AH 93-W-174 (ah93w174-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: AH 93-W-174 (ah93w174-il) Reynolds number: 1,000,000 Max Cl/Cd: 148.38 at α=9° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-ah93w174-il-1000000.txt Download as CSV file: xf-ah93w174-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: AH 93-W-174
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 1.000 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-18.250 -0.9198 0.09139 0.08855 -0.0536 1.0000 0.0198
-18.000 -0.9433 0.08394 0.08099 -0.0580 1.0000 0.0199
-17.750 -0.9668 0.07662 0.07356 -0.0623 1.0000 0.0199
-17.500 -0.9886 0.06965 0.06647 -0.0665 1.0000 0.0201
-17.250 -1.0099 0.06291 0.05962 -0.0706 1.0000 0.0201
-17.000 -1.0264 0.05697 0.05356 -0.0743 1.0000 0.0202
-16.750 -1.0396 0.05169 0.04815 -0.0775 1.0000 0.0204
-16.500 -1.0482 0.04717 0.04352 -0.0803 1.0000 0.0205
-16.250 -1.0530 0.04336 0.03961 -0.0825 1.0000 0.0207
-16.000 -1.0556 0.04000 0.03615 -0.0843 1.0000 0.0209
-15.750 -1.0545 0.03724 0.03329 -0.0855 1.0000 0.0210
-15.500 -1.0510 0.03489 0.03085 -0.0864 1.0000 0.0212
-15.250 -1.0610 0.03145 0.02732 -0.0873 1.0000 0.0215
-15.000 -1.0634 0.02901 0.02481 -0.0875 1.0000 0.0219
-14.750 -1.0522 0.02711 0.02286 -0.0888 0.9988 0.0223
-14.500 -0.9449 0.02502 0.02060 -0.1076 0.9158 0.0235
-14.250 -0.8992 0.02407 0.01917 -0.1138 0.8106 0.0242
-14.000 -0.8918 0.02321 0.01810 -0.1124 0.7739 0.0246
-13.750 -0.8814 0.02249 0.01722 -0.1111 0.7488 0.0249
-13.500 -0.8777 0.02140 0.01599 -0.1093 0.7287 0.0253
-13.250 -0.8758 0.02031 0.01479 -0.1070 0.7123 0.0259
-13.000 -0.8691 0.01955 0.01394 -0.1049 0.6984 0.0264
-12.750 -0.8603 0.01897 0.01328 -0.1026 0.6864 0.0269
-12.500 -0.8510 0.01852 0.01276 -0.1002 0.6768 0.0273
-12.250 -0.8358 0.01813 0.01229 -0.0986 0.6676 0.0280
-12.000 -0.8187 0.01768 0.01177 -0.0973 0.6600 0.0285
-11.750 -0.7987 0.01736 0.01136 -0.0963 0.6526 0.0291
-11.500 -0.7825 0.01678 0.01070 -0.0949 0.6460 0.0299
-11.250 -0.7646 0.01621 0.01009 -0.0937 0.6400 0.0309
-11.000 -0.7436 0.01583 0.00966 -0.0929 0.6341 0.0317
-10.750 -0.7215 0.01550 0.00928 -0.0922 0.6286 0.0325
-10.500 -0.6981 0.01519 0.00892 -0.0917 0.6241 0.0335
-10.250 -0.6739 0.01495 0.00861 -0.0912 0.6194 0.0342
-10.000 -0.6534 0.01441 0.00802 -0.0903 0.6149 0.0357
-9.750 -0.6298 0.01407 0.00766 -0.0898 0.6110 0.0370
-9.500 -0.6049 0.01379 0.00734 -0.0895 0.6075 0.0382
-9.250 -0.5795 0.01356 0.00706 -0.0891 0.6035 0.0393
-9.000 -0.5556 0.01320 0.00666 -0.0887 0.5996 0.0411
-8.750 -0.5310 0.01292 0.00635 -0.0883 0.5953 0.0430
-8.500 -0.5047 0.01268 0.00609 -0.0881 0.5928 0.0447
-8.250 -0.4780 0.01249 0.00587 -0.0879 0.5900 0.0460
-8.000 -0.4530 0.01212 0.00549 -0.0876 0.5869 0.0489
-7.750 -0.4266 0.01191 0.00527 -0.0874 0.5838 0.0514
-7.500 -0.3997 0.01179 0.00508 -0.0873 0.5805 0.0532
-7.250 -0.3740 0.01149 0.00479 -0.0871 0.5774 0.0570
-7.000 -0.3467 0.01129 0.00459 -0.0870 0.5751 0.0600
-6.750 -0.3195 0.01108 0.00437 -0.0870 0.5725 0.0634
-6.500 -0.2924 0.01087 0.00417 -0.0869 0.5698 0.0677
-6.250 -0.2647 0.01075 0.00401 -0.0869 0.5672 0.0708
-6.000 -0.2378 0.01053 0.00381 -0.0868 0.5645 0.0765
-5.750 -0.2103 0.01045 0.00368 -0.0868 0.5612 0.0808
-5.500 -0.1827 0.01023 0.00350 -0.0868 0.5595 0.0876
-5.250 -0.1545 0.01009 0.00337 -0.0869 0.5573 0.0927
-5.000 -0.1267 0.00989 0.00321 -0.0869 0.5550 0.1017
-4.750 -0.0987 0.00974 0.00307 -0.0870 0.5526 0.1104
-4.500 -0.0706 0.00961 0.00296 -0.0870 0.5502 0.1192
-4.250 -0.0428 0.00947 0.00284 -0.0871 0.5478 0.1316
-4.000 -0.0150 0.00937 0.00276 -0.0872 0.5450 0.1446
-3.750 0.0133 0.00923 0.00267 -0.0873 0.5431 0.1590
-3.500 0.0417 0.00907 0.00257 -0.0874 0.5413 0.1755
-3.250 0.0702 0.00892 0.00249 -0.0876 0.5392 0.1939
-3.000 0.0986 0.00878 0.00241 -0.0878 0.5370 0.2144
-2.750 0.1269 0.00863 0.00233 -0.0879 0.5349 0.2387
-2.500 0.1553 0.00849 0.00226 -0.0881 0.5328 0.2658
-2.250 0.1834 0.00836 0.00221 -0.0883 0.5304 0.2980
-1.750 0.2398 0.00804 0.00214 -0.0886 0.5261 0.3797
-1.500 0.2684 0.00785 0.00210 -0.0889 0.5243 0.4261
-1.250 0.2969 0.00769 0.00208 -0.0891 0.5223 0.4714
-1.000 0.3256 0.00757 0.00207 -0.0893 0.5204 0.5117
-0.750 0.3544 0.00749 0.00207 -0.0895 0.5184 0.5471
-0.500 0.3830 0.00743 0.00209 -0.0897 0.5163 0.5766
-0.250 0.4117 0.00743 0.00211 -0.0898 0.5140 0.6020
0.000 0.4402 0.00747 0.00218 -0.0899 0.5111 0.6246
0.250 0.4692 0.00744 0.00221 -0.0901 0.5097 0.6443
0.500 0.4983 0.00743 0.00225 -0.0903 0.5081 0.6602
0.750 0.5273 0.00744 0.00229 -0.0905 0.5062 0.6747
1.000 0.5564 0.00746 0.00232 -0.0907 0.5042 0.6885
1.250 0.5852 0.00747 0.00236 -0.0909 0.5021 0.7016
1.500 0.6139 0.00750 0.00241 -0.0910 0.4999 0.7131
1.750 0.6425 0.00758 0.00247 -0.0912 0.4977 0.7244
2.000 0.6708 0.00769 0.00258 -0.0913 0.4950 0.7350
2.250 0.6997 0.00771 0.00264 -0.0915 0.4936 0.7448
2.500 0.7285 0.00773 0.00270 -0.0916 0.4918 0.7549
2.750 0.7571 0.00776 0.00277 -0.0917 0.4897 0.7647
3.000 0.7857 0.00781 0.00284 -0.0919 0.4877 0.7745
3.250 0.8140 0.00785 0.00291 -0.0920 0.4856 0.7825
3.500 0.8423 0.00792 0.00299 -0.0921 0.4834 0.7905
3.750 0.8704 0.00802 0.00308 -0.0921 0.4808 0.7974
4.000 0.8983 0.00812 0.00320 -0.0922 0.4784 0.8044
4.250 0.9270 0.00817 0.00328 -0.0924 0.4768 0.8113
4.500 0.9549 0.00820 0.00336 -0.0924 0.4747 0.8179
4.750 0.9831 0.00825 0.00345 -0.0925 0.4724 0.8248
5.000 1.0112 0.00831 0.00353 -0.0926 0.4701 0.8310
5.250 1.0386 0.00838 0.00363 -0.0926 0.4677 0.8373
5.500 1.0660 0.00850 0.00374 -0.0926 0.4648 0.8440
5.750 1.0933 0.00860 0.00388 -0.0925 0.4622 0.8501
6.000 1.1208 0.00863 0.00397 -0.0925 0.4597 0.8568
6.250 1.1485 0.00868 0.00405 -0.0926 0.4564 0.8633
6.500 1.1749 0.00872 0.00414 -0.0923 0.4528 0.8699
6.750 1.2011 0.00885 0.00426 -0.0921 0.4487 0.8771
7.000 1.2275 0.00891 0.00438 -0.0919 0.4451 0.8839
7.250 1.2541 0.00895 0.00449 -0.0918 0.4413 0.8913
7.500 1.2799 0.00903 0.00459 -0.0915 0.4368 0.8988
7.750 1.3039 0.00916 0.00473 -0.0909 0.4312 0.9075
8.000 1.3296 0.00919 0.00484 -0.0905 0.4259 0.9161
8.500 1.3755 0.00938 0.00509 -0.0888 0.4127 0.9409
8.750 1.3994 0.00944 0.00522 -0.0882 0.4060 0.9656
9.000 1.4289 0.00963 0.00541 -0.0889 0.3967 1.0000
9.250 1.4525 0.00990 0.00564 -0.0885 0.3841 1.0000
9.750 1.4953 0.01060 0.00624 -0.0869 0.3552 1.0000
10.000 1.5134 0.01104 0.00662 -0.0855 0.3371 1.0000
10.250 1.5268 0.01164 0.00713 -0.0834 0.3146 1.0000
10.500 1.5316 0.01238 0.00774 -0.0798 0.2910 1.0000
10.750 1.5307 0.01325 0.00850 -0.0753 0.2669 1.0000
11.000 1.5263 0.01428 0.00942 -0.0706 0.2443 1.0000
11.250 1.5185 0.01556 0.01060 -0.0659 0.2235 1.0000
11.500 1.5087 0.01716 0.01214 -0.0616 0.2060 1.0000
11.750 1.4984 0.01916 0.01409 -0.0582 0.1899 1.0000
12.000 1.4888 0.02148 0.01637 -0.0555 0.1747 1.0000
12.250 1.4777 0.02417 0.01902 -0.0531 0.1590 1.0000
12.750 1.4602 0.02968 0.02448 -0.0496 0.1349 1.0000
13.000 1.4490 0.03276 0.02753 -0.0480 0.1221 1.0000
13.250 1.4432 0.03547 0.03024 -0.0468 0.1131 1.0000
13.500 1.4350 0.03845 0.03320 -0.0456 0.1037 1.0000
13.750 1.4261 0.04159 0.03631 -0.0446 0.0938 1.0000
14.000 1.4211 0.04450 0.03921 -0.0439 0.0853 1.0000
14.250 1.4179 0.04734 0.04205 -0.0433 0.0777 1.0000
14.500 1.4140 0.05034 0.04504 -0.0429 0.0708 1.0000
14.750 1.4111 0.05330 0.04798 -0.0426 0.0639 1.0000
15.000 1.4104 0.05613 0.05083 -0.0424 0.0579 1.0000
15.250 1.4094 0.05904 0.05374 -0.0423 0.0526 1.0000
15.500 1.4079 0.06205 0.05673 -0.0422 0.0474 1.0000
15.750 1.4091 0.06484 0.05954 -0.0423 0.0433 1.0000
16.000 1.4089 0.06784 0.06255 -0.0425 0.0394 1.0000
16.250 1.4097 0.07076 0.06548 -0.0427 0.0357 1.0000
16.500 1.4105 0.07375 0.06849 -0.0430 0.0324 1.0000
16.750 1.4109 0.07683 0.07157 -0.0434 0.0294 1.0000
17.000 1.4126 0.07981 0.07460 -0.0439 0.0270 1.0000
17.250 1.4130 0.08297 0.07777 -0.0444 0.0245 1.0000
17.500 1.4147 0.08604 0.08089 -0.0450 0.0229 1.0000
17.750 1.4154 0.08925 0.08411 -0.0456 0.0212 1.0000
18.000 1.4167 0.09247 0.08738 -0.0464 0.0201 1.0000
18.250 1.4190 0.09555 0.09051 -0.0472 0.0189 1.0000
18.500 1.4194 0.09893 0.09393 -0.0481 0.0179 1.0000
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