AH 93-W-257 (ah93w257-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: AH 93-W-257 (ah93w257-il) Reynolds number: 1,000,000 Max Cl/Cd: 120.72 at α=8.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-ah93w257-il-1000000.txt Download as CSV file: xf-ah93w257-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: AH 93-W-257
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
------ -------- --------- --------- -------- -------- --------
-19.000 -1.1366 0.09585 0.09165 -0.0237 1.0000 0.0800
-18.750 -1.1361 0.09279 0.08858 -0.0248 1.0000 0.0818
-18.500 -1.1358 0.08972 0.08549 -0.0258 1.0000 0.0837
-18.250 -1.1297 0.08739 0.08312 -0.0266 1.0000 0.0854
-18.000 -1.1301 0.08427 0.07999 -0.0275 1.0000 0.0876
-17.750 -1.1319 0.08102 0.07672 -0.0285 1.0000 0.0900
-17.500 -1.1286 0.07842 0.07411 -0.0293 1.0000 0.0924
-17.250 -1.1251 0.07582 0.07147 -0.0300 1.0000 0.0945
-17.000 -1.1271 0.07266 0.06831 -0.0309 1.0000 0.0978
-16.750 -1.1260 0.06986 0.06551 -0.0316 1.0000 0.1009
-16.500 -1.1233 0.06727 0.06289 -0.0323 1.0000 0.1040
-16.250 -1.1247 0.06429 0.05992 -0.0329 1.0000 0.1082
-16.000 -1.1240 0.06152 0.05714 -0.0336 1.0000 0.1123
-15.750 -1.1241 0.05875 0.05439 -0.0341 1.0000 0.1173
-15.500 -1.1247 0.05594 0.05158 -0.0346 1.0000 0.1225
-15.250 -1.1216 0.05341 0.04868 -0.0358 0.8335 0.1292
-15.000 -1.1221 0.05091 0.04602 -0.0360 0.7917 0.1356
-14.750 -1.1235 0.04828 0.04332 -0.0363 0.7656 0.1436
-14.500 -1.1263 0.04548 0.04047 -0.0366 0.7453 0.1515
-14.250 -1.1233 0.04328 0.03824 -0.0368 0.7292 0.1601
-14.000 -1.1255 0.04059 0.03553 -0.0371 0.7153 0.1692
-13.750 -1.1237 0.03834 0.03327 -0.0373 0.7031 0.1780
-13.500 -1.1194 0.03628 0.03117 -0.0376 0.6918 0.1865
-13.250 -1.1170 0.03411 0.02902 -0.0377 0.6827 0.1956
-13.000 -1.1118 0.03218 0.02705 -0.0379 0.6730 0.2034
-12.750 -1.1050 0.03042 0.02529 -0.0381 0.6656 0.2117
-12.500 -1.0982 0.02866 0.02354 -0.0382 0.6587 0.2191
-12.250 -1.0903 0.02705 0.02190 -0.0384 0.6513 0.2270
-12.000 -1.0812 0.02556 0.02039 -0.0385 0.6442 0.2339
-11.750 -1.0740 0.02395 0.01879 -0.0385 0.6395 0.2413
-11.500 -1.0620 0.02277 0.01760 -0.0385 0.6341 0.2475
-11.250 -1.0596 0.02120 0.01602 -0.0379 0.6288 0.2544
-11.000 -1.0416 0.02027 0.01504 -0.0386 0.6224 0.2607
-10.750 -1.0249 0.01883 0.01363 -0.0401 0.6192 0.2684
-10.500 -1.0014 0.01789 0.01268 -0.0418 0.6157 0.2757
-10.250 -0.9763 0.01681 0.01159 -0.0440 0.6116 0.2830
-10.000 -0.9483 0.01594 0.01071 -0.0463 0.6074 0.2904
-9.750 -0.9184 0.01531 0.01002 -0.0485 0.6026 0.2962
-9.500 -0.8869 0.01443 0.00914 -0.0515 0.5976 0.3041
-9.250 -0.8544 0.01391 0.00860 -0.0537 0.5952 0.3102
-9.000 -0.8203 0.01323 0.00792 -0.0566 0.5922 0.3169
-8.750 -0.7858 0.01269 0.00736 -0.0593 0.5890 0.3236
-8.500 -0.7523 0.01239 0.00701 -0.0612 0.5857 0.3285
-8.250 -0.7162 0.01182 0.00644 -0.0643 0.5821 0.3357
-8.000 -0.6817 0.01151 0.00608 -0.0665 0.5779 0.3420
-7.750 -0.6479 0.01129 0.00582 -0.0683 0.5747 0.3485
-7.500 -0.6130 0.01094 0.00551 -0.0705 0.5728 0.3571
-7.250 -0.5798 0.01079 0.00533 -0.0720 0.5704 0.3624
-7.000 -0.5466 0.01061 0.00513 -0.0734 0.5678 0.3667
-6.750 -0.5129 0.01040 0.00493 -0.0751 0.5651 0.3720
-6.500 -0.4799 0.01027 0.00478 -0.0764 0.5624 0.3764
-6.250 -0.4473 0.01020 0.00465 -0.0776 0.5595 0.3801
-6.000 -0.4146 0.01013 0.00454 -0.0788 0.5560 0.3839
-5.750 -0.3814 0.01001 0.00441 -0.0803 0.5528 0.3888
-5.500 -0.3484 0.00989 0.00430 -0.0815 0.5513 0.3930
-5.250 -0.3156 0.00981 0.00420 -0.0827 0.5495 0.3969
-5.000 -0.2830 0.00976 0.00411 -0.0837 0.5473 0.3999
-4.750 -0.2499 0.00962 0.00400 -0.0850 0.5452 0.4049
-4.500 -0.2170 0.00953 0.00391 -0.0862 0.5429 0.4091
-4.250 -0.1845 0.00948 0.00384 -0.0873 0.5406 0.4132
-4.000 -0.1521 0.00946 0.00378 -0.0883 0.5381 0.4167
-3.750 -0.1197 0.00944 0.00373 -0.0893 0.5351 0.4204
-3.500 -0.0872 0.00942 0.00371 -0.0904 0.5315 0.4250
-3.250 -0.0545 0.00935 0.00365 -0.0915 0.5303 0.4291
-3.000 -0.0220 0.00931 0.00361 -0.0925 0.5288 0.4331
-2.750 0.0104 0.00929 0.00357 -0.0934 0.5271 0.4362
-2.500 0.0430 0.00922 0.00353 -0.0944 0.5252 0.4409
-2.250 0.0755 0.00918 0.00351 -0.0954 0.5232 0.4454
-2.000 0.1078 0.00917 0.00349 -0.0964 0.5212 0.4495
-1.750 0.1399 0.00918 0.00347 -0.0972 0.5189 0.4530
-1.500 0.1719 0.00919 0.00346 -0.0981 0.5164 0.4564
-1.250 0.2040 0.00920 0.00347 -0.0990 0.5133 0.4609
-1.000 0.2359 0.00926 0.00353 -0.0998 0.5105 0.4648
-0.750 0.2681 0.00925 0.00353 -0.1007 0.5095 0.4686
-0.500 0.3002 0.00925 0.00354 -0.1015 0.5081 0.4718
-0.250 0.3323 0.00925 0.00354 -0.1023 0.5063 0.4746
0.000 0.3644 0.00922 0.00355 -0.1032 0.5043 0.4789
0.250 0.3964 0.00923 0.00357 -0.1040 0.5022 0.4826
0.500 0.4282 0.00925 0.00360 -0.1047 0.5002 0.4862
0.750 0.4599 0.00929 0.00363 -0.1055 0.4981 0.4893
1.000 0.4915 0.00936 0.00366 -0.1062 0.4958 0.4918
1.250 0.5228 0.00942 0.00371 -0.1069 0.4929 0.4950
1.500 0.5543 0.00949 0.00380 -0.1076 0.4902 0.4989
1.750 0.5860 0.00950 0.00385 -0.1083 0.4889 0.5022
2.000 0.6176 0.00953 0.00391 -0.1090 0.4873 0.5052
2.250 0.6492 0.00956 0.00396 -0.1097 0.4855 0.5079
2.500 0.6807 0.00960 0.00400 -0.1103 0.4834 0.5102
2.750 0.7122 0.00965 0.00404 -0.1110 0.4812 0.5122
3.000 0.7434 0.00965 0.00409 -0.1116 0.4790 0.5163
3.250 0.7744 0.00972 0.00416 -0.1122 0.4766 0.5194
3.500 0.8052 0.00983 0.00427 -0.1127 0.4736 0.5221
3.750 0.8359 0.00995 0.00439 -0.1133 0.4707 0.5246
4.000 0.8671 0.00999 0.00446 -0.1138 0.4692 0.5270
4.250 0.8983 0.01003 0.00453 -0.1144 0.4673 0.5293
4.500 0.9293 0.01009 0.00460 -0.1150 0.4650 0.5311
4.750 0.9602 0.01011 0.00466 -0.1155 0.4626 0.5342
5.000 0.9909 0.01015 0.00474 -0.1160 0.4599 0.5373
5.250 1.0212 0.01024 0.00483 -0.1164 0.4568 0.5397
5.500 1.0509 0.01041 0.00498 -0.1168 0.4527 0.5420
5.750 1.0816 0.01045 0.00507 -0.1172 0.4501 0.5445
6.000 1.1122 0.01048 0.00515 -0.1177 0.4469 0.5469
6.250 1.1425 0.01054 0.00523 -0.1181 0.4433 0.5490
6.500 1.1724 0.01064 0.00532 -0.1184 0.4392 0.5506
6.750 1.2011 0.01082 0.00546 -0.1186 0.4335 0.5525
7.000 1.2317 0.01080 0.00553 -0.1191 0.4300 0.5560
7.250 1.2616 0.01087 0.00564 -0.1194 0.4253 0.5586
7.500 1.2903 0.01100 0.00577 -0.1196 0.4192 0.5609
7.750 1.3191 0.01114 0.00592 -0.1197 0.4126 0.5630
8.000 1.3480 0.01126 0.00606 -0.1199 0.4050 0.5652
8.250 1.3752 0.01150 0.00626 -0.1198 0.3972 0.5674
8.500 1.4040 0.01163 0.00642 -0.1200 0.3899 0.5695
8.750 1.4300 0.01192 0.00666 -0.1197 0.3790 0.5710
9.000 1.4570 0.01216 0.00688 -0.1196 0.3680 0.5721
9.250 1.4825 0.01242 0.00713 -0.1193 0.3568 0.5755
9.500 1.5061 0.01281 0.00749 -0.1187 0.3429 0.5782
9.750 1.5279 0.01329 0.00791 -0.1178 0.3263 0.5805
10.000 1.5476 0.01387 0.00842 -0.1166 0.3078 0.5826
10.250 1.5640 0.01457 0.00902 -0.1150 0.2871 0.5846
10.500 1.5752 0.01545 0.00979 -0.1126 0.2645 0.5865
10.750 1.5791 0.01648 0.01071 -0.1091 0.2435 0.5884
11.000 1.5743 0.01760 0.01177 -0.1042 0.2260 0.5901
11.250 1.5727 0.01911 0.01320 -0.1008 0.2086 0.5915
11.500 1.5688 0.02112 0.01517 -0.0981 0.1927 0.5926
11.750 1.5644 0.02366 0.01768 -0.0965 0.1780 0.5942
12.000 1.5597 0.02655 0.02056 -0.0954 0.1652 0.5969
12.250 1.5534 0.02971 0.02371 -0.0943 0.1537 0.5989
12.500 1.5459 0.03300 0.02701 -0.0933 0.1434 0.6007
12.750 1.5389 0.03624 0.03026 -0.0923 0.1342 0.6025
13.000 1.5299 0.03962 0.03365 -0.0912 0.1261 0.6041
13.250 1.5190 0.04319 0.03722 -0.0901 0.1183 0.6057
13.500 1.5106 0.04653 0.04058 -0.0891 0.1111 0.6073
13.750 1.5037 0.04979 0.04385 -0.0882 0.1044 0.6088
14.000 1.4960 0.05330 0.04735 -0.0875 0.0979 0.6101
14.250 1.4903 0.05667 0.05073 -0.0870 0.0916 0.6114
14.500 1.4872 0.05979 0.05386 -0.0865 0.0856 0.6126
14.750 1.4817 0.06327 0.05733 -0.0861 0.0802 0.6136
15.000 1.4786 0.06647 0.06052 -0.0857 0.0746 0.6145
15.250 1.4761 0.06969 0.06377 -0.0855 0.0697 0.6164
15.500 1.4744 0.07287 0.06697 -0.0853 0.0652 0.6188
15.750 1.4724 0.07607 0.07018 -0.0852 0.0608 0.6209
16.000 1.4711 0.07926 0.07340 -0.0851 0.0572 0.6228
16.250 1.4705 0.08233 0.07649 -0.0850 0.0537 0.6246
16.500 1.4693 0.08557 0.07975 -0.0850 0.0505 0.6263
16.750 1.4688 0.08870 0.08291 -0.0851 0.0477 0.6279
17.000 1.4697 0.09167 0.08589 -0.0851 0.0449 0.6295
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