AH 93-W-257 (ah93w257-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: AH 93-W-257 (ah93w257-il) Reynolds number: 500,000 Max Cl/Cd: 92.68 at α=8.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-ah93w257-il-500000-n5.txt Download as CSV file: xf-ah93w257-il-500000-n5.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 = 0.500 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.000 -1.0530 0.10604 0.10107 -0.0219 1.0000 0.0803
-18.750 -1.0507 0.10309 0.09812 -0.0231 1.0000 0.0824
-18.500 -1.0479 0.10022 0.09520 -0.0241 1.0000 0.0845
-18.250 -1.0439 0.09751 0.09246 -0.0252 1.0000 0.0864
-18.000 -1.0429 0.09445 0.08940 -0.0263 1.0000 0.0886
-17.750 -1.0418 0.09139 0.08632 -0.0273 1.0000 0.0908
-17.500 -1.0371 0.08884 0.08374 -0.0282 1.0000 0.0929
-17.250 -1.0330 0.08621 0.08109 -0.0291 1.0000 0.0952
-17.000 -1.0341 0.08295 0.07782 -0.0301 1.0000 0.0979
-16.750 -1.0306 0.08030 0.07515 -0.0309 1.0000 0.1009
-16.500 -1.0263 0.07775 0.07259 -0.0317 1.0000 0.1038
-16.250 -1.0236 0.07464 0.06918 -0.0336 0.8442 0.1075
-16.000 -1.0210 0.07231 0.06665 -0.0338 0.7986 0.1111
-15.750 -1.0197 0.06964 0.06385 -0.0344 0.7733 0.1147
-15.500 -1.0187 0.06693 0.06105 -0.0350 0.7544 0.1191
-15.000 -1.0160 0.06159 0.05558 -0.0362 0.7250 0.1289
-14.500 -1.0146 0.05623 0.05014 -0.0373 0.7030 0.1415
-14.250 -1.0126 0.05373 0.04759 -0.0378 0.6932 0.1485
-14.000 -1.0127 0.05103 0.04488 -0.0383 0.6847 0.1564
-13.750 -1.0115 0.04852 0.04235 -0.0387 0.6758 0.1641
-13.500 -1.0078 0.04625 0.04004 -0.0391 0.6681 0.1720
-13.250 -1.0064 0.04382 0.03763 -0.0395 0.6614 0.1802
-13.000 -1.0021 0.04166 0.03543 -0.0398 0.6547 0.1877
-12.750 -0.9974 0.03960 0.03336 -0.0401 0.6486 0.1962
-12.500 -0.9929 0.03752 0.03126 -0.0404 0.6435 0.2037
-12.250 -0.9853 0.03574 0.02949 -0.0407 0.6387 0.2120
-12.000 -0.9793 0.03385 0.02759 -0.0409 0.6337 0.2190
-11.750 -0.9702 0.03225 0.02597 -0.0412 0.6288 0.2265
-11.500 -0.9606 0.03074 0.02443 -0.0413 0.6240 0.2328
-11.250 -0.9523 0.02913 0.02280 -0.0415 0.6200 0.2398
-11.000 -0.9397 0.02788 0.02154 -0.0417 0.6160 0.2464
-10.750 -0.9332 0.02622 0.01989 -0.0418 0.6117 0.2535
-10.500 -0.9201 0.02509 0.01874 -0.0419 0.6073 0.2603
-10.250 -0.9117 0.02369 0.01733 -0.0418 0.6033 0.2665
-10.000 -0.9035 0.02258 0.01619 -0.0412 0.5996 0.2731
-9.750 -0.8868 0.02157 0.01515 -0.0418 0.5966 0.2793
-9.500 -0.8692 0.02037 0.01397 -0.0431 0.5937 0.2866
-9.250 -0.8461 0.01951 0.01308 -0.0445 0.5905 0.2936
-9.000 -0.8219 0.01849 0.01207 -0.0465 0.5872 0.3007
-8.750 -0.7945 0.01768 0.01122 -0.0487 0.5838 0.3084
-8.500 -0.7653 0.01686 0.01039 -0.0512 0.5802 0.3163
-8.250 -0.7338 0.01608 0.00956 -0.0540 0.5766 0.3271
-8.000 -0.7005 0.01532 0.00882 -0.0571 0.5737 0.3362
-7.750 -0.6669 0.01483 0.00830 -0.0596 0.5712 0.3425
-7.500 -0.6335 0.01446 0.00788 -0.0617 0.5685 0.3471
-7.250 -0.5993 0.01402 0.00745 -0.0641 0.5657 0.3523
-7.000 -0.5654 0.01370 0.00709 -0.0662 0.5629 0.3572
-6.750 -0.5321 0.01347 0.00679 -0.0679 0.5602 0.3619
-6.500 -0.4992 0.01326 0.00654 -0.0695 0.5574 0.3659
-6.250 -0.4661 0.01305 0.00630 -0.0711 0.5544 0.3703
-6.000 -0.4329 0.01287 0.00610 -0.0727 0.5519 0.3750
-5.750 -0.3999 0.01271 0.00591 -0.0741 0.5497 0.3794
-5.500 -0.3670 0.01257 0.00574 -0.0755 0.5475 0.3830
-5.250 -0.3339 0.01240 0.00559 -0.0769 0.5451 0.3871
-5.000 -0.3009 0.01227 0.00544 -0.0783 0.5428 0.3917
-4.750 -0.2681 0.01217 0.00531 -0.0796 0.5404 0.3961
-4.500 -0.2355 0.01209 0.00517 -0.0808 0.5379 0.3997
-4.250 -0.2029 0.01199 0.00507 -0.0820 0.5354 0.4034
-4.000 -0.1703 0.01192 0.00497 -0.0832 0.5327 0.4078
-3.750 -0.1376 0.01185 0.00489 -0.0844 0.5306 0.4122
-3.500 -0.1049 0.01178 0.00481 -0.0855 0.5288 0.4162
-3.250 -0.0722 0.01171 0.00474 -0.0866 0.5269 0.4200
-3.000 -0.0396 0.01164 0.00469 -0.0878 0.5249 0.4243
-2.750 -0.0070 0.01159 0.00465 -0.0888 0.5226 0.4287
-2.500 0.0254 0.01155 0.00459 -0.0899 0.5202 0.4330
-2.250 0.0577 0.01153 0.00453 -0.0909 0.5178 0.4366
-2.000 0.0899 0.01150 0.00450 -0.0919 0.5154 0.4404
-1.750 0.1220 0.01149 0.00449 -0.0928 0.5133 0.4444
-1.500 0.1541 0.01151 0.00449 -0.0937 0.5111 0.4486
-1.250 0.1863 0.01150 0.00448 -0.0947 0.5095 0.4526
-1.000 0.2186 0.01148 0.00446 -0.0956 0.5078 0.4557
-0.750 0.2506 0.01147 0.00449 -0.0965 0.5057 0.4592
-0.500 0.2827 0.01147 0.00452 -0.0974 0.5035 0.4632
-0.250 0.3146 0.01148 0.00453 -0.0982 0.5011 0.4672
0.000 0.3465 0.01149 0.00453 -0.0991 0.4989 0.4708
0.250 0.3783 0.01152 0.00453 -0.0999 0.4969 0.4738
0.500 0.4099 0.01155 0.00458 -0.1007 0.4949 0.4771
0.750 0.4413 0.01160 0.00464 -0.1014 0.4927 0.4807
1.000 0.4727 0.01166 0.00470 -0.1021 0.4904 0.4843
1.250 0.5044 0.01168 0.00475 -0.1029 0.4886 0.4877
1.500 0.5361 0.01171 0.00479 -0.1036 0.4866 0.4907
1.750 0.5677 0.01175 0.00484 -0.1044 0.4846 0.4935
2.000 0.5989 0.01179 0.00493 -0.1050 0.4825 0.4966
2.250 0.6301 0.01185 0.00502 -0.1057 0.4801 0.4998
2.500 0.6612 0.01190 0.00509 -0.1063 0.4777 0.5030
2.750 0.6922 0.01197 0.00515 -0.1069 0.4754 0.5059
3.000 0.7231 0.01205 0.00522 -0.1075 0.4732 0.5087
3.250 0.7539 0.01216 0.00530 -0.1081 0.4710 0.5113
3.500 0.7849 0.01221 0.00542 -0.1087 0.4691 0.5141
3.750 0.8157 0.01227 0.00554 -0.1092 0.4667 0.5169
4.000 0.8464 0.01234 0.00567 -0.1098 0.4644 0.5197
4.250 0.8769 0.01242 0.00578 -0.1103 0.4619 0.5223
4.500 0.9074 0.01250 0.00589 -0.1108 0.4592 0.5250
4.750 0.9376 0.01260 0.00598 -0.1112 0.4566 0.5278
5.000 0.9677 0.01272 0.00608 -0.1117 0.4540 0.5304
5.250 0.9976 0.01283 0.00622 -0.1121 0.4515 0.5328
5.500 1.0277 0.01291 0.00638 -0.1125 0.4489 0.5351
5.750 1.0576 0.01300 0.00655 -0.1128 0.4459 0.5375
6.000 1.0872 0.01311 0.00670 -0.1132 0.4425 0.5401
6.250 1.1165 0.01322 0.00684 -0.1134 0.4390 0.5429
6.500 1.1453 0.01337 0.00697 -0.1136 0.4349 0.5454
6.750 1.1744 0.01348 0.00713 -0.1139 0.4305 0.5477
7.000 1.2035 0.01359 0.00728 -0.1141 0.4255 0.5499
7.250 1.2318 0.01374 0.00743 -0.1142 0.4201 0.5520
7.500 1.2591 0.01391 0.00762 -0.1142 0.4143 0.5545
7.750 1.2871 0.01404 0.00783 -0.1142 0.4074 0.5568
8.000 1.3136 0.01425 0.00804 -0.1140 0.4000 0.5589
8.250 1.3401 0.01446 0.00829 -0.1139 0.3919 0.5611
8.500 1.3645 0.01476 0.00856 -0.1134 0.3809 0.5635
8.750 1.3886 0.01508 0.00887 -0.1128 0.3677 0.5660
9.000 1.4106 0.01549 0.00924 -0.1120 0.3535 0.5683
9.250 1.4306 0.01598 0.00968 -0.1109 0.3390 0.5703
9.500 1.4475 0.01659 0.01022 -0.1094 0.3222 0.5719
9.750 1.4590 0.01738 0.01095 -0.1071 0.3019 0.5740
10.000 1.4598 0.01836 0.01187 -0.1032 0.2818 0.5760
10.250 1.4558 0.01972 0.01317 -0.0991 0.2623 0.5780
10.500 1.4514 0.02160 0.01500 -0.0960 0.2432 0.5798
10.750 1.4460 0.02402 0.01739 -0.0940 0.2254 0.5816
11.000 1.4400 0.02692 0.02026 -0.0927 0.2093 0.5833
11.250 1.4329 0.03011 0.02343 -0.0917 0.1949 0.5850
11.500 1.4245 0.03350 0.02680 -0.0907 0.1820 0.5867
11.750 1.4166 0.03684 0.03015 -0.0898 0.1703 0.5885
12.000 1.4084 0.04021 0.03351 -0.0888 0.1598 0.5901
12.250 1.3997 0.04362 0.03691 -0.0879 0.1502 0.5916
12.500 1.3904 0.04709 0.04038 -0.0870 0.1412 0.5929
12.750 1.3832 0.05039 0.04368 -0.0862 0.1319 0.5943
13.000 1.3778 0.05367 0.04697 -0.0856 0.1236 0.5959
13.250 1.3724 0.05704 0.05036 -0.0851 0.1159 0.5973
13.500 1.3684 0.06030 0.05362 -0.0847 0.1082 0.5988
13.750 1.3658 0.06351 0.05685 -0.0844 0.1012 0.6003
14.000 1.3645 0.06657 0.05992 -0.0841 0.0948 0.6018
14.250 1.3622 0.06982 0.06317 -0.0839 0.0889 0.6034
14.500 1.3617 0.07289 0.06626 -0.0838 0.0831 0.6052
14.750 1.3617 0.07591 0.06929 -0.0837 0.0777 0.6070
15.000 1.3602 0.07918 0.07256 -0.0837 0.0729 0.6088
15.250 1.3609 0.08217 0.07557 -0.0836 0.0680 0.6105
15.500 1.3610 0.08532 0.07873 -0.0837 0.0638 0.6121
15.750 1.3610 0.08847 0.08189 -0.0838 0.0599 0.6134
16.000 1.3628 0.09139 0.08482 -0.0840 0.0561 0.6146
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