AH 93-W-257 (ah93w257-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: AH 93-W-257 (ah93w257-il) Reynolds number: 1,000,000 Max Cl/Cd: 114.17 at α=7.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-ah93w257-il-1000000-n5.txt Download as CSV file: xf-ah93w257-il-1000000-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 = 1.000 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.250 -1.1189 0.10123 0.09687 -0.0219 1.0000 0.0650
-19.000 -1.1200 0.09787 0.09348 -0.0231 1.0000 0.0663
-18.750 -1.1167 0.09512 0.09072 -0.0241 1.0000 0.0677
-18.500 -1.1129 0.09246 0.08802 -0.0250 1.0000 0.0693
-18.250 -1.1104 0.08962 0.08515 -0.0260 1.0000 0.0705
-18.000 -1.1079 0.08685 0.08236 -0.0269 1.0000 0.0722
-17.500 -1.1023 0.08160 0.07646 -0.0288 0.7804 0.0756
-17.250 -1.0965 0.07934 0.07408 -0.0295 0.7568 0.0772
-17.000 -1.0925 0.07684 0.07149 -0.0302 0.7386 0.0789
-16.750 -1.0917 0.07398 0.06856 -0.0310 0.7234 0.0810
-16.500 -1.0869 0.07159 0.06611 -0.0317 0.7107 0.0833
-16.250 -1.0826 0.06915 0.06358 -0.0324 0.6984 0.0854
-16.000 -1.0793 0.06665 0.06103 -0.0330 0.6887 0.0878
-15.750 -1.0752 0.06423 0.05858 -0.0336 0.6788 0.0906
-15.500 -1.0713 0.06180 0.05607 -0.0343 0.6692 0.0932
-15.250 -1.0658 0.05959 0.05383 -0.0348 0.6616 0.0961
-15.000 -1.0627 0.05714 0.05135 -0.0353 0.6536 0.0995
-14.750 -1.0567 0.05500 0.04914 -0.0358 0.6457 0.1028
-14.500 -1.0517 0.05279 0.04692 -0.0363 0.6406 0.1065
-14.250 -1.0484 0.05043 0.04453 -0.0367 0.6354 0.1105
-14.000 -1.0413 0.04846 0.04254 -0.0371 0.6299 0.1147
-13.750 -1.0375 0.04621 0.04028 -0.0375 0.6245 0.1199
-13.500 -1.0320 0.04413 0.03818 -0.0378 0.6201 0.1250
-13.250 -1.0274 0.04202 0.03608 -0.0381 0.6165 0.1315
-13.000 -1.0242 0.03976 0.03383 -0.0384 0.6126 0.1382
-12.750 -1.0182 0.03784 0.03191 -0.0386 0.6084 0.1462
-12.500 -1.0165 0.03552 0.02961 -0.0389 0.6041 0.1547
-12.000 -1.0046 0.03175 0.02586 -0.0393 0.5961 0.1716
-11.750 -0.9988 0.02991 0.02405 -0.0394 0.5929 0.1802
-11.500 -0.9901 0.02829 0.02243 -0.0396 0.5894 0.1877
-11.250 -0.9826 0.02663 0.02079 -0.0397 0.5860 0.1960
-11.000 -0.9735 0.02515 0.01931 -0.0397 0.5826 0.2033
-10.750 -0.9656 0.02362 0.01779 -0.0397 0.5791 0.2115
-10.250 -0.9479 0.02095 0.01514 -0.0395 0.5736 0.2255
-10.000 -0.9287 0.01990 0.01408 -0.0406 0.5713 0.2319
-9.750 -0.9084 0.01865 0.01285 -0.0424 0.5686 0.2396
-9.500 -0.8833 0.01775 0.01194 -0.0442 0.5654 0.2467
-9.250 -0.8568 0.01663 0.01083 -0.0468 0.5620 0.2556
-9.000 -0.8273 0.01593 0.01011 -0.0489 0.5585 0.2623
-8.750 -0.7962 0.01499 0.00917 -0.0519 0.5551 0.2709
-8.500 -0.7640 0.01442 0.00858 -0.0543 0.5525 0.2779
-8.250 -0.7295 0.01359 0.00778 -0.0576 0.5507 0.2869
-8.000 -0.6955 0.01309 0.00727 -0.0600 0.5487 0.2944
-7.750 -0.6586 0.01232 0.00653 -0.0637 0.5464 0.3067
-7.500 -0.6216 0.01170 0.00593 -0.0669 0.5438 0.3189
-7.250 -0.5869 0.01138 0.00559 -0.0691 0.5409 0.3268
-7.000 -0.5530 0.01114 0.00532 -0.0709 0.5379 0.3316
-6.750 -0.5190 0.01089 0.00506 -0.0728 0.5347 0.3371
-6.500 -0.4858 0.01074 0.00488 -0.0742 0.5318 0.3418
-6.250 -0.4528 0.01061 0.00473 -0.0756 0.5304 0.3454
-6.000 -0.4192 0.01042 0.00454 -0.0771 0.5288 0.3500
-5.750 -0.3857 0.01025 0.00438 -0.0786 0.5270 0.3547
-5.500 -0.3526 0.01013 0.00425 -0.0799 0.5249 0.3588
-5.250 -0.3198 0.01004 0.00413 -0.0811 0.5225 0.3625
-5.000 -0.2868 0.00994 0.00401 -0.0824 0.5199 0.3665
-4.750 -0.2537 0.00982 0.00388 -0.0837 0.5173 0.3709
-4.500 -0.2209 0.00974 0.00379 -0.0849 0.5149 0.3749
-4.250 -0.1883 0.00968 0.00371 -0.0860 0.5123 0.3789
-4.000 -0.1558 0.00964 0.00364 -0.0870 0.5103 0.3821
-3.750 -0.1227 0.00953 0.00355 -0.0883 0.5090 0.3867
-3.500 -0.0898 0.00945 0.00348 -0.0894 0.5074 0.3907
-3.250 -0.0571 0.00939 0.00341 -0.0905 0.5053 0.3948
-3.000 -0.0247 0.00935 0.00336 -0.0915 0.5031 0.3985
-2.750 0.0079 0.00930 0.00331 -0.0925 0.5009 0.4022
-2.500 0.0406 0.00924 0.00325 -0.0936 0.4988 0.4067
-2.250 0.0730 0.00920 0.00321 -0.0946 0.4967 0.4113
-2.000 0.1053 0.00919 0.00319 -0.0955 0.4944 0.4153
-1.750 0.1373 0.00920 0.00317 -0.0964 0.4919 0.4187
-1.500 0.1699 0.00915 0.00314 -0.0974 0.4900 0.4234
-1.250 0.2023 0.00911 0.00312 -0.0984 0.4885 0.4276
-1.000 0.2346 0.00909 0.00311 -0.0993 0.4867 0.4316
-0.750 0.2667 0.00909 0.00311 -0.1002 0.4849 0.4353
-0.500 0.2989 0.00908 0.00311 -0.1011 0.4830 0.4390
-0.250 0.3311 0.00906 0.00311 -0.1019 0.4810 0.4431
0.000 0.3631 0.00907 0.00312 -0.1028 0.4787 0.4469
0.250 0.3949 0.00909 0.00313 -0.1036 0.4763 0.4509
0.500 0.4265 0.00912 0.00315 -0.1043 0.4737 0.4542
0.750 0.4582 0.00916 0.00318 -0.1051 0.4712 0.4579
1.000 0.4903 0.00915 0.00321 -0.1059 0.4700 0.4616
1.250 0.5222 0.00916 0.00324 -0.1067 0.4685 0.4654
1.500 0.5539 0.00918 0.00328 -0.1074 0.4666 0.4692
1.750 0.5855 0.00921 0.00331 -0.1081 0.4643 0.4723
2.000 0.6171 0.00924 0.00335 -0.1088 0.4620 0.4751
2.250 0.6486 0.00927 0.00340 -0.1095 0.4599 0.4785
2.500 0.6800 0.00931 0.00346 -0.1102 0.4575 0.4818
2.750 0.7111 0.00938 0.00352 -0.1108 0.4548 0.4853
3.000 0.7421 0.00945 0.00359 -0.1114 0.4520 0.4886
3.250 0.7734 0.00949 0.00365 -0.1120 0.4505 0.4912
3.500 0.8047 0.00953 0.00372 -0.1126 0.4486 0.4933
3.750 0.8360 0.00957 0.00379 -0.1133 0.4463 0.4964
4.000 0.8671 0.00962 0.00387 -0.1139 0.4436 0.4993
4.250 0.8980 0.00968 0.00395 -0.1144 0.4409 0.5024
4.500 0.9285 0.00977 0.00404 -0.1149 0.4379 0.5055
4.750 0.9589 0.00987 0.00414 -0.1153 0.4347 0.5081
5.000 0.9895 0.00995 0.00424 -0.1158 0.4322 0.5102
5.250 1.0202 0.01001 0.00432 -0.1163 0.4295 0.5118
5.500 1.0508 0.01008 0.00442 -0.1168 0.4259 0.5147
5.750 1.0809 0.01018 0.00454 -0.1172 0.4210 0.5178
6.000 1.1102 0.01033 0.00467 -0.1175 0.4152 0.5206
6.250 1.1405 0.01040 0.00479 -0.1179 0.4110 0.5232
6.500 1.1702 0.01052 0.00491 -0.1183 0.4054 0.5255
6.750 1.1987 0.01072 0.00508 -0.1184 0.3976 0.5279
7.000 1.2281 0.01084 0.00522 -0.1187 0.3906 0.5300
7.250 1.2562 0.01106 0.00540 -0.1187 0.3817 0.5315
7.500 1.2844 0.01125 0.00559 -0.1189 0.3719 0.5341
7.750 1.3107 0.01157 0.00586 -0.1187 0.3571 0.5366
8.000 1.3355 0.01198 0.00619 -0.1183 0.3380 0.5391
8.250 1.3589 0.01247 0.00659 -0.1177 0.3177 0.5417
8.500 1.3804 0.01305 0.00707 -0.1169 0.2961 0.5440
8.750 1.3975 0.01387 0.00773 -0.1154 0.2669 0.5459
9.000 1.4108 0.01482 0.00851 -0.1134 0.2372 0.5477
9.250 1.4213 0.01581 0.00935 -0.1110 0.2116 0.5493
9.500 1.4312 0.01670 0.01014 -0.1084 0.1924 0.5508
9.750 1.4323 0.01758 0.01098 -0.1044 0.1780 0.5525
10.000 1.4355 0.01873 0.01209 -0.1012 0.1641 0.5549
10.250 1.4379 0.02018 0.01352 -0.0987 0.1512 0.5569
10.500 1.4394 0.02206 0.01537 -0.0969 0.1395 0.5588
10.750 1.4409 0.02429 0.01761 -0.0958 0.1288 0.5609
11.000 1.4424 0.02672 0.02003 -0.0950 0.1195 0.5630
11.250 1.4436 0.02925 0.02257 -0.0943 0.1111 0.5649
11.500 1.4432 0.03194 0.02528 -0.0936 0.1037 0.5667
11.750 1.4404 0.03485 0.02819 -0.0927 0.0967 0.5681
12.000 1.4368 0.03782 0.03117 -0.0919 0.0902 0.5694
12.250 1.4345 0.04061 0.03398 -0.0910 0.0843 0.5706
12.500 1.4300 0.04365 0.03702 -0.0902 0.0787 0.5716
12.750 1.4249 0.04673 0.04012 -0.0893 0.0738 0.5730
13.000 1.4234 0.04949 0.04291 -0.0886 0.0690 0.5752
13.250 1.4212 0.05249 0.04594 -0.0881 0.0648 0.5771
13.500 1.4203 0.05536 0.04884 -0.0876 0.0608 0.5790
13.750 1.4205 0.05820 0.05171 -0.0872 0.0574 0.5806
14.000 1.4214 0.06097 0.05450 -0.0868 0.0539 0.5823
14.250 1.4216 0.06391 0.05747 -0.0865 0.0509 0.5838
14.500 1.4233 0.06663 0.06020 -0.0862 0.0480 0.5854
14.750 1.4236 0.06959 0.06319 -0.0860 0.0451 0.5869
15.000 1.4252 0.07242 0.06604 -0.0859 0.0426 0.5884
15.250 1.4275 0.07515 0.06879 -0.0857 0.0400 0.5898
15.500 1.4276 0.07820 0.07187 -0.0856 0.0380 0.5911
15.750 1.4301 0.08095 0.07464 -0.0855 0.0359 0.5923
16.000 1.4326 0.08374 0.07745 -0.0855 0.0341 0.5935
16.250 1.4339 0.08674 0.08051 -0.0856 0.0326 0.5956
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