 36.000 -3.000- 0.311 _ Thermoc0uple Locatigns _ _ _ X/C Y/C Z/C X. (in.) Y,(in:) _Z,(in.)

1 0.1000 0.0833 -0.0284 3.600 3.000 -1.022 2 0.0500 0.0833 -0.0241 1.800 3.000 -0.868 3 0.1000 0.0833 -0.0307 3.600 3.000 -1.104 4 0.0500 0.0833 -0.0218 1.800 3.000 -0.786 5 0.0000 0.0833 0.0000 0.000 3.000 0_000 6 0.0000 -0.2500 0.0000 0.000 -9.000 0.000 NASA/TP--2000-210031 33 B3.--GENERAL AVIATION PRESSURE TAP LOCATIONS [Y measured from tunnel centerline] No. I X/C ! Y/C Z/C i X, (.in.) i Y, (in.) i Z_i_n.)_ i 1" 0.59703-0.08333 i -0.05-865_-2"1.493_ -3.000, -2.1121 -:2-- _9_4i_ -.0_.1_ 38_89j -0.03255 3.418 -5.000 -1,1721 3 : 0.00475 -0.16111-0.00949_ 0.171_-5,800_0.342 4 I 0.00000 -0.16667 i 0_0OO()0/ O_05_--6_0001 O_000 --5-t 0.00_ -0.17222 i 0.01601"- 0_235_ -6.2.2-00 -5.000i 1.786 6 0.088161 -0.13889 0.04962: 3.174 7 0.59967_ 0,07346_ 21 ._ General Aviat on Thermocouple Locations| ................ + X/C ! Y/C : Z/C _-X,_in.) _ Y, _in_ _ Z, (in.l

1 5._oo_ 5__6-0oo _ o.ooooo/-oooo7q8.o6o! 5 6o6 _

2 0.599671 0.50000 ! 0.07346 21.588 18.000 2.645 34 NASA/TP 2000-210031 B4.--GENERAL AVIATION (LTPT) PRESSURE TAP LOCATIONS [Baseline leading edge and main body] No. i x/c y/c z/c I x, in. i y, in. _ z, in.

t 09700 013074 -002630 34.92014.707 i -0.947

2 i 0.950001--0_12575--616_034.200: 4.527 -0.929 3 : 0.900000.11328-0.02570 q_ 32.400 4.078-0.925- - 4 0.85000__0.10082 -6:()28_ 130.600 3.629_-1.015_ 5 ' 0.82500__0..09459 -0.0305329.700 3.405 -1.099 6 " 0.80000 0.08835 -0.03320 28.800 3.181:-1.195 7 0.78750 0.08524 -0.03500 28.350 3.068! -1.260 " 6.77500T 0.08212 -0.0367027.900 2.956-1.321 9 " 0.76250! 0.07900 -0.03890 27.450 2.844 -1.400 2.732 -1.480 10 0.75000 0.07589-0.0411027.000 2.620 -1.573 11 _ 0_73750_--01(J7277 _ -0.0437026.550_ 2.507 -1.676- 120.725000.06965-0.04640:26.100 2.395 -1.750 1_ 0.7__!290 ___0;06654 -0.04860 25.65d -1.832 14 0.70000 0.06342 -0.05090 25.200 2.283 -1.940 15- 0.67500" 0.0-5719-0.0539024.300 2.059 -2.016 16 i 016-50000.05971 -0.0560023.400 2.150 -2.070: 17_O_6_0---0106594 -0.0575022.500 2.374 -2.110 180.60000 0.07218 -0.0588021.600 2.598 19 ! 0.55000 0.08464 -0.05980 19.800 3.047 -2.153 3.496 -2.160!

20 0.50000 0.09711 -0.06000 18.000 -2.142 21 0.45000 0.10958 -0.05950i 16.200 3.945 22 0.40000 0.12204 -0.05820 14.400 4.394 23 0.35000 0.13451, -0.05610 12.6001 4.842 _-2.020 i -1.9191 24 0.30000 0.13035 -0.05330 10.800 4.693

--l:f86*

25 " 0.25000 0.117891 -0.04970 9.000 4.244 I 26 0.20000 0.10542' -0.04540' 7.200i 3.795 -1.6341 Baseline -1.4401 Leading_ 27 0.15000 0.09296 -0.04000, 5.4001 3.346 28 0.12500 0.08672 -0.03670 4.5001 3.122 -1.3211Ed e9£__ -1.2021 29_ 0:10_000i 0.08049 -0.033401 3.600] 2.898 30 _ 0.0_80000.0_7550 -0.03080 _ 2:8 _ 2.718 -1.1091 31 ! 0.0700010.07301 -0.02890 2.520 2.628-1.040!

32!0.06000 0.07052 -0.02650 2.160_ 2.539---0.954 T _[ 0.55600! 0_06802_-0_024401 1.8001 2.449 -0.878 - 3410.04000 0.06553-0.02210 1.440J 2.359 -0.796 35 i 0.03000 0.06304_-0.01960! 1.080 2.269 -0.706 36- 0.02500! 0.06179 -0.01810_0.900N__ 2.224 -b_ ....

37_ 0.02000 0.0605 -0.01650 0.7201 2.180 -0.594 38_O.61506 O]O5Cj30 _ -0.01470 0.5401 2.135 -0.529 39 0_0-10-00 _ 0.05805 -0.01260 b_360__ 2.090 -0.454 40 0.00500 0.05680-0.00990 0_-80_ 2.045--0.3156- 41 0.00220 0.05618-0.00590 0.079 + 2.022-0.212 0_0472.001-0.068 42 0.00010 0.05558 -0.00190 43 - 0_0510--0_05558 0.00220 0.004: 2.001! 0.0791 44 -- 0.00_2120 0.05618 0.00830

0.079 2.o22 _

45 0.00500 0.05680 0.01440 0.180 2.045 0.5181

0.360 2.001 0.702i 46 _ 0.0-10()0_ 0.05558 0.01950 f 47 " 0.0_0_--0_05930 0.02310 0.540 2.135 0.832 i 48 0.02000 0.06054 0.02610 0.720 2.180: 0.940_ 0.900 2.224_ 1.0331 49 0.02500i 0.06179 0.02870 -50_ 0.03000 0.06304 0.03100_ 1.080 2.269:1.116 i .__ 51 0.04000 0.0655310.03510J_440 2.359 1.264_ 52_ 0.05000 0.06802! 0.03870|1.800 2.449 1.393 53 i 0.06000 _ 0.07052 0.04200 2.160 2.539 1.512 54 i 0.07000 --0.07301 0.045001 2.520 --2.628 1.620 55 [ 0.08000 0.07550 0.04800, 2.880 2.718 1.728 End 56 i 0.10000 0.08049 0.05240 3.600 2.898 1.886BaSeline 57 0.12500 0.08672 0.05720' 4.500 3.1221 2.0591Leadin& 58 0.15000 0.09296 0.06190 5.400 3.346] 2.228!Edge NASA/TP--2000-210031 35 B4.--Continued.

[Baseline leading edge and main body] I 59 I 0.17500 0.09794_ 0.0656_ 6:300! 3.526_ _2.362' 60 0.20000 0.1041_ 0.06930 7.200, 3.750i--2.495 61 0.22500 0.11165 0.__..1-0-0 i 4.020"--_-2..596 _ - 0_07490- 91(_00" 4.244 2.696

62-t 0.25000 F 011789r

0.27500! 0.12412i 63 0.07690 9.900 4.468! 2.768i , 4.693! 2.840!

0.30000' 0.13035' 0.07890 10.800 0.32500 0.13659i 0.08020! 111700t 4.917 2.887 0.13451 E66v .

0.35000 0.08140j 12.600 4.842, 2.930i 0.12828!

167 o.375oo 0.08200_ 13500,- 4_8__2.9_J

68 0.40000 0.12204 6-i08260_- 1-_,_-400 i 4_394 2.9741 69_ 0.42500 0.115811 0.08255 15.300 / _69i zeFE 70 0-.4_0 0.10958 i 0.08250_ l&:)-O0 3.945 2.970 71 0.47500 _ 0.10334 0.08f8_1-60-3_720-! 2.945i 72 0.50000J 0.09711 6108100_1&.00-0! ......3-,¢§6 _- 2.916 73 ' 0.5250_ 0.09081 0.07960 i 18.900 3.272i 2.866_ 74 _00 _ 0.08464 0.07810 19.80-01 3.047_ 2181;2! -- 75 0.57500 0.07841" 0.07580 20.700 i 2.._ _2_72{) ?

76 i 0.60000 0.07211 0.07350 21.600_ 2_598_2__.6_ -- 77 ! 0.62500 0.06594 0.07040 22.500 2.374 2.534 78 0.65000 0.05971 o.o668ol 23.400___ _.2 1501 2.4051 790.67500 0.05719 0.062601 _24.300 i 2.059 2.254!

0.05730: 25.200[ 2.283 8o i o.7oooo 0.063421 2.063 ..... 0.06654 o.o54ooi 25.650 2.395i 1.944i 81 ' 0.71250 0.0696? 0_050_8__0 26.100-]_ _2.507]_1T829! -- 82 i 0.72500_ 83 i 0.73750 0.07277 0.04670 _0-|- 2.620_-1_68;I _ - -- 84 ! 0.75000 0.07589 0.04260 i 27.000|-2_.7-3'2- _4_ ....

85 _ 0.76250 0.07900 0.03800 27.450' 2.844! 1.368i 86 0.77500 0,08212 0.03350 27.900 2.956! 1.206_ 87 0.78750_ 0.08524i 0.02890, 28.350i 3.068 _ 1.0401 88 0.80000 i 0.0883_ 0.024401 28.8001 3.1811 0.878, 8_- 6._550 / _ 0.o158oi 29.700 3.405 i 0.569 90 , 0.85000! 0.1008_ 0.00730] 30600j 3.629 0.263 91 I 0.90000j 0.11328 4.078-0.256_ -0.00710! 32.400 92 _ 0.12575 -0.01850 i -0.666 34 200, 4.527 0.95000_ _ 0.13074 -0.022401 34.920 4.707 -0.8061 94 0.70000! 0.25000i 2.063_ .....

0.05730 25.200 9.000 95 i 0.70000 0.33333 0_5730! 27._n_nO 12.000 2.063 96 i 0.70000! 0.38889 O.05_00____0 2.063i 15.000 2.0631 0.41667 0.0573_ 25.200 98 0.70000 i 0.430561 15.5001 2.0631 0.05_0_ 2_.20E 16.000: 2.063'

0.057325.2

_0 i 0.70000 0.44444 , 0.45833 16.500 2.063 o.700001 0.05730' 25.200I 17.0001 2.063 _00 ! 0.47222 0.05730] 25.200 102 0.70000 i 0.48611 17_051 2_0631 0.05730 i 25.200¢ 103 i 0.70000 -0.05556_ -2.000_ 2.063 0.057301 25_200_ 104_ 0.700001 -0.16667 -6.000 2.063 0.05730 _L 0.05730_ 25.2001 -9.000 2.063j ......

105 0.700001 -0.25000 106 0.70000! -0.33333 107 0.70000'-0.38889 0.0573_2_ -12.000-2.063! ---- t _05730_&.200_ -1_ 2.063! --- 0 70000 -0.41667i 0.05730; 25.2501-_15.000 2_b6-3_-

#

-0.430561 _-i 0.70000 0.057301 25.200_-1-5_00_2.063_

-_0' 0.70000 -0.44444! o.o573o I 25.20_116-_00_2.0_

111_ o.7oooo-o.45833

0.057301 25.200_-116_0_2:063L .... _ 0.057301 25.200|-17000 2063 1_ 0.700001 -0.4722_ 113 : 0.70000 -0.4861_ 0._5730 i 25.20_ -17.500, 2.063 i 114 i 1.00000 0.2500_ -0.027511 36.00_ ...... §._0 -0.990] 115 0.33333 1.00000 -0.02751_Q00 12.00_--00:99-0 116 1.000001 0.416671-0_2751_3&-.000_;000!-0.990 i 36 NAS A/TP--2000- 210031 B4.--Continued.

[Baseline leading edge and main body] 117 1.00000 0.47222 -0.02751 36.000_ 17_.000 -0.990 `118 7 1.00000 -0.05556 -0.02751 36.000! -2.000 -0.990 119 I 1.00000 -0.16667, -0.0_2751 36.000 t -6.000 -0.990 ];_()-_ 1.00000 -0.25000 -0.02751 36.000i -9.000 -0.990_- - 121 1.00000 -0.33333-0.02751 36.000_-12.000 -0.990 ----- b 122 ; 1.00000 -0.41667 -0.02751 36.0001-15.000-0.990!

123 1.00000 -0_4722:_ -0.02751, 36.000!-17.000 -0.990 B4.--Continued.

[Leading edge for ice shape 621] No. x/c y/c _ z/c x, in. _, in. z, in.

26 0.18721:0.0-83-331 -0.04417 6_7401 3.000T :1.590 27 70.;15944 0.083_0-z_`111 .... 5.740T - 3_0001 -11480 28 ! _1_3167_ 01-08:]33'-0.03778 4_740_ :31_0_ "1.360 2g _ 0.10390- 0.08333! -0.03444 3.740_ 3.0001 -1.240 3(3 _ 0076101 0.08333-0.03028 2.7401 3.000 t -1.090 31 _0_05528_ 0.08333 -0.02611 1.990_ 31000 :0194_0 • - -4 32 _ 0.04139 0.08333 -0.02278 1.490 3.000 -0.820 33 : 0.02839T 0.08333"-0.02000 1.022" 3.000!-0.720 34_0.01536_ 0.08333_0_;1611 _ - 0.553 3.0001 -0.580 35 0.00494! 0.08333 -0.01139 0.178 3.000 -0.410 36 _-0_00i19_0.083:]3- 0.00()28! -01(343" 31000_ 0.01(3 3_.(30072! 0.08:333- b.51_-_i(3:26__ 3_000_0_(3 38 _ 0.00550 _ 0.08333 0:018333 0.198 3.000. 0.660 39 _0.01417i 0.08333 0.02389 0.510 3.000 0.860 40 i 0.02458! 0.08333 0.02917--0_885- 3.000 1.050 41_ _ (].03500_ 0.08333 __0.03361- -1.260_ --3.000_1:210 42 0.04889 0.08333 0.03833 1.760 3.000 1.380 - -43_ 0.06278- 0.08333 _ ()_6_4_ 2.260 3.000 1.540 44 0.08014- 0.08333 0.04778 2.885 3.000 1.720 45 0.10097 0.08333 0.05278 3.635 3.000 `11900 46 0.12180 0.08333 0.05694 4.385 3.000 2.050 --47 -- 0.;14264-- D.O8:]:]_6b_5_1:35_ :3.00(3 2_]90 NASA/TP--2000- 210031 37 B4.--Continued.

[Leading edge for ice shape 622] No. _ . x/c .__y/c _ __Z/C ' x, in. _y, in. _,z, in.

260.18721 0.08333 i 6.740 ,q_-3._0-1.5-90 _7-_ -0.04417 i i_ 0.15944 0.08333!-0.041111 5.740 3.000i-1.480 28 i 0.13167! 0.08333 -0.03778 4.7777_-- 3.000t-1.360 29 0.10390i 0.08333-0.03722 i 3.740 3.000-1.340

30 i 0.07610 _.08333-_31_9! Z(4_ i _._oo_-_._i_

31 ] 0.05528 0.08333 -0.02667 1 9_ 3000 -0960 .... L . ..... ! __ t.....

32 0.03444 0.08333 -0.02306 _1.2.40 Z 3.000:-0.830 ,_ 0.01708J 0.08333-0.01917! 0.615 i 3.000 i -0.690 3 0.00180! 0.08333 -0.01333 ....... 0:06_5__ 3.0()0_--0.48__ _ 35 -0.00464 0.08333 i 0.00028 -0.167 3.000! 0.01_ 36 i -0.002301 0.08333i 0.01000-0.083i 3.000 0.360 3"7 0.002361 0.083331 0i0i944" O_O85_ 3.00-0__ 38 0.01417 0.08333 0.02500 0.510 3.000 _ 0.900 39 0.02200 0.08333! 0.02917 0.792: 3.000 1.050 40 ' 0.02980! 0.08333' 0.03278 1.073[ 3.000i__I ;I.18_0 -_41 ! 0.0384_ 0.08333 0.03611 1.385! 3.000! 1.300 _.42 0.04889 i 0.08333! 0.038331 1.760 3.000 1.3801 i --- ' I -_ -- - 43 i 0.059301 0.08333 0.04167j 2.135_. 3.000 1._ 44!0.08014 ! _0_0_i3333 0_04'750 ,' 2.885_31000_i:T1_] 45 0.100971 _1-01052501 31635 31(3C)01 _46_ 0A-21_ O..08333! 0_ _4_3-8-5- 3_000 i 2.050 I 47 i 0.14125i 0.08333 0.06056 5.085i 3.0001 2.1801 B4.--Concluded.

[Leading edge for ice shape 623]

y, in. i z, in. I

No. i x/c _ _ z/c x, in.

--2.66_-3.6o_ 1

2610.17680 0.0833-01-0_04444--6.365 27 0.14900 0.08330! -0.04139 5.364 0.08330-0.03472 3.614 28 W 0.10040!

2.99_ -_

_L o:o_

0.083301 -0.0305_ 2_491_

30 ! 0_6201

l

o -o

0.08330 ! -0.0-3056. -0._ 0

31 -0.000_ 2.9991 -1.1oo 1

0.08330 -0.028611 -0.198 32 _ -0_._550_ 2._030J 33 -0.01160!

o.%_;:_6 i -_o2_o-0r '6;418

.... 21999 -0.9OC)] 34 -0.01880

_99_: o.o_ I

0.08-330 _ 0.02889 -0.6ff

35-0.01880i

-2.99C-_

.... 2.996!--1.1001

0.0_330i 0.030_ c0.4_ 36 ] -0.01360 i

37 _ -0.00840!

0.083-301 0._ -0:302 2.9991 --1_100'

0.08330! _02861 _6 38 0.02460: 2.999 1.030 - i A9--i 0.04110 0_08330 0.03556 !- 1.48(] 2.999. 1.280 40 0_()6020_ 0.0_8330i 0_()419__ - :2.1-67 2.999i 1.510 41 0.08010, 0108330! 0.04_ 2.884 21999 1.710

_ 0.10100 0.08330 0.05250 3.63( 2.999 1.890

--43' 0.12530 0.083301 0.05750 i 4.511--2.999_-2.070 44 0.13920 0.08330[ 0.06000 i 5._1 r---2__999_ 2_60" 38 NAS A/TP---2000-210031

Appendix C

Test Matrices

NAS A/TP--2000-210031 39

C1 .--COMPLETED BUSINESS JET (1st ENTRY) TEST MATRIX Run Mach Airspd Attitude Tt Tt Ts i Ts MVD LWC . LWC Par Pwat / Spray ; Notes " i I 7- _ _ -- _ ....... .3, _ .... -3 -_ _ _ f "_ - No. No, kts) deslredl F , C _ F , C : um (g/m) i (g/m) si sd _ rnn ' ; i : ' I desired act 072595.01 0.28 175 6.0' 30.6 -0.8 23.0 -5.0! 20_.54() + 0,540 -_- 17.0----371_- 610i 072595.02 0.28 F -_ --, --_ ..... _ _ ---._ _ ........

0725,9510-31 0.28! 175: 60 30:61 -0,8 23:0 _ -,5.0 20 0_4_2,540_ - 17.0i 37.9! 6.01repeat of 072595.01

, , 175i 6.0 i 306 -0.8L_23_.0-5.0 20_ 0.54_0.540 17.0]-37.9 22.5! ..... -

072595.04 i 0.28' 175_ 6.0__ 30.6! -0.8_ 23.0 -5.0, 20 0.540 0540 : 170 379 450

072695.011 0.28 1751 6.0! 28.9 -1.7 21.4i -5.91 201 0,300 0.405-[ 10.3 18.6i 4.4

072695.02 028 L 175 80 289 L -18, 212 -60, 20 0.300 0:3: -i8 ; 7i

072695.03 i 0.28! 175 6.0_ 28.9! -1.7i 21.4' -5.9, 201 0.300 0.405 10.3 18.6 ! 33.3 , , t _ .... , ............

072695.04! 0.28 175 6.0 21.4, -5.9 14.0_0_ 201 0.430 0.430_ 11.6 21.6 6.0 07 6 5.05 0.28 175 6.0, 0:430ii.E ....

072795.01 0.281 175i 6o1_ 2141.I _&91 14.01-10.0 2-0-_-&430 0430 116i .... 2i_ 2;_5_

6.0_ 21.41 -5.91 14.0!-10.0 15_ 0.600 0.600__60.0] 66.7 6.0! 072795.02i 0.28 175!

I :072795.03! 0.28 175 I 6.0 21.4 -5.9 14.0:-10.0 i 15 I 0.600 0.600+60.0 66.7 22.5 -- 15 O-60_ 0-.60(),-- 60.0" -66,7 i 45.0_ .......... 072795,04_ 0.28 175 6.0 21.4 -6.0 14,0 ]-10.01 20 0.300 _- (Z-_3i 1816! 44i 072795.05! 0._ 175 6.0 12.31 -t10 5,0 -1_ 072795.060.281 175 t _6._ 123! -11,0i 50 -15.0 20 , 0.3000,405 10,31 18.6 33.3:mold

07_2895.02 i 0.39i 2501 1.529.7 -1,3 ! 15.3 -9.3 t 15 0.600 0.500 i 71.2 82.7 3.9

07289503 0.39 250 1.5 29.7 -1.3 151 15 0.600 4 0.500 i 71.2 82._ 7,2

.... 8.2 .......... 072895.04 0.39 i 250 1.5

072895.05 0.391 250 _.5 _ 28,0 -Z-2! 1&7 -10.2 ! 20_ 0.430 1 0.430 18.2_ 41.8i 3,01 . 13.7 -10.2 20 I 0,430 0.430 1 4i[8 _ 61()" 072895_()6 0.39 250- 1_5"_2-8_0_ _2.2] i3:_ :'10:_ 20! 0.540 0.540 29.1 75.1_ 3._+-- 072895.07 0.39 / 250 1.5 28 0 -2 2, 13 7 -10.2 20 0 540 0 540 29 1 75 1 6 0 072895.08 0.391-175 6.0 12:3_-11.0_ 5.01-1_.0 20--0:_I0 01540 ! 17.'0_ 3719 _ --45.%_mold ......

073195.01 0_-39-! 250 _ 1_9! -73F---_---20_0.300-_ 0.310 - i0.3: 18.5' Z9_ .......

073195.02t r 0.3_ T 250 1,5_ 18.9 i -7.31 4.7-15.1-- 20_.3()0- 0,31010,3- 18-15"- 5'8_ .....

073195.03i (3-128 175 _- 6.0- 12.3- -_-E_15_0 _ 20"-(}_300_ 0.405 I 10 3 1_}-6-- 161_ ........

-0T3%5.0_ _ 0_8 "?T_' ...._.0_ _2.3 -ST.o_ _ -15.01 20--0540t0.540_5_ 3-/# 60|

080195.01_ 0.39 250 +1 1.5_ 9.5: -1Z5! -4.3- -2-0_2 40 T--()]1-()0_0.410 i 1016 32.6 i 0.7' -.....

080195.02! 0.39 250 1.5 9.5!-12.5 -4.3_-20.2 i 40 0.100 i0.4101 10.6 32.6__ 1.5: 080195_030.28_ 175 60 678_-t4.0:0_4_-18.0 20 0.540 _,0.5351-i-7_ _19_ 6.0! ........

080195.04i, o.28 I 175 4,oi 6.8i -14.0i -0,4 -18.0__ 20 0.540 0,535 17.0_ - 3719 60!r_(38-0_ 080195.051 0.28 175 4.0 68 -14,0! -0.4 -18.0 40 0.540 0,535 , 10.6 32.6 6.0

o8o195.o6 o.34 212 4.o 6,8 -14.0 -3.7+-19.9 4o %1_4_--0.535-_ 10.6 32.6_ _.oi

080195.07 0.34 212 4.0 6.81 -14.0, -3.71 -1_ 20 0.5'_0 0.540 !-_17.0, 37.9i ..... 61_ ...........

6:q4- 61 -0.4i -18.0 40 0.540 0.540 10.6i 32.6 6.0

080195.08 0.28 I 175 I 6.0i 6.87 -14.04 -0.4 -18.0 40 0.100 0.535 10.6 32.6 4.2

080195.09 0.28 1751 ...... _---- ....

080295.01 I 0.28 1751 6.0' 30.6 -0.8 23.0 -5.0 20 0340 0.540 17.0 37.9, 120 -5.0 20 0.540 i 0.540_ 37 91- 22 5 080295.02 ' 0.28 175 : 4.0 30.6! -0.8 23.0 i ......................... " ....

I ......... _---_ I :i - 080295,04 0.28 175 4.0i 3-(316_ --(3181 23.0_ -5.0 20 0.540 _0.540 17.0_ 37.9 22.5

o8o295.o5 i 0.34 212 4-(3_-3.9!-i410 -10.0 20= 0.430 0.430 11.6 i 21.6' 22.5

080295.06' 0.28 175 - 4.0 30.6_ -0.8 23.0i -5.0 i 20 _ 0.540 0.540 17.0 37.9 22.5imold ....

-_ 2.500 0.750 28.9 t - , .......

__ - i5 9,9_ lO.OJ 080395.01 0.39 250 1.5, ---8 71 20_ 080395.02 0.39 250 1.51 30.8 -0:7.___16.4_ 2.250 1.250 68.0__ 57.5_. --54_.: - 080395.03 0.28 175 6.0_ 28.4i -2_01-20.9' _ 15i 2.500 1.000 28.319,8 15.01 080-39-5_04J 0.28 175 6.0l 24.2 -4.4 16.7 -8.5 20/ 2.250 1.600 70.8 61.3" 8.4"-- .......

, , 1 080395.05 0.39 250 1.5 18.8 i -7.4 4.7i-15.2i 15 i 2500 0750 I 289 99i 100 080395.06 0.39 L 250 1.5 18.8, -7.4 4.7i -15.2i 20 2.250 _ 1.250 i 68.0 57.5, 5.4 6.0_ 12.3j _.04 -15.0+ 20 2.255 -i7600 _ _7_--8.4_;__ 080395.07 0.28 i 080495.0_ 0.28_ 175 6.0 -18.0 -27.8i -24.9' -31.6 160 0.830 0.830 5.0 50.0!

080495.02 0.28

175 _-_;0 -1810i _ :2_9--_6-.6 _ 0.830 0.830 _ 50_ 6.0

175 .....-6.0' 12.21 -1_ ...... _-___ 160 _` 0.830 ' 0.830 j 5.0- _ 20_---

080495.03 0.28 i I 4 _ "-_ _ ' i 080495.04! 0.28' 175_ .0_ 12.2j -11.0__ 4.9,-15.0 160 0.830 L 0.830 5.0_--5010 20.0 0804_i05 ! 0.28 175_--6_ 30_6 -0-_i _ _51d 16{3- i 0.8300.830 5.01 5()__ 080495.06 0.28;

175: -6.0_%0.6 i -0.8 _ 23T0- -_-.o _ 2o 1 0.540 0.540 _ 37_ 22.5[mo_

40 NASA/TP--2000-210031

C2.--COMPLETED BUSINESS JET (2nd ENTRY) TEST MATRIX Run Mach Airspd Attitude Tt i Tt Ts ; Ts MVD LWC LWC Pair Pwat i Spray . Notes No. _ No. - _ desired (F)_+_) {F) i-(_n?_**(glm!_i (g/m3)_ !PsLq[± (psid) i (min) .

l _ desired act

201 028 175 60 300 -08 224 -50 2o 0300, 040_iq3! 1961 441

202 . 0.28+ 175 60 30.0! -0,8 22.4 -5.0 20 0.540; 0.540 17.0 37.91 2.0.

202r- _0,28 175 !_ 60, 3_.0.0 _ -0,8 22.4_ -5.0 20__ 0.540 i 0.540: 17.0 37.91 2.0repeat 202m_ 0.28 175 ! 6,O_ 30.0_ -0.8 22.4 -50 20 0.540, 0.540 17.0j 37.9_ 2.0mold 203 0.28 175 6,0 30.0' -0,8 22.4: -5.0 20 0.5401 0.540 17.0 37.91 6.0 204 0.28. 175. 6,0 30.0 -0,8 22.4 -5,0 20 0.540i 0.540 17.0 37.9_ 22.5 205q 0.28/ 175. 6.0 20.8 -5.9 13.4-10.0 40 0.100_ 0.535__ 10.6+ 3_2.6: 1.1.

205r 0.28i 175 60 208 -59 134 -100 40 01001 0.535 10.6 32.6 1.!repeat 206_028 i 175 6:0 220.8:_-5.9 13.4 -10.0 40 0.100 0.535 10.#_ 326 4.2 207 L 0.28 ! 175 , 6.0 20.8 -5.9 13.4. _-10.0 _ 0.4301 0.430 11.6! 21.6: 2.0 208 0.28 175 6.0 20.8 -5.9 13.4 -10.0 20 0.430! 0.430 11.61 21.6; 6.0 209-0.28! 175 _ 610 _ 20.8 -5.9_ 13.4-10.0 20 0.430 0.430 11.6 21.6 22.5

2i0_ 028_ i_(T 6.0_ _.7 -116 10.3! 18.6_ 20

" - " 4.4 _ 20 _ 0.4_ t " 21 ! + 0,28 175 ! 6,0__. 11:7 -11,0- _ 4,4-15.01 20 0,300! 0.405 10.3: 18.6 4.4 212 L 0.28 175 6,04 11.7 -11.0 4.4 -15.0! 20 0.300 0.405; 10.31 18.6 16.7

_i3 0.28- 17_i 610i 20;8 -5,9i 13.4 _ _ 0.600 0.6001 600 665_ 2.0-

:fi_ 0._75_ _-2516--.516-i3_4_-10.01-_ 0.600; 0.6oo 600_ 6_5- 60-

221 0.39' 250 1.5_ 30.0 -0.8_ 22.4 -5.0i 20 0.540 0.540 29.1 75.1 30 222---(_39/ 250 .... 1_5 30,0 -0.8! 224 -5,0! 20_ 0.540 0.540__ 29.11 75.1_ 601 223 0.39! 250; 1.5! 30.0 -0.8_ 22.4: 20 0.300 0.310 10.3 18.5 2.9 i 224 i 0.39_ 250 1.51 30.0 -0.8! 22,4,-5.0L _ 0.300 0.310_ 10.31 18.5." 5.81 225 t 0.39 __ 250 ; 1,5__ 20.8 -5.91 . 13.4_ -10.01 15 0.600 0.500 71.2 82.7 3.6 2261 0.39 250 1.5i 20.8 -5.9: 134 -10.01 15 0.600 0.500; 71.2 82.7 7.2 231_ 0.28. 175, 4.0i 30.0 -0.8 22.41 _-6.0 20 0.540 0.540 17.0 37.9 2.0+ 232_ 0.28 175 . 4.0i 30.0 -0.8i 22.4 -5.0 L 20 0.540_ 0.540 17.0 37.9. 6.0 233! 0.28 175 4.0 20.8 -5.9 13.4-10.0 15 0.600 0.600 60.0 66.7 20 234_ 0.28 1 " 175 4.0_. 20.8 -5._9 134_-1_0 0 150,600 0.600 60.0.. 66.7 L 6.0_ 235 _ 0.28 175 4.0i_20.8 _ -5.9__ 13.4_-10.0 40 0.100 0.535 10.6 32.6 !.1.

236 0.28; 175 4.0 20.81 -5.9 13.4i -10.0 40 0.100 0.535 10.6 32.6 4.2 237 0.28 175 4.0 11.71 -11.0 4:.4- -15.0 20 0.300 0.405_ 10.3 18.6+ 1.5 238 0.28 T 1"75- 4.0 11.7' -11.0 4.4 -15.0 20 0.300 0.405 10.3 18.6 4.4 NASA/TP--2000-210031 41 C3.--PLANNED COMMERCIAL TRANSPORT TEST MATRIX Run Mach Airspd Attitude Tt Tt Ts Ts MVD LWC Spray No. No. (kts) (F) (C) (F) (C) (um) (g/m s) (min I 101 0.45 284 0.0 32.0 0.0 12.8 -10.6 20 0,410 6,0 102 0.45 284 0.0 32.0 0.0 12.8 -10,6 20 0.410 6.0 103 0.45 284 0.0 32.0 0.0 12.8 -10.6 20 0.410 22.5 104 0.45 279 -1.0 14.0 -10.0 -4.4 -20.2 15 0.295 6.0 105 0.45 279 -1.0 14.0 -10.0 -4.4 -20.2 15 0,295 22.5 106 0.45 279 0.0 14.0 -10.0 -4.4 -20,2 15 0,295 6.0 107 0.45 279 0,0 14,0 -10,0 -4.4 -20.2 15 0.295 22.5 108 0,45 279 0.0 14.0 -10.0 -4.4 -20.2 15 0,295 30,6 110 0.45 282 -1.0 23.0 -5.0 4.2 -15.4 20 0,285 6,0 111 0.45 282 -1.0 23.0 -5.0 4.2 -15.4 20 0,285 22.5 112 0.45 282 0.0 23.0 -5.0 4.2 -15.4 20 0,285 6,0 113 0.45 282 0.0 23.0 -5.0 4.2 -15.4 20 0.285 45.0 114 0.45 282 0.0 23.0 -5.0 4.2 -15.4 20 0.285 30.0 115 0,45 282 0.0 23.0 -5.0 4,2 -154 20 0.285 22.5 116 0.45 284 0.0 32.0 0.0 12.8 -10.6 20 0410 6.0 122 0.45 284 -1.0 32,0 0.0 12.8 -10,6 20 0,410 6.0 123 0.45 284 -1.0 32.0 0.0 12.8 -10.6 20 0.410 22.5 124 0.45 284 0.0 32.0 0,0 12.8 -10.6 20 0.410 6.0 126 0.45 284 0.0 32.0 0.0 12.8 -10.6 20 0,410 30,0 127 0.45 284 0.0 32.0 0.0 12.8 -10.6 20 0.410 22.5 128 0.45 282 0.0 23.0 -5.0 4,2 -15.4 20 0.285 2.0 129 0.45 284 0.0 32.0 0.0 12.8 -10,6 20 0.410 2.0 130 0.40 253 0.0 32.0 0.0 16.7 -84 56 0.420 22.5 131 0.40 253 0.0 33.0 0.6 17.7 -7.9 56 0.420 22.5 132 0.40 253 0.0 35.0 1.7 19.7 -6.8 56 0.420 6.0 133 0.40 253 0.0 34.0 1.1 18.7 -7.4 56 0,420 22.5 141 0.45 284 0.0 18.0 -7.7 -0.6 -18.1 40 0,100 7,5 142 0.45 284 0.0 18.0 -7.7 -06 -18.t 40 0.100 2.0 143 0.45 284 0.0 32.0 0.0 12,8 -10.6 40 0,512 6.0 144 0.45 284 0.0 32.0 0.0 12.8 -10,6 40 0,200 6,0 145 0.45 284 0.0 32.0 0.0 12.8 -10.6 40 0.200 22.5

42 NAS A/TP--2000-210031

C4.--COMPLETED COMMERCIAL TRANSPORT TEST MATRIX Run i Mach Airspd Attitude Tt Tt Ts Ts i MVD LWC LWC ! Pair Pwat S_ray i Notes NO" I No. , (k_S) : desired_) C(_(F) (C_ i u_ (g/m-) (g/m)_(psg) _sid____m!n ) ' i _- " C ----- i- ._7 ____,clesired act 101 _ 0.45i 284; 0.0 32.0 00 13.0 -10.0 20 0.410' _ 20.0 47.0 6.0 not scaled 102- 0.40_250 t 010- 320 t 0.0 _ 13.5"- _ 20 Q-4_ 0.460 20_0 4710 6.0_not scaled 103-Q_250_ 0-0_ 3210- 00_ 1-3-5"-100 + 201 ().4]-01 0.460 i 20.0 47.0 22.5ino_scaled

104 0.401_48_ -1.0 10.5 -1201 4o -20.01 15 I o.295 0.339- 17.:3__25.3_ 59

105- 0.40, 2_,-8_ _110!_0;5 --120_.0_-2_5 0.295! 0_3391 17.3 25.3 22.0

106 ...... ()AO_ 248 T 0101 __---2_5 i o295] 0.339 _ 17a_5----59 _ - -

106r1- -0._6_,48 i 00!-10:5_---1_-200 15! 0.29-5i 0.33_-- 25_3----_._ _i - _07" _--248_ -&O _015_-12.0"--_4_0_-20_ 15W01295 0.339_7.3_25.3--22.0" 108_ 040T 248_ "_00W105: -_ 12.0 --4.0_-20.0! 15!--0295 0.339i 17.3 .... 25.3--29.3' 110 0.40_ 250 -1 0 20.0i -6.3 5.1, -14.6 i 21 ! 0.285i 0.3414 11.8 23.2 5.7

11i-; 6.40'_25{) = :10T 20.OP -6,3_51! -146 211 0._5 0,341 _ i118 23_2 21.1: "

112 I 040 250 0.0 20.0! -6.3i 5.11 -14.6! 21 I 0.285 0.341 118 232 5.7 .....

_{4 1 B_.40_ 2-56_-206_--6_ t. -14.6 21 0.285; 0.341 _ i_8 23:2 28.3

115 0.40 250 0.0: 20.01 -6.31 5.1! -146 21 0.285! 0.341 11.8 23.2: 21.1 mold made i16 " 0.40T 255 _ -1.0-3816_ 4.0! 23.1_-4.6 ' 21 0.410 0.500 23.8 62.6 55 ice shed - no data 122 0.40i 253 _ -1.0 29_ -1.1 14.3 i -9.5 21 0.410 0.563 29.7 83.22 4.9 123 0.40i 253 -1.0 29.5 i -1.1 14.3_ -9.5 21 0.410 0.563 29.7 83.2 18.5 124_ OT40_ 253 0.0 29.51 -1.1 14.3' -9.5 21 0,410 0.563 29.7 83.2 i 4.9 _ _ 126 0.4_0_ 0.0 29.5 -1.1 14,3: -9.5 21 0,410 0.563 29.7 83,2 24,6

_27, 5 217.1 _-43! ;gT 21' 0.410 0563 29.7_ 83.2: 18.5mo_0 made

1_ 0.40 _ 250_ 010" 20,0 _- -613- 5i]*-14.6 21 0,285 0.341 11.8 23.2L 2.0 ........

.... + ..............

129 i 0.40 253 0.0 29.5 -1.1 14.3 -9,5 21 0.410 0.563 29.7_ 83.21 2.0 130 0.40i 253 0.0 32.0 0.3 16.7 -8.t 56 0.420 unk 8.2: 32.0 18.0 not scaled 131 0.40_ _ 253_ ._0.0 33.0 0.9 17.7 -7.6i 56 0.420. unk -, 8.2 32.0 18.0.no_t scaled___ : not scaled, ice shed - _ 132 0.402 .... 253 . 0.0 35.0 2.0 19.7 -6.5_ 56 0.420 unk 8.2 32.0 5.2 no data 56 0.420 unk 8.2 32.0 18.0 not scaled 133 0.40! 253 0.0 34.0 1.4 18.7 -7.1 i 141 ..... 0.402z$9--0_0 _ 15.0 .... £9.1-- 013- -1_ 42' 0.100 0400 10.1 30.3 67 i42_ 0.404 249 010 15_0 -9.1 0_3-17.3 i 42 0.100 0.400 i 10.1 30.3 2:Q

Q4_3 _ 0.40_ 253 0.0 29.0 -1.3, 13.8:-9.81 42 0.512 0.6501 21.8 101.8 5.3 ._

144 I 0.40 253 0.0 i 25.51 -3.31 10.4-11.6 42 0.200 0.400! 10.4 31.3 3.0 14_ 0.40 253 0.0_ 25.5_ -3.3! 10.4_-Jt_6 _ 42J__ 0.200 9.400- 19.4 31.3 _ .

i 145m 'Q40_253- 0.0:25.5 -3.3; 10.4:-11.61 42! 0.200 0.4001 10.4 31,3 11.2,molemade NAS A/TP--2000- 210031 43 C5.--GENERAL AVIATION AIRFOIL TEST MATRIX I6i02_ Run FMach ÷ Airspd Attitude 4 Tt i T_t Ts Ts .MVD LWC L_, Pair Pwat Spray_ Noles NO: i No. I (kts) i desire_ (F)____C) [ (F_C) _ _ (g/_) (g/m3i_(psip)! _idii (rnin) _ ! : I ! -desired- aci i _ --. ......

60_--0.29; 180 0,_-3Q0- -6.8. 224 _- -5.0_ 20" 0154-0i 0,540i 19.0- 41.0 _ 210_ 0_2.9L 18<L 0.0-30_0.8_2:4[-5.0 i _ 0_-0__19___ 411_ I 6._i_i i_I 2rn 0.29 | 180! 0.0! 30.0 -0.8 22.41_ -5.01 20 1 0.540 0.640_ 19.0 41.01 6.0_mold ....

-- I _ +- ........

60_ 0.29_ 180! 0.0 30.0 i -0.8 22.4_ -5.0 20 0.540 0.540! 19.0 41.0_ 22.5 i __ 0.29. 180 0.0 20.81 -5_.9i 13.4 _ -i0.0- 2_0 0:__.:30_ 0_430* 14._ 25.0_ 210 _ - 607 [ 0.29 i 180' 0.0 i 20.8] -5.91 _ 13.4 -10.0_-- 2__ -0:4-30: _14.5- 25.0_ " 16_0_ 607__m: 0.29 180 0.0 20.8: -5,9 13.4-10.0 201 0,430 _5 25.01 6.0imoid 608; 0.291 180! 0.0, 20.8J -591 134' -1()i01 __0- -0_4301 14-5V-25_.0 -2_ - 6091 0.29i' 180 0.0 11.7 -110 44i-15.0 ;0--osoo 0 -30 10:01-- 45 ....

610, 0.29 1801 0.0, 11.7-11.0, 4,4[-15.(3_ 0300 03301 10.0 14.5_ 8.0i

-611 0.29! 1801 _ _76_4- -150! 2o' 0_0330!-i0_ .....1-4_2_5T--

_ 612 i 0.29 [ 180-_ 0.0* 2_00:8___-5.9 13.4 -10.0_ -0.600 O_t-801()_----_-- 612r: 0.29 I 180 I O_ 20.8! -5.9; 13.4L-10.0 # 15! 0:600 -0_5_ 80.0 _-- -80_0 _ -- 210_rr_ -613i 0.29! 180 I 0.0 2_9_.z1/-_0: -15'01600- 0.560__6:_6.0 ....

621m 0.21 ! 130 2.0 i 26.4 -2.81 22.4'--5.0_--20-' 0:_0_ o..5_()L - 14_ _._.2.0"mo1_- --622_ 0-.21 _0-_0- 26.4! -2.8, ___-0.540_0:5_,0_ 14.0_-23.0' -60! -- 622rl 0.21 130__ 2.0,' 26.4 -- -2.81-- 22.4 -5 0 i 20 0.54()--5.5401_z[5/230--_eat _- 622r2_ 0.21 : 130: 2.01 26._ -2.8 L 22 4 -5._ 20; 0 540i 0.540 14.01 23.0_ 6.0 repeat 622m 0.2"t[ 130 I 2.0! 26.4! 3:8! 22._-5.0_._i--20 0_40_0_,_i_23.0! .... 6})irnold 623 0.21 130 20 264 -28 224' -50' 20 0540 0540 140 230 _ 225 _ - " 623m I 0.21 130-'_2__-- 20_0. 540 *_ 0 _1114 -0--23 ()--_mo_d ....

625 0.21I 130 i 2.01 -_81 13.41-lo,o_ -_j%o: 0:6_1010! 341(3_ 0:9_--

626: 0.21 ! 1301 2.0 17.3 -7.8 13.4! -10.0 20 0.430 0.440 10.0' 15.0! 2.0i .......

627/ 0.21 130.: 2.Q 17.3 -7.8 13.4 i -10.0 20 0.4301 0.44_ 15.0 5.9

627m[- 0.21 130 2.01 173i-781 13.41 -10.0i 20i ....01430 _ 0,4-4o 10.01--__9+mo]_ -

_ 627r 0.21 [ 130[__ 17.31 -7.81 13.41 -10.0_0_-_:430 _--i5.0 i _5.9;repea, -

627r2 0.21 i 130 2.0 17.3 -7.8 13.4-10.0 20 -&436__5.0[ 15.0-59_reepe_-- 628 i 0.21 130 2.0 17.3 -7_-10.0 -20 _ 6A30_o_o-t10.O * i5.L220; -- 6291 0.21 130, 2.0 83 -12.9 4.4 _ 0.300 0440 1001 1501 14- ....

30 0.21 130_20 8.3-12.9 4.41-15.0_-#0 o.30o 0.440 100 15.0 4,11

631 0.21 130 2.0 8.3 -12 9 4 4 -15.0 20 0.300 0.440 10.0 15.0' 15.3

_--OW2_ 130/ 2._ ;-/A -781 13.,_ -10.01 15/%:600 0,600 35.0 A-5_e-__-

633m 021 / 130 _- -2-0 17 3 78 13-_ i -_-'" ....... _- " ' --- - ____ ...... _ _._ ,,.,., -,.o ,o.l -10.0 15 0.600: _ 35.0 6.0 mold 0.21 130 ' 0.0 17.3 -7.8 13.4 -10_- -20-'---0._4__1-5_0_ 2;0_ ---- 1 / . / -78 134 -100 20, 0430 0440 10.0 150 220 644! __0_.21_130 4.0 17.3: -7.8 134 -10.0 20 0.430! 0.440_ 150 2.0: 0.21 130 40i 17 3 -7.8 13.4 -10_ * :_0-_ - 0.436_" 0.440 i0_-0_ 15.6__-- ¢_5mJ 0.21--_30_-_4.0 17.3 -7.8 13.4-10.0--3_ ()ii_40 _6! 59m_o/d ....

646 0.21 1301 40 173] -78! 13 41--10.0[_Q;,30 044_-_50 220----

-64_0-21 ! 130 t- 6:_ _-7.8, 13.4 ! -10.0 t 20 "_ 514_0_10_.0_-_5.0-_---

60, :43o: 0:44o 1ool 5o7

-649 0.21 __: 6:()17.3 _i3_41-10.0i 201-VA30_ 0_440" 10 _ i5.01 _-

665i o13: 83 - 13.4! .10 20'oeo7 -

656! 0.13 83 6.0 15.0 -91 134 -100 20 0430 i 0650 100, 150 _ ............

661 0.21 I 1301 0.0 28.2 -1.8 -2_ _ 2051 1.0(30 1000'35,5 100-0_ 15"04 ---- 44 NASA/TP----2000-210031 C6.--LaRC/LeRC ICING CONTAMINATION TESTS NOVEMBER 1998 Run nos. 301-310 ice shape 622-2D (SLA) Run nos. 23-35 clean wing Reynolds Mach number Reynolds Mach number number number 0.29 0.05 0.12 0.21 0.05 0.12 0.21 0.29 1 310 1 35 3 3O8 3 25 4.6 3O9 4.6 26 302 307 304 6.4 6.4 24 28 27 8.1 8.1 29 301 306 10 23 30 12 32 Run nos. 401-410 ice sha Runnos. 101-112 icesha Mach number Reynolds Reynolds Mach number number number 0.05 0.12 0.21 0.29 0.05 0.12 0.21 0.29 410 1 1 112 3 409 3 109 4.6 403 4.6 103 6.4 402 407 404 6.4 106 108 111 8.1 8.1 107 10 40 t 406 10 101 102 12 105 Run nos. 501-510 ice sha Run nos. 201-211 ice sha Reynolds Mach number Reynolds Mach number number number 0.05 0.12 0.21 0.29 0.21 0.29 0.05 0.12 510 1 1 211 5O8 3 3 208 4.6 504 4.6 6.4 502 507 505 207 210 6.4 202 8.1 8.1 10 501 503 201 203 Run nos. 701-705 clean wing Reynolds Mach number number 0.05 0.12 0.21 0.29 705 3 7O2 4.6 8.1 701 703 NAS A/TP--2000-210031 45

Appendix D1

Test Results, Business Jetmlst Entry

NAS A/TP--2000-210031 47

Business Jet- Run 072595.01

Tt = -0.8°C (30.6°F)

LWC = 0.54 g/m 3 C._t... = 0.0093

T, = -5.0°C (23.0°F)

C_-ic_ = 0.0481

MVD = 20 _m

V = 90 m/s (175 kts)

Spray = 6.0 min

Attitude = 6.1 o

chord = 90 cm (36 in)

0.08 0.06 0.04 0.02 o __ I I Ice Thickness -0.02 ower Max -0.04 -0.06 -0.05 0,00 0.05 0.10 0.15 0,20 0.25 X/C

48 NASA/TP--2000-210031

Business Jet - Run 072595.02

Cd<t_,n= 0.0093

LWC = 0.54 g/m 3

Tt = -0.8°C (30.6°F)

C__ic_= 0.0478

T, = -5.0°C (23.0°F)

MVD = 20 pm

V = 90 m/s (175 kts) Spray = 6.0 min

Attitude = 6.1°

chord = 90 cm (36 in)

0.08 0 06 0.04 0_02

J

u

Lower Max

I

i UpperMa x /t: _rnha tckoneu _ e

-0.02 _36" Tracin_l 11.43 mm IO45"/I 3.81 mm (0.15" I , -0.04 -0,06 ................. L ....................

_.05 0.00 005 010 0.15 020 0.25 X/C

NASA/TP--2000- 210031 49

Business Jet - Run 072595.03

Tt = -0.8°C (30.6°F) LWC = 0.54 g/m 3

T, = -5.0°C (23.0°F)

MVD = 20 p.m

V = 90 m/s (175 kts)

Spray = 22.5 min

Attitude = 6.1°

chord = 90 cm (36 in)

0,08 0.06 0.02 o

Upper Max Stagnation Line Lower Max

I ,ceT.,ckne.s I I

_36"Tracin_l 32.1 mm(1.26" I 12.8mml0.50" ) -0,02 _04 _0.06 ...................... _ ....................

-0.05 0.0o 0.05 0_I0 0.15 0,20 0.25 yJc

50 NASA/TP--2000-210031

Business Jet - Run 072595.04

LWC = 0.54 g/m 3

Tt = -0.800°C (30.6°F)

T, = -5.0°C (23.0°F)

MVD = 20 pm

Spray = 45.0 min

V = 90 m/s (175 kts)

Attitude = 6.103 chord = 90 cm (36 in)

0 O4 _11 Ice Thickness Lower Max -002 -004 -0 06 -o.o8 ................

o.o5 OlO o15 020 -o lO _ 05 o.oo xJc

NASA/TP--2000-210031 51

Business Jet - Run 072695.01

T, = -1.7°C (28.9°F) LVVC = 0.405 g/m 3 Cd-c_=n = 0.0093

T, = -5.9°C (21.4°F) C_._,_= 0.0258

MVD = 20 p.m

V = 90 m/s (175 kts) Spray = 4.4 min

Attitude = 6.1 o

chord = 90 cm (36 in)

0.08 F

I

i 0.06 0.04 0.02 J ooo Lower Max upper Max Sta_lnation Line I _36" Tracin_l 9.07 mm (0.36") 3.56 mm (0.14" 1 I Ice Thickness =0.02 -0.04 _306 _ ...........

-005 0.00 0.05 0.10 015 0,20 0.25 x/c

52 NASA/TP--2000-210031

Business Jet - Run 072695.02

LWC = 0.405 g/m 3 C,j-ci,,.n = 0.0093

Tt = -1.8°C (28.9°F)

C,j-ic_ = O. 0526

Ts = -6.0°C (21.2°F)

MVD = 20 p.m

Spray = 16.7 min

V = 90 m/s (175 kts)

Attitude = 6.1°

chord = 90 cm (36 in)

O08 0.06 0.02 J u !

000- Ice Thickness Lower Max UpperMax I Stagnation Line j 24.0 mm (094" I 11.8 mm (0.47" I 36" Tracing -0.02 -0.04 -006 .......................

015 020 _).05 000 005 010 _C

NASA/TP--2000-210031 53

Business Jet - Run 072695.03

"It = -1.7°C (28.9°F)

LWC = 0.405 g/m 3 C_._l=, = 0.0093

T, = -5.9°C (21.4°F)

C__,:,_= 0.1001

MVD = 20 I_m

V = 90 m/s (175 kts)

Spray = 33.3 min

Attitude = 6.1°

chord = 90 cm (36 in)

0.06 0.04 0.02 //

i ,ceThickn

Lower Max

O,_,oe.'.x I _*',,°..,'o°'-'ne I

__ . , . . " -0.02 -0.04

__ 119o > 21,rnm 10'_/

-0.08 -01o -0.05 0.00 0.05 0 10 015 0.20 X/C

54 NASA/TP--2000-210031

Business Jet- Run 072695.04

LVVC = 0.43 g/m 3 Cd-:_,,,o = 0.0093

Tt = -5.9°C (21.4°F)

Cd.i_ = 0.0202

T, = -10.0°C (14.0°F)

MVD = 20 p,m

V = 90 m/s (175 kts) Spray = 6.0 min

Attitude = 6.1°

chord = 90 cm (36 in)

0.06 c)

I I ,oe_,c_oe,_

Lower Max

upper Max Sta_lnation Line

I --36"Tracin_l , 8.9mm(.35")I 6_3mml25"/ I -002 _104 -006 .......................

0.20 025 _005 0.00 005 0.10 015 xJc

NASA/TP--2000-210031 55

Business Jet - Run 072695.05

"It = -5.9°C (21.4°F)

LVVC = 0.43 g/m 3 Cd._n = 0.0093

T, = -10.0°C (14.0°F)

Cd-_d = 0.0412

MVD = 20 Hm

V = 90 m/s (175 kts)

Spray = 45.0 min

Attitude = 6.1°

chord = 90 cm (36 in)

0.(38 • !

l 0.06 0.04 0.02

0.O0 _.-.---"_J I I ,ceT,,_°e,s

Lower Max

__ \ J J Upper Max [ Sta_lnation LineJ

-0.02 _ _ !--36"Tracin_ [ 67.2mm(264",J44.gmm(1.77.)[ -004 _ -0,06 ..............

-0.10 -0.05 0,00 005 010 0.15 0,20 x/C

I*

56 NAS A/TP----2000-210031

Business Jet - Run 072795.01

LWC = 0.43 g/m 3 Cd-:,_o= 0.0093

TI = -5.9°C (21.4°F)

Cd.ic_ = 0.0277

T, = -10.0°C (14.0°F)

MVD = 20 _m

Spray = 22.5 min

V = 90 m/s (175 kts)

Attitude = 6.1°

chord = 90 cm (36 in)

OO6 0.04

J

0 02 u 0.00

Lower Max

upper Max Sta_lnation Line I

I Ice Thickness I

I 32.0 mm (126') 20,3 mm (0.80") I

-002

cin_

-0.04 -006 ......

0.15 020 025 _0.05 0.00 0.05 0.10 x/c

NAS A/TP--2000-210031 57

Business Jet - Run 072795.02

"It = -5.9°C (21.4°F) LVVC = 0.60 g/m 3 Cd<l_n = 0.0093

T, = -10.0°C (14.0°F) Cd._ = 0.0125

MVD = 15 _m

V = 90 m/s (175 kts) Spray = 6.0 min

Attitude = 6.1°

chord = 90 cm (36 in)

o.oej

I

!

0.06 0.04 0.02 0,00 Lower Max Upper Max Stal]nation Line I Ice Thickness I 36" Tracin_ 11 mm (.43") 4.1 mm (.16"1 -0,02 -004 -0.06 -0.05 0.00 0.05 0.10 015 0,20 0.25 x/c

58 NASA/TP--2000-210031

Business Jet - Run 072795.03

C___t_,= 0.0093

LWC = 0.60 g/m 3

T, =-5.9°C (21.4°F)

Cd-io.d= 0.0251

T, = -10.0°C (14.0°F)

MVD = 15 _tm

V = 90 m/s (175 kts) Spray = 22.5 min

Attitude = 6.1 o

chord = 90 cm (36 in)

o Lower Max Upper Max Sta_lnation Line J Ice Thickness J 35" Tracing 45.1 mm/1.78 / -0.02 -0 04 -006 00o 005 o 10 015 020 • .0 05 x/c

NASA/TP--2000- 210031 59

Business Jet - Run 072795.04

"It = -6.0°C (21.4°F)

LWC = 0.60 g/m 3

Cd<t_, = 0.0093

T, = -10.0°C (14.0°F)

Cd..:_ = 0.0266

MVD = 15 p.m

V = 90 m/s (175 kts) Spray = 45.0 min

Attitude = 6.1 o

chord = 90 cm (36 in)

0.08 r

006 i

004 L l I i 0.00 [

Upper Max StaQnation Line I Lower Max

I

Ice Thickness I J

719 mm (2.83I

_)02 - _).04 -OC_i -0.I0 4_.05 0.00 0.05 010 0.15 020 xJc

60 NASA/TP--2000-210031

Business Jet - Run 072795.05

Cd<l,,o = 0.0093

LWC = 0.405 g/m 3

Tt = -11.0°C (12.3°F)

Cd.,c,_= 0.0197

T, = -15.0°C (5.0°F)

MVD = 20 pm

Spray = 4.4 min

V = 90 m/s (175 kts)

Attitude = 6.1°

chord = 90 cm (36 in)

0 O8

J

c> O.C(] Upper Max Stagnation Line Lower Max

I I I'ceT--ss I I

_36" Tracing 6.0 mm (24" I 4) 02 -004 -00.8 0.00 005 010 015 020 025 -005 x/c

NAS A/TP--2000-210031 61

Business Jet - Run 072795.06

Tt = -11.0°C (12.3°F) LWC = 0.405 g/m 3

Cd-cl,, = 0.0093

T, = -15.0°C (5.0°F)

Cd.ic_ = 0.0218

MVD = 20 pm

V = 90 m/s (175 kts)

Spray = 33,3 min

Attitude = 6.1 o

chord = 90 cm (36 in)

0.08 r 0.06 L 0.04 0.02 "_ I Ice Thickness 0.00 Lower Max -0.02

_oo, 1,0u_ ,-,;_, is",n"°° "he I

-004 -0.06 - - - _.i0 _},05 0.00 0.05 010 0.15 0.20 YJc .....

62 NASA/TP--2000-210031

Business Jet- Run 072895.02

Cd_clea n = 0.0082

T, = -1.3°C (29.7°F) LVVC = 0.50 g/m 3

T, = -9.3°C (15.3°F) Cd-_ = 0.0132

MVD = 15 pm

V = 129 m/s (250 kts) Spray = 3.9 min

Attitude = 1.6 °

chord = 90 cm (36 in)

0.06 .

004 , 002 • 0.00 •

Ice Thickness

Lower Max

36" Tracm

-0.02 , -004 -006 ...........................

-005 0.00 005 0 10 0 15 0 20 0.25 x/c

NASAITP--2000- 210031 63

Business Jet - Run 072895.03

Tt = -1.3°C (29.7°F)

LVVC = 0.50 g/m 3 C_._t_,o = 0.0082

T, = -9.3°C (15.3°F)

C_.,c_ = 0.0161

MVD = 15 pm

V = 129 m/s (250 kts) Spray = 7.2 min

Attitude = 1.6 °

chord = 90 cm (36 in)

0,08 0.06

J

0.02

J

J

u 0,011

Ice Thickness

Lower Max

36" Tr

-0.02 -004 -0.06 .......

-0.05 OCO 005 0 10 0.15 020 0.25 x,'C

64 NASA/TP--2000-210031

Business Jet- Run 072895.04

Cd-_l,_,= 0.0082

LVVC = 0.43 g/m 3

It = -2,2°C (28°F)

Cd-ic_ = 0.0170

Ts = -10.2°C (13.7°F)

MVD = 20 pm

V = 129 m/s (250 kts) Spray = 3.0 min

Attitude = 1.6 °

chord = 90 cm (36 in)

jf

/ • i 0.00

Upper Max Sta_lnation Line Lower Max

I Ice Thickness I _36" Tracin_ 3,38 mm t0.13"/ -002 -004 _0.o6 010 015 020 025 -005 000 0 05 X/C

NASA/TP--2000-210031 65

Business Jet- Run 072895.05

T, = -2.2°C (28.0°F)

LWC = 0.43 g/m 3

Cd-ct,an = 0.0082

T, =-10.2°C (13.7°F)

Cd-ic,d= 0.0264

MVD = 20 _m

V = 129 m/s (250 kts) Spray = 6.0 rain

Attitude = 1.6 °

chord = 90 cm (36 in)

OO8 0.06 i 000.

Ice Thickness Lower Max --36" _,02 -0.04 -006 _0.05 0.00 0.05 0.10 0.15 0.20 0.25 xJc

66 NASA/TP--2000-210031

Business Jet - Run 072895.06

C_._,_n= 0.0082

LWC = 0.54 g/m 3

T_= -2.2°C (28.0°F)

C__,c,_ = 0.0188

T, = -10.2°C (13.7°F)

MVD = 20 I_m

Spray = 3.0 min

V = 129 m/s (250 kts)

Attitude = 1.6°

chord = 90 cm (36 in)

0.06 0.04

J

0.02 u 0.00

Ice Thickness ]

I-- 36" Tracin_l I upper Max

I Sta,nation Line l Lower Max

8.88 rnrn/0.35") 9.35 mm (0.37" /

-0.02 -004 • -006 ...................

015 0.20 0.25 -0.05 000 005 010 YJC

NAS A/TP--2000-210031 67

Business Jet - Run 072895.07

"It = -2.2°C (28.0°F) LWC = 0.54 g/m 3

C_.cl_o= 0.0082

T, = -10.2°C (13.7°F)

Cd._ = 0.0315

MVD = 20 _m

V = 129 m/s (250 kts)

Spray = 6.0 min

Attitude = 1.6 °

chord = 90 cm (36 in)

0.08 ,

I

0.06 0.04 0.02 u L i 0(30 Ice Thickness Lower Max B36" -9.02 [

i

-004 i i _006 -0.05 0.00 0.05 0.10 0.15 0.20 025 X,'C

68 NASAJTP--2000-210031

Business Jet - Run 072895.08

LWC = 0.54 g/m 3 Cd-cl_n= 0.0093

T, = -11.0°C (12.3°F)

Cd.ic_ = 0.0220

Ts = -15.0°C (5.0°F)

MVD = 20 }am

V = 90 m/s (175 kts) Spray = 45.0 min

Attitude = 6.1° chord = 90 cm (36 in)

0.06 0.04 ¢.___,_._-_-_;_J I I ,ce Th,ck°e,, Lower Max

'___ I -_o Tracin_l I._==,_%?, 1 Sta_lnation.ne I

-0 02 -0 04 0.15 -0 10 X).05 0 00 0 05 0 10 X/C

NAS A/TP--2000-210031 69

Business Jet - Run 073195.01

Tt = -7.3°C (18.9°F)

LWC = 0.31 g/m 3 Cd._l_o= 0.0082

T, = -15.0°C (5.0°F) C_.,=_= 0.0125

MVD = 20 _um

V = 129 m/s (250 kts) Spray = 2.9 min

Attitude = 1.5 °

chord = 90 cm (36 in)

0.06 O00

Upper Max Leading Edge Lower Max

I I '°eT"'ck°e" 1 1

_36" Tracin 9 3.6 mm (,14") J -0.02 -0.04 -005 0.00 005 o. 10 0 15 0.20 0.25 x/c

70 NAS A/TP--2000-210031

Business Jet - Run 073195.02

Cd-cl_n= 0.0082

LWC = 0.31 g/m 3

T, = -7.3°C (18.9°F)

Cd_,=_ = 0.0134

T, = -15.0°C (5.0°F)

MVD = 20 pm

V = 129 m/s (250 kts) Spray = 5.8 min

Attitude = 1.5 °

chord = 90 cm (36 in)

0 08 0.06 0.04 0.02 0,00

upper Max I Leading Ed,qe I Lowe, M.x

Ice Thickness I I I --36" Tracing

I 7,67 mm/0,30"/

-002 -004 -006 015 0.20 0.25 0.10 _).05 0.(30 005 x/C

NAS A/TP--2000-210031 71

Business Jet - Run 073195.03

It = -11.0°C (12.3°F) LWC = 0.405 g/m 3

Cd-d_n= 0.0093

T, = -15.0°C (5.0°F)

C_-ic_ = 0.0220

MVD = 20 Hm

V = 90 m/s (175 kts)

Spray = 16.7 min

Attitude = 6.1 o

chord = 90 cm (36 in)

0,08 0,06 0.04 0,00

Lower Max

Upper Max Leadin_l Eddie

I I'ceTh'ckn" I

21,3 mm (0.84")

-002

1 _36" Tracin_

.0.04 i .0.06 ....

.0.05 000 005 0.10 015 0.20 0.25 x/c

72 NASA/TP--2000-210031

Business Jet- Run 073195.04

Cd.clea n " 0.0093

LVVC = 0.54 g/m 3

Tt = -11.0°C (12.3°F)

Cd-ic_ = 0.0212

Ts = -15.0°C (5.0°F)

MVD = 20 pm

Spray = 6.0 min

V = 90 m/s (175 kts)

Attitude = 6.1 o

chord = 90 cm (36 in)

0.08 0.06 0(30 Lower Max Stagnation Line 9.86 mm 10.39 '/ _.02 Ice Thickness -0.06 ..............

015 0.20 0.25 -005 000 0.05 010 x/c

NAS A/TP--2000- 210031 73

Business Jet - Run 073195.05

T, = -11.0°C (12.3°F)

LWC = 0.54 g/m 3 Cd.clea n -"0.0093

T, = -15.0°C (5.0°F)

Cd.,=_ = 0.0299

MVD = 20/am

V = 90 m/s (175 kts)

Spray = 22.5 min

Attitude = 6.1°

chord = 90 cm (36 in)

0,06 004 - 0.00 I I ,°eT.,okne..

f \ I J Upper Max 1 LeadingEdge

-oo2 _ _ I --36"Tracing I i40.2mm(1.58.,,I LowerMax J

_0.04 -006 ............................................

_). 10 -0.05 0.00 005 0,10 0.15 020 X/C

74 NAS A/TP--2000-210031

Business Jet - Run 080195.01

Cd-_,_, = 0.0082

LVVC = 0.41 g/m 3

T, = -12.5°C (9.5°F)

Cd-_:_ = 0.0091

T, = -20.0°C (4.3°F)

MVD = 40 pm

V = 129 m/s (250 kts) Spray = 0.7 min

Attitude = 1.5 °

chord = 90 cm (36 in)

0.08 0.06 0.04 Ice Thickness

Lower Max

I

Upper Max Leadin,qEd(:le

1.07 mn_ t0.04"/ I 36" Tracin_l -002 -004 -006 ..............

0 10 0 15 020 _) 05 000 005 x/C

NASA/TP--2000- 210031 75

Business Jet - Run 080195.02

T, =-12.5°C (9.5°F)

LWC = 0.41 g/m 3

Cd.c_o = 0.0082

T, = -20.0°C (-4.3°F)

Cd._ = 0.0112

MVD = 40 pm

V = 129 m/s (250 kts)

Spray = 1.5 min

Attitude = 1.5 °

chord = 90 cm (36 in)

0.06

o04 i

i 0.02 I i o ; 000: Upper Max Leadin 9 Edge J Lower Max

I I i ' Th'ckne [

_36" Tracin_l 2,87 mm (0.11" / J -0.02 -0.04 -0.05 0,00 0.05 010 0.15 0.20 0.25 x/C 'ili :41 '1

76 NAS A/TP--2000-2 t0031

Business Jet - Run 080195.03

Cd-_,_.= 0.0093

LWC = 0.535 g/m 3

Tt = -14.0°C (6.8°F)

Cd-ic. = 0.0188

Ts = -18.0°C (-0.4°F)

MVD = 20 #m

V = 90 m/s (175 kts) Spray = 6.0 min

Attitude = 6.1° chord = 90 cm (36 in)

Ice Thickness 13.00 Lower Max _02 -004 _).OB .............................

_005 0.00 0 05 0 10 015 0 20 X/C

NAS AffP--2000-210031 77

Business Jet - Run 080195.04

-It = -14.0°C (6.8°F) LWC = 0.535 g/m 3

C_-c_an = 0.0087

T, = -18.0°C (-0.4°F)

C_-ice_ = 0.0151

MVD = 20/am

V = 90 m/s (175 kts)

Spray = 6.0 min

Attitude = 4.0 °

chord = 90 cm (36 in)

0.02 /""/ I Ice Thickness O.OO Lower Max -0.02 -0.04 -0.06 -0.05 0.00 0.05 0.10 O. 15 020 0 25 X/C

78 NASA/TP--2000-210031

Business Jet - Run 080195.05

LWC = 0.535 g/m 3 C_<,_ = 0.0087

Tt = -14.0°C (6.8°F)

C__,_ = 0.0201

T, = -18.0°C (-0.4°F)

MVD = 40 _.m

V = 90 m/s (175 kts) Spray = 6.0 min

Attitude = 4.0 ° chord = 90 cm (36 in)

0.08 002 . lJ J o 001) J J Ice Thickness Lower Max -002 ; L -0.04 .

-006 .................................

-0.05 0.00 0.05 010 015 0.20 0.25 X/C

NASA/TP--2000-210031 79

Business Jet- Run 080195.06

"It = -14.0°C (6.8°F)

LVVC = 0.535 g/m 3

Cd._,,,,o = 0.0087

T, = -19.9°C (-3.7°F)

Cd.,=_= 0.0192

MVD = 40 pm

V = 109 m/s (212 kts) Spray = 6.0 min

Attitude = 4.0 °

chord = 90 cm (36 in)

0,08 0.06 0.04 I I Ice Thickness 0.00 _02 _,,____' \ _ I --36" Tracin_l I Upper Max I 1L.ega_rm g/E.d_le, i I Lower Max I -0.04 -oo6 ........................................

_)05 0.00 0.05 0 10 0 15 020 0.25 xJc

80 NASA/TP--2000-210031

Business Jet - Run 080195.07

Cd-cl_,n = 0.0087

LWC = 0.535 g/m 3

Tt = -14.0°C (6.8°F)

Cd_io_ = 0.0174

T, = -19.9°C (-3.7°F)

MVD = 20 pm

V = 109 m/s (212 kts) Spray = 6.0 min

Attitude = 4.0 °

chord = 90 cm (36 in)

0.04 0¸[7:)

Upper Max Leading Edge Lower Max

I I I'ceTh'c'°''s I

_36" Tracing] 11.8 mm t0.47') -002 .O, 04 -006 0 15 0 20 0.25 0(30 0.05 010 -O05 x/C

NAS A/TP--2000-210031 81

Business Jet- Run 080195.08

"It = -14.0°C (6.8°F) LVVC = 0.535 g/m 3

Cd-_l,,,n = 0.0093

T, = -18.0°C (-0.4°F)

Cd._ = 0.0302

MVD = 40 _m

V = 90 m/s (175 kts)

Spray = 6.0 min

Attitude = 6.2 °

chord = 90 cm (36 in)

0.08 0.06 O04 0.00

Upper Max Leading] EdFje Lower Max

I I Ice Thickness

_36" Tracin_l 123 mm (0.49" I

-0,02 -0.04 -0.06 -005 000 0.05 010 0.15 020 025 X/C

!'! i'iiii_iil

i¸ ii!ii_il; ¸

i!_

iiiii_ii_!iiii!i_

82 NAS A/TP--2000-210031

Business Jet - Run 080195.09

LVVC = 0.535 g/m 3 Cd-_l,,o= 0.0093

Tt = -14.0°C (6.8°F)

Cd._ = 0.0275

T, = -18.0°C (-0.4°F)

MVD = 40 [um

V = 90 m/s (175 kts) Spray = 4.2 min

Attitude = 6.2 °

chord = 90 cm (36 in)

0.08 0.06 0 O2 Ice Thickness t Upper Max I Leading Edge I Lower Max I s28 mm (0.33") I I -002 -0.04 -0.06 ......................

0.20 Q25 -0.05 000 0.05 0.10 015 X/C

NAS A/TP--2000-210031 83

Business Jet - Run 080295.01

"It = -0.8°C (31.0°F)

LWC = 0.54 g/m 3

C___,,,n = 0.0093

T, = -5.0°C (23.0°F)

Cd_ic_= 0.0679

MVD = 20 pm

V = 90 m/s (175 kts)

Spray = 12.0 min

Attitude = 6.0 °

chord = 90 cm (36 in)

O06 0,04 0.02 I Ice Thickness 0,(30 Lower Max

I Upper Max I Stagnation Line I

.0.02 _36"Tracin_ I 19,6 mm 10.77"11 8.20 mm I0.32" / -0.04 - 0.00 0.05 0,10 0.15 0.20 0,25 x/c

84 NASA/TP--2000-210031

Business Jet - Run 080295.02

Cd-cl_o= 0.0087

LVVC = 0.54 g/m 3

Tt = -0.8°C (31.0°F)

C_.,c_ = 0.0014

T, = -5.0°C (23.0°F)

MVD = 20 pm

V = 90 m/s (175 kts) Spray = 22.5 min

Attitude = 4.1°

chord = 90 cm (36 in)

0.08 0.06 0.04 0.02 u __j/ [ Ice Thickness 0.00 [ _ _ Lower Max -002 -0.04 -006 ..............................

-O.08 000 0.08 0 10 015 0 20 025 >dC

NASAfrP--2000- 210031 85

Business Jet - Run 080295.04

"It = -0.8°C (31.0°F) LWC = 0.54 g/m 3

C__cl_,= 0.0087

T, = -5.0°C (23.0°F)

C_._ = 0.0217

MVD = 20 _m

V = 90 m/s (175 kts)

Spray = 6.0 min

Attitude = 4.1°

chord = 90 cm (36 in)

o_o8 r

!

0.06 0.04 0.02 - u 0.170

__ J I Ice Thickness

I -_. T=o0 I_u,:: _oaX I ,St,_n,_oo_,_,,,,; I Lower Max J

43.02 -004 _0.06 i ...........

-0.05 0,00 0.05 010 015 0.20 0.25 x,'c

86 NASA/TP--2000-210031

Business Jet - Run 080295.05

Cd.clea n = 0.0087

LWC = 0.43 g/m 3

Tt = -3.9°C (24.9°F)

Cd-ic,_= 0.0352

T, = -10.0°C (14.0°F)

MVD = 20 _m

V = 109 m/s (212 kts) Spray = 22.5 min

Attitude = 4.1° chord = 90 cm (36 in)

0.08 i i _ickness Lower Max _)02 _)04 -006 ............

010 0 15 020 025 -0 05 000 0,05 xJc

NASA/TP--2000-210031 87

Business Jet- Run 080295.06

T, = -0.8°C (31.0°F)

LVVC = 0.54 g/m 3

C___l_,o = 0.0087

T, = -5.0°C (23.0°F)

Cd_,:_= 0.0679

MVD = 20 pm

V = 90 m/s (175 kts) Spray = 22.5 min

Attitude = 4.1 o

chord = 90 cm (36 in)

0,08 0.04 0.02 u

I I Joe T,iokne,s I

0.00 I I Upper Max I Sta_lnation Line I Lower Max I -002

I _36"Tracin_ I 32.0 mm (1.26")1 7.32mm (0.29" I ] I

_).04 -006 _)05 Q00 005 0,10 0.15 0.20 0.25 X/C

88 NASA/TP--2000-210031

Business Jet- Run 080395.01

Cd__,_,o = 0.0082

LVVC = 0.75 g/m 3

T, = -0.7°C (30.8°F)

Cd-iced = 0.0380

T, = -8.7°C (16.3°F)

MVD = 15 p.m

Spray = 10.0 rain

V = 129 m/s (250 kts)

Attitude = 1.5 ° chord = 90 cm (36 in)

006 - 0.04¸ 0.0(I i Ice Thickness i Lower Max 36" Tracir -002 -004 , -006 ...................

-0 05 O.00 005 0 10 0.15 :'Jc

NASA/TP--2000-210031 89

Business Jet - Run 080395.02

T, = -0.7°C (30.8°F) LWC = 1.25 g/m 3

Cd_:,_,o = 0.0082

T, = -8.7°C (16.3°F)

C_.,_ = 0.0247

MVD = 20 !um

V = 129 m/s (250 kts)

Spray = 5.4 min

Attitude = 1.5 °

chord = 90 cm (36 in)

0.04 0 O2 0,00 Ice Thickness Lower Max --45" Traci_ -O.02 -004 -O.06 -O05 000 0.05 0.10 015 0.20 0.25 XJC

90 NASA/TP--2000-210031

Business Jet - Run 080395.03

Cd_clea n = 0.0093

LWC = 1.00 g/m 3

Tt = -2.0°C (28.4°F)

C_.,c_ = 0.0775

T, = -6.2°C (20.9°F)

MVD = 15 p.m

V = 90 m/s (175 kts) Spray = 15.0 min

AOA = 6.1 °

chord = 90 cm (36 in)

J

ceThck

I I UpperMax I Stal]nati°nLine I LowerMax _0 O2 I _36"Tracin_l I 36.6 mm (144")1 128.7 mm (1,13") -004 _o.o6 ......

005 OlO o15 0,20 _3.o5 o.oo xJc

NASA/TP--2000-210031 91

Business Jet - Run 080395.04

"It = -4.4°C (24.2°F)

LWC = 1.60 g/m 3

Cd.clea n = 0.0093

T, = -8.5°C (16.7°F)

C_._,_= 0.1027

MVD = 20 pm

V = 90 m/s (175 kts)

Spray = 8.4 min

Attitude = 6.1°

chord = 90 cm (36 in)

008 , 0.06 0,04 0,02 o 0.00 Lower Max Upper Max Stagnation Line I Ice Thickness _36"Tracin_] 38.5mm/1,51" / 14.0mm(0.55 ) I -002 _)04 _.06 -005 000 005 0.10 015 020 0.25 xJc

92 NASA/TP--2000-210031

Business Jet - Run 080395.05

LVVC = 0.75 g/m 3

Tt = -7.4°C (18.8°F)

Ts = -15.2°C (4.7 °F)

MVD = 15 p.m

Spray = 10.0 min

V = 129 m/s (250 kts)

Attitude = 1.60

chord = 90 cm (36 in)

o

Upper Max Stagnation Line Lower Max

I I i'c'_'ck°'ss i I

_36"Tracina I 28.7mm(1.13") 16,8mm(0.66") 27.9mm(1.10") -9 O2 -O04 -0.06 .......................

020 025 -005 0.O0 0.05 010 0.15 xJc

NASA/TP--2000-210031 93

Business Jet - Run 080395.06

Tt = -7.4°C (18.8°F) LWC = 1.25 g/m 3

Cd-cl=o= 0.0082

T, = -15.2°C (4.7°F)

C,-,c_ = 0.0577

MVD = 20 _.m

V = 129 m/s (250 kts)

Spray = 5.4 min

Attitude = 1.6 °

chord = 90 cm (36 in)

0.08 0.06 0.04 0.02 0.00

Lower Max

Upper Max I Sta_lnation Line I

I I Ice Thickness I

_36" Tracin_l I 34,3 mm 11.35") I 11.3 mm (0.44"} I

_02 -0.04 -006 .............

_).05 0(30 0.05 010 015 0.20 0.25 xJC

i_i:!!iii_iii

94 NASA/TP--2000-210031

Business Jet - Run 080395.07

Cd-c,_n= 0.0093

LWC = 1.60 g/m 3

T, = -11.0°C (12.3°F)

Cd-ic_ = 0.0433

Ts = -15.0°C (5.0°F)

MVD = 20 pm

V = 90 m/s (175 kts) Spray = 8.4 min

Attitude = 6.1 o chord = 90 cm (36 in)

008 r 0.06 0.04 u J 009_ __...._ I Ice Thickness I Stagnation Lin Lower Max I _36"Tracir 21.6 mm {0.85 .

-0.02 -004 4306 ...........................

-o lo -005 o.oo 005 o lO 0.15 x/c

NASA/TP--2000- 210031 95

Business Jet - Run 080495.01

TI = -27.8°C (-18.0°F) LVVC = 0.83 g/m 3

T, = -31.6°C (-24.9°F)

MVD = 160 pm

V = 90 m/s (175 kts)

Spray = 6.0 min

Attitude = 6.1 o

chord = 90 cm (36 in)

0.08 0.06 0.04 J 002 i 0.00 I --36" Tracing 18,4U3PmP_ ;a;3,,)I StaFIn:tiOn Line I -0 02 __ Lower Max J -0.04 _.o6 .....

-0.05 o.00 0.05 0.10 015 020 025 X/C

96 NASA/TP--2000-210031

Business Jet- Run 080495.02

LVVC = 0.83 g/m 3

"It = -27.8°C (-18.0°F)

T, = -31.6°C (-24.9°F)

MVD = 160 pm

V = 90 m/s (175 kts) Spray = 6.0 min

Attitude = 4.1 o

chord = 90 cm (36 in)

O08 0.06 0,02 o % 0(73 I Ice Thickness Lower Max ] Upper Max ] Stagnation Line I

-002 _ I _36" Tracin_l I I

_O4 -0(1t3 _ .....................

020 025 -005 0.(30 0 05 0 10 0 15 YJc

NAS A/TP--2000-210031 97

Business Jet - Run 080495.04

Tt = -11.0°C (12.2°F)

LWC = 0.83 g/m 3

T, = -15.0°C (5.0°F)

MVD = 160 Hm

V = 90 m/s (175 kts)

Spray = 20.0 min

Attitude = 4.1°

chord = 90 cm (36 in)

006 , I

o.o4

I

I 002 i

_racin

-0.08 -0.10 -0.05 0,00 0,05 010 0.15 0.20 X/C

98 NASA/TP--2000-210031

Business Jet- Run 080495.05

LWC = 0.83 g/m 3

Tt = -0.8°C (30.6°F)

T, = -5.00C (23.0°F)

MVD = 160 pm

Spray = 20.0 min

V = 90 m/s (175 kts)

Attitude = 6.2 °

chord = 90 cm (36 in)

008 •

i

o.c_ [ i oo4 i L I 0.02 i i u I Ice Thickness 0.00 i

I Lower Max

Upper Max Sta,qnation I

_36" Tracin_ 34.2 mm (1.35") I ' Line 4?.02 -004 _).o6 .............................

-005 000 005 0 10 0 15 0 20 X/C

NAS A/TP--2000- 210031 99

Business Jet - Run 080495.06

Tt = -0.8°C (30.6°F)

LWC = 0.54 g/m 3

Cd-cl_o= 0.0093

T, = -5.0°C (23.0°F)

C_._ = 0.1201

MVD = 20 p.m

V = 90 m/s (175 kts)

Spray = 22.5 min

Attitude = 6.2 °

chord = 90 cm (36 in)

0.08 0.06 0.04 u 0.00 Ice Thickness Lower Max -0.02 -004 -0.06 *0.05 o.oo 0,05 010 015 0.20 0.25 X/C

100 NAS A/TP----2000-210031

Appendix D2

Test Results, Business Jet--2nd Entry

NAS A/TP--2000-210031 101

Business Jet - Run 201

Tt = -0.8°C (30°F)

LWC = 0.405 g/m 3

C_._l_n= 0.0092

T, = -5.0°C (22°F)

Cd.,c,_= 0.0353

MVD = 20 pm

V = 90.0 m/s (175 kts)

Spray = 4.4 min Ci.ctea n -" 0.676

AOA = 6.2 °

chord = 90 cm (36 in) C,=ed= 0.654

0.08 r _:_ Thickn@s_ upper Max Leadin_ Edge Lower Max --42" Tracing 6,7 mm (.27") 4.3 mm (.17") 2.5 mm (0,10") 0.06 36" Tracing 5.6 mm (.22") 3.5 mm (. 14") 1.8 mm (0.07") -- 30" Tracing 6.7 mm (.26") 4.4 mm (.17") 3.7 mm (0.15") 0.04

J

u 0,00 -0.02 -0.04 -0.06 .....

-005 0,00 0,05 0.10 0.15 020 0,25 X/C 1.2 ........

Clean --e-- Iced

.=_=

E

=_

-I ;

o o

0.0 5.0 10.0 15.0 Angle of Attack, deg

102 NASA/TP---2000-210031

Business Jet - Run 202

Cd-clo_n = 0.0092

LVVC = 0.54 g/m 3

Tt = -0.8°C (30°F)

Cd-_ = 0.0293

T, =-5.0°C (22°F)

MVD = 20 I_m

C_-:_e,o = 0.676

Spray = 2.0 min

V = 90.0 m/s (175 kts)

Cl-,ced = 0.646

AOA = 6.2 °

chord = 90 cm (36 in)

0.08 Ice Thickness Leading Edge Lower Max upper Max 4.0 mm (.16") 25 mm (.10") -- 42" Tracing _ 36" Tracing 27 mm (.11") 2.1 mm (.08") 30" Tracing 3.7 mm (.15") 2.8 mm (.11") u -002 -004 -o D6 .......................................

-0 05 00O 0 05 0 10 0 15 020 025 :,dC 1.2- - _ _-- - , + Clean --e-- Iced 1.0 0,8 = .e 0.6 o O 0,2 0,0 ........ L ......

0.0 5.0 10.0 15.0 AngLe of Attack, deg

NAS A/TP--2000-210031 103

Business Jet- Run 202m

"It =-0.8°C (30°F)

LWC = 0.54 g/m 3

C_-_te,, = 0.0092

T, = -5.0°C (22°F)

Cd-_d = 0.0292

MVD = 20/am

V = 90.0 m/s (175 kts)

Spray = 2.0 min Cl-_Lean = 0.676

AOA = 6.2 °

chord = 90 cm (36 in) C_-ic,d = 0.661

0.08 Ice Thickness i

Upper Max Leadin_l Edge Lower Max

-- 42" Tracing 0.06 i 36" Tracing 30" Tracing 5.0 mm (20") 4.2 mm (.17") 27 mm (.11") i 0.04 !

0.02 i 0.00 F i -0.02 -0.04 4) 06 -0.05 000 0.05 0.10 015 0.20 0.25 x/c 1.2 I 0.0 0.0 5.0 10.0 15.0 Angle of Attack, deg

104 NAS A/TP--2000-210031

Business Jet - Run 202r

C,<_, = 0.0092

LWC = 0.54 g/m 3

Tt = -0.8°C (30°F)

C,_ic_ = 0.0291

T, = -5.0°C (22°F)

MVD = 20 _m

Cl_clea n = 0.676

Spray = 2.0 min

V = 90.0 m/s (175 kts)

AOA = 6.2 ° Cl-_e_= 0.651

chord = 90 cm (36 in)

0.08 Ice Thickness Upper Max Leading Edge Lower Max -- 42" Tracing 3.7 mm (.15") 2.2 mm (.09") 0.06 _36" Tracing 2.9 mm (.12") 2.2 mm (,09") 3.7 mm (.15") 2.7 mm (.11") 30" Tracing 0.04 J 0.02 J u -002 _04 _o6 0 15 020 025 ooo 005 olo -o.o5 x/c 1,2

I

+ Clean + Iced 1.0 0.8 o 0.6

E

_J 0.4 0.2 0.0 ....

15.0 0.0 5.0 10.0 Angle of Attack, deg

i

NASA/TP--2000- 210031 105

Business Jet - Run 203

"It = -0.8°C (30°F)

LWC = 0.54 g/m 3 C_.c,=n= 0.0092

T, = -5.0°C (22°F)

Cd.,=_= 0.0158

MVD = 20 pm

V = 90.0 m/s (175 kts) Cl.clea n " 0.676

Spray = 6.0 min

AOA = 6.2 °

Cl-_ed= 0.631

chord = 90 cm (36 in)

0.08 Ice Thickness i Lower Max Upper Max Leadina Edae -- 42" Tracing 11.1 mm (0.44") 5.60 mm (0.22") 36" Tracing 11.0 mm (0.43") 5.20 mm (0.21") - 30" Tracing 11.9 mm (0.47") 5.30 mm (0.21") 0.04 X)02

!

-0.04 -0.06 -0.05 0.00 0,05 010 0.15 020 025 x/c 1,2

i

Clean --e-- Iced

I

1.0

i

i 0.0 0.0 5.0 10.0 15.0 Angle of Attack, dog

106 NASA/TP--2000-210031

Business Jet - Run 204

Cd_,_ao = 0.0092

LWC = 0.54 g/m 3

Tt = -0.8°C (30°F)

C_-_,d= 0.1104

T, = -5.0°C (22°F)

MVD = 20 pm

Ci_,..o = 0.676

Spray = 22.5 min

V = 90.0 m/s (175 kts)

C_-,cea = 0.632

AOA = 6.2 °

chord = 90 cm (36 in)

Ice Thickness Upper Max Leadin_l Eddie Lower Max 40.8 mm (1.61") 11.1 mm (0.44") 20.4 mm (0.80") -- 42" Tracing 0.06 _36" Tracing 37.7 mm (1.49") 100 mm (0.40") 19.7 mm (0.77") 44.4 mm (1,75") 11 4 mm (0,45") 22.9 mm (0.90") L 30" Tracing 004 .

ooo2

-004 - " -006 000 005 010 015 0.20 025 -0 05 X/C 1.2 i Clean --e-- Iced 1.0 i 0.6 0.4 0.8 __ 0.2 0.0 + 15.0 5,0 10.0 0.0 Angle of Attack, deg

NASA/TP--2000-210031 107

Business Jet - Run 205

Tt = -5.9°C (20.8°F)

LWC = 0.535 g/m 3

Cd-_,,,,n = 0.0092

T, =-10.0°C (13.4°F)

C,-i_ = 0.0173

MVD = 40 pm

V = 90.0 m/s (175 kts)

Spray = 1.1 min Cl..clea n - 0.676

AOA = 6.2 °

chord = 90 cm (36 in) C_-iced = 0.668

Ice Thickness

i

Leading Edge Lower Max

Upper Max

-- 42" Tracing 2.3 mm (.09") 0.06 !

2.4 mm (.09") 36" Tracin_ 30" Tracing 2.2 mm (,09") I

o.o21

J 0(30 _ -002 i 4).04 -006 _.05 0.00 0.05 015 0,20 025 X/C 1.2 I --a-Clean--e--Iced 0.8 0.6 !

-I

L

0.0 0.0 5.0 10.0 15,0 Angle of Attack, deg

108 NAS A/TP--2000-210031

Business Jet - Run 205r

Cd-c_o = 0.0092

LWC = 0.535 g/m _

Tt = -5.9°C (20.8°F)

Cd._ = 0.0176

Ts = -10.0°C (13.4°F)

MVD = 40 pm

C_-clean = 0.676

Spray = 1.1 min

V = 90.0 m/s (175 kts)

Cl-iced = 0.662

AOA = 6.2 °

chord = 90 cm (36 in)

0.08 Ice Thickness Leadin_ Ed,qe Lower Max Upper Max -- 42" Tracing 2.8 mm (.11") 0.06 36" Tracing 1,9 mm (,08") 1.5 mm (06") 30" Tracing 0.04 0.02 o 0.00 -002 -004 -006 .........

020 025 005 0 10 0 15 -0.05 000 xJc 1.2 - --l--Clean ---t-- Iced 1.0 0.8 0.6 O O -I 0.4 --- 0.2 0.0, - ! ......

0.0 5,0 10.0 150 Angle of Attack, deg

NAS A/TP--2000- 210031 109

Business Jet - Run 206

"1", = -5.9°C (20.8°F)

LWC = 0.535 g/m 3

C,._,_,, = 0.0092

"Is =-10.0°C (13.4°F)

Cd-ic_ = 0.0176

MVD = 40 pm

V = 90.0 m/s (175 kts)

Spray = 4.2 min C,-_l_.o = 0.676

AOA = 6.2 °

chord = 90 cm (36 in) C_-iced = 0.637

0.08 Ice Thickness Upper Max Leading Eddie Lower Max -- 42" Tracing 10.2 mm (0.40") 11.0 mm (0,44") 6,9 mm (0,27") 0,06 8.8 mm (0.35") 36" Tracin_l 9.1 mm (0.36") 5.6 mm (0.22") .... 30" Tracing 9,9 mm (0.39") 10.5 mm (0.41") 6.6 mm (0.26") 0.04

u j/

0(30 -o 02 -0.04 _].06 -0.05 0.(30 0,05 O.10 0 15 020 0.25 X/C 1.2 T 1.0 0.8 0.6 i rj 0,4 i 0.0 0.0 5.0 10.0 15.0 Angle of Attack, deg

110 NASA/TP--2000-210031

Business Jet - Run 207

LWC = 0.43 g/m 3 Cd_clea n "- 0.0092

Tt = -5.9°C (20.8°F)

Cd-_ = 0.0186

T, = -10.0°C (13.4°F)

MVD = 20 pm

C_lean= 0.676

V = 90.0 m/s (175 kts) Spray = 2.0 min

Ct-iced = 0.657

AOA = 6.2 °

chord = 90 cm (36 in)

Ice Thickness

Lower Max

Leadin_l Eddie

upper Max

2.5 mm (.10") -- 42" Tracing _36" Tracing 2.2 mm (.09") 30" Tracing 2.7 mm (.t1") 0.04 0.02 u 00(1 -002 -0 04 -006 ...........

010 015 0.20 -005 OO0 005 x/C 1.2 -- -- Clean --e-- Iced 1,0 0.8 0.6 0.4 0,2 - -_ | ._ _ 0.0 j 0.0 5.0 10.0 15.0 Angle of Attack, deg

NASA/TP--2000-210031 111

Business Jet - Run 208

Tt = -5.9°C (20.8°F) LWC = 0.43 g/m 3

Cd-c_n = 0.0092

T, = -10.0°C (13.4°F)

Cd-ic_ = 0.0301

MVD = 20 t_m

V = 90.0 m/s (175 kts)

Spray = 6.0 min C_leao = 0.676

AOA = 6.2 °

chord = 90 cm (36 in) Cl-_ = 0.641

0.08 Ice Thickness Lower Max

upper Max Leading Edge

-- 42" Tracing 9.8 mm (.38") 5.8 mm (.23") OO6 36" Tracing 8.4 mm (.33") 53 mm (.21") 30" Tracing 9.6 mm (,38") 5.8 mm (.23") 0.04 0 O2 u 0.00 - i i -0.02 , -0.04 i _.o6 L -0.05 0.00 0,05 010 0.15 0.20 xJc

1.2 _ .......... •

Clean _ Iced r o

=_

-J 0,4 i 0.2 5.0 10.0 15.0 Angle of Attack, deg

112 NASA/TP 2000-210031

Business Jet - Run 209

Cd-d_n= 0.0092

LVVC = 0.43 g/m 3

T_= -5.9°C (20.8°F)

Cd-_ = 0.0343

T, = -10.0°C (13.4°F)

MVD = 20 pm

C_cl_n= 0.676

Spray = 22.5 min

V = 90.0 m/s (175 kts)

AOA = 6.2 ° C_.iced = 0.655

chord = 90 cm (36 in)

0.08 Ice Thickness Upper Max Leading Edge Lower Max 37.7 mm (1.48") 25.9 mm (1.02") -- 42" Tracing 0.06 i 32.6 mm (129") 22.0 mm (0.87") _36" Tracin_ 37.5 mm (1.48") 24.7 mm (0,97") -- 30" Tracing 002 .

/ u 0.017, -0.02 -004 .

-006 ..........

020 025 005 010 015 _.05 000 xJc 1,2 - -- Clean + Iced 1.0 _ * - 0.8_ - - - 0.6.

-i 0.4 15,0 5.0 10,0 Angle of Attack, dog NASA/TP--2000-210031 113

Business Jet - Run 210

It = -11.0°C (11.7°F)

LWC = 0.405 g/m 3 Cd-d_n= 0.0092

T, = -15°C (4.4°F)

Cd-ic_ = 0.0171

MVD = 20 pm

V = 90.0 m/s (175 kts) Cl-cje,,= 0.676

Spray = 2.0 min

AOA = 6.2 °

Cl-,=ed = 0.660

chord = 90 cm (36 in)

0.08 Ice Thickness Lower Max upper Max Leadin_l Eddie -- 42" Tracing 2.3 mm (.09") 36" Tracing 2.0 mrn (.08") 30" Tracing 2.3 mm (.09") 0.04

J

0.00 -0.02 -0.04 -0.06 ....

-0.05 O00 0.05 010 015 0.20 0.25 X/C 1.2 ----=-- Clean --e- Iced i i

,_==

E O =_ .,J 0.4 F 0.2 0.0' 0.0 5.0 10.0 15.0 Angle of Attack, deg 114 NAS A/TP---2000-210031

Business Jet- Run 211

LVVC = 0.405 g/m 3 Cd-d_o = 0.0092

"It = -11.0°C (11.7°F)

Cd_icl_ I = 0.0252

Ts = -15°C (4.4°F)

MVD = 20 #m

Cl-_,eao = 0.676

Spray = 4.4 min

V = 90.0 m/s (175 kts)

AOA = 6.2 ° C_-_ed = 0.647

chord = 90 cm (36 in)

Ice Thickness Lower Max Leading Edge upper Max 5.8 mm (23") 5.8 mm (.23") -- 42" Tracinc_ 5.2 mm (20") 5.2 mm (20") 36" TracinQ 6.6 mm (26") 5.7 mm (.23") 30" Tracing 0.04 0,02 u -002 .006 ..................

0.15 020 0.25 -005 000 005 010 xJc 1.2 .... _ -- I

• -.- Clean _ Iced

1.0 0.8 _ 0.5 0.4 0.2 0,0 .......

0.0 5.0 10.0 15.0 Angle of Attack, deg

NASA/TP--2000-210031 l 15

Business Jet - Run 212

T: = -11.0°C (11.7°F)

LVVC = 0.405 g/m 3

Cd.cl,,,n = 0.0092

T, = -15°C (4.4°F)

Cd.ic_ = 0.0287

MVD = 20 pm

V = 90.0 m/s (175 kts)

Spray = 16.7 min C_de,, = 0.676

AOA = 6.2 °

C_.i_ed = 0.658

chord = 90 cm (36 in)

Ice Thickness 30" Tracing I Upper Max I Leadin_lEd_le I Lower Max J 24.0 mm (0.95") J 21.9 mm (0,86") I 0,06 F 004 - 0.02 - u .0.02 -004 -0.06 .005 0.00 0.05 0,10 020 0,25 X/C O .d

o.o i i

0.0 5.0 10.0 15.0 Angle of Attack, deg l 16 NASA/TP---2000-210031

Business Jet- Run 213

Cd-c_o = 0.0092

LWC = 0.60 g/m 3

T, = -5.9°C (20.8°F)

Cd-,;_ = 0.0129

Ts = -10.0°C (13.4°F)

MVD = 15 tJm

C,-c_,n= 0.676

V = 90.0 m/s (175 kts) Spray = 2.0 min

C_-ioed = 0.660

AOA = 6.2 °

chord = 90 cm (36 in)

Ice Thickness Upper Max Leading Edge Lower Max --42" Tracing 3.3 mm (.13") _36" Tracing 3.1 mm (.12") 30" Tracing 3.6 mm (.14") -002 -0.04 *0.05 ...............

0,15 O20 025 _).05 0.00 0.05 010 x/C 1.2 T I Clean +Iced 1_0 , 0.0 • 15.0 5,0 10.0 0.0 Angle of Attack, deg NASA/TP--2000-210031 117

Business Jet - Run 214

Tt = -5.9°C (20.8°F)

LWC = 0.60 g/m 3

Cd-_,,a, = 0.0092

T, = -10.0°C (13.4°F)

Cd.ic_ = 0.0158

MVD = 15 _m

V = 90.0 m/s (175 kts)

Spray = 6.0 min C_<leao = 0.676

AOA = 6.2 °

chord = 90 cm (36 in) C_-iced = 0.675

0.08 ice Thickness Lower Max upper Max Stagnation Line -- 42" Tracing 12.1 mm _.48") 0.06 - 36" Tracing 11.1 mm (0.44") L -- 30" Tracing 12.6 mm (0.50") 0.02 -0.02 -0.04 -0,06 <}.05 000 0.05 0.10 015 0,20 0,25 x/C 1.2 Clean --e-- Iced

! f

'_o.o! __7,/ i

0.4 !.... _

i '

0,0 5.0 10,0 15.0 Angle of Attack, deg

118 NAS A/TP--2000- 210031

Business Jet - Run 221

LVVC = 0.54 g/m 3 Cd-_n = 0.0081

Tt = -0.8°C (30°F)

Cd-ic_ = 0.0151

T, = -5.0°C (22°F)

MVD = 20 pm

C_cle,o = 0.228

Spray = 3.0 min

V = 129 m/s (250 kts)

AOA = 1.5 ° C_._ed = 0.220

chord = 90 cm (36 in)

0.08 Ice Thickness Lower Max Upper Max Leading Edge 2.8 mm (. 11") 7.8 mm (31") 7.0 mm (27") -- 42" Tracing 6.6 mm (.26") 2.6 mm (.10") 63 mm (25") 36" Tracing 7.6 mm (.30") - 30" Tracing 7.8 mm (31") 2.6 mm (.10") o 02 0.(30 -0.02 _O.04 -0.08 ...............

015 0.20 0.25 -0.05 0.00 0,05 010 X/C 1.2 1.0 0.8 .O 0.6 O O (J

¢_

-I 0.4 0.2 0.0 ,-- 15.0 0,0 5.0 10.0 Angle of Attack, deg

NASA/TP--2000-210031 119

Business Jet - Run 222

Tt = -0.8°C (30°F) LWC = 0.54 g/m 3

Cd-c_,n= 0.0081

Ts = -5.0°C (22°F)

C_.ic_ = 0.0238

MVD = 20 pm

V = 129 m/s (250 kts)

Spray = 6.0 min C__c_,o = 0.228

AOA = 1.5 °

chord = 90 cm (36 in) C_-_ed = 0.222

0,08 Ice Thickness ; Upper Max Lower Max Leadin_ Edge -- 42" Tracing 14.5 mm (0.57") 5.5 mm (0.22") 13.5 mm (0.53") 0.06, _36" Tracing 14.3 mm (0.56") 4.8 mm (0.19") 12.3 mm (0.48") i i 30" Tracing 16,1 mm (0.64") 5,1 mm (0.20") 15.6 mm (0,61") 0.04 - 0,02 u -0.02 _04 -006 , -0.05 0.00 0.05 0.10 015 0,20 0,25 X/C --.m-- Clean _ Iced 1.0 _-_ i

o8 i

c E 0.4 0,2 0,0 ± 0.0 5.0 10.0 15.0 Angle of Attack, deg 120 NAS A/TP--2000- 210031

Business Jet - Run 223

C___,_n = 0.0081

LWC = 0.31 g/m 3

It = -0.8°C (30°F)

C_._ = 0.0125

Ts = -5.0°C (22°F)

MVD = 20 pm

Cb-c,eao = 0.228

V = 129 m/s (250 kts) Spray = 2.9 min

C_-_c.d = 0.226

AOA = 1.5 °

chord = 90 cm (36 in)

Ice Thickness Upper Max Leading Edge Lower Max -- 42" Tracing 8.7 mm (34") 3.8 mm (.15") 8.3 mm (.33") 36" Tracin_l 7.7 mm (.31 ") 3.6 mm (. 14") 7.6 mm (.30") 30" Tracing 9.1 mm (36") 3,8 mm (. 15") 7.7 mm (.30") 0.02 u -0 02 _).04 -0.06 ................................

-005 0.00 005 010 015 0.20 0.25 XlC 1,2 -- --a--Clean--e--Iced 1.0 0.8_ 0,6 O O 0.4 0.2 0.0 - 15.0 0.0 5.0 10.0 Angle of Attack, deg

NASA/TP--2000-210031 121

Business Jet - Run 224

Tt = -0.8°C (30°F)

LWC = 0.31 g/m 3

Cd_l_,n= 0.0081

T, = -5.0°C (22°F)

Cd-_ = 0.0179

MVD = 20 pm

V = 129 m/s (250 kts)

Spray = 5.8 min C_-_,.,n = 0.228

AOA = 1.5 °

C_-iced = 0.232

chord = 90 cm (36 in)

Ice Thickness

Upper Max Leadin_l Edc=le Lower Max -- 42" Tracing 17.8 mm (0.70") 7.60 mm (0.30") 16.8 mm (0.66") 0.06 _36" Tracin_ 17.3 mm (0.68") 6.80 mm (027") 13.2 mm (0.52") ..... 30" Tracin_ 17,8 mm (0.70") 6.90 mm (0.27") 15.8 mm (0.62") 0_04 I 0.02 L u .0,02 .0.04 - -006 -0.05 O00 005 010 0.15 0.20 0.25 _c 1.2

f

1.0 0.8 C

._o

0.6

! i

0.4 0.2 i i

i

I

i

0.0 '- 0.0 5.0 10.0 15.0 Angle of Attack, deg

122 NASA/TP--2000-210031

Business Jet - Run 225

C___o = 0.0081

LWC = 0.50 g/m 3

T_= -5.9°C (20.8°F)

Cd.,_ = 0.0096

T, = -10.0°C (13.4°F)

MVD = 15 pm

Ct-_,,an = 0.228

V = 129 m/s (250 kts) Spray = 3.6 min

Ct-,ce_ = 0.217

AOA = 1.5 °

chord = 90 cm (36 in)

0.08 Ice Thickness Upper Max Leading Edge Lower Max -- 42" Tracing 1.7 mm (.07") 0,06 1.7 mm (.07") 36" Tracing 30"Traong 1.7 mm (.07") 0.02 jJ o 0,00_ -0,02 • -004 , -0 05 0 oo 005 0 to 0.15 0.20 xJc

1.2- -- i " -

--=--Clean --e--Iced

1.o "

0.8 0.6 0.4 0.2 0.0 _ 15,0 0,0 5.0 10.0 Angle of Attack, deg

NASA/TP--2000-210031 123

Business Jet - Run 226

"It = -5.9°C (20.8°F)

LVVC = 0.50 g/m 3 Cd-_t_,n = 0.0081

T, = -10.0°C (13.4°F)

C_-ic_ = 0.0113

MVD = 15/_m

V = 129 m/s (250 kts) C_,_o = 0.228

Spray = 7.2 min

AOA = 1.5°

Cl__ = 0.227

chord = 90 cm (36 in)

0.08 Ice Thickness Lower Max upper Max Leadin_l Eddie -- 42" Tracing 3.8 mm (.15") 0.06 _36" Tracing 3.8 mm (.15") 30" Tracing 3.9 mm (.15") 0.04 0.02 r -002 -0.04 -0.06 -0.05 0(73 005 010 0.15 020 0.25 x/c i 0,8 O

.=_