WHITCOMB INTEGRAL SUPERCRITICAL AIRFOIL (whitcomb-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: WHITCOMB INTEGRAL SUPERCRITICAL AIRFOIL (whitcomb-il) Reynolds number: 500,000 Max Cl/Cd: 49.1 at α=6° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-whitcomb-il-500000.txt Download as CSV file: xf-whitcomb-il-500000.csv |
XFOIL Version 6.96
Calculated polar for: WHITCOMB INTEGRAL SUPERCRITICAL AIRFOIL
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.500 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-15.750 -0.9131 0.09182 0.08851 -0.0492 1.0000 0.0269
-15.500 -0.9522 0.08051 0.07699 -0.0565 1.0000 0.0268
-15.250 -0.9845 0.07177 0.06804 -0.0615 1.0000 0.0267
-15.000 -1.0103 0.06517 0.06125 -0.0647 1.0000 0.0267
-14.750 -1.0325 0.05995 0.05586 -0.0664 1.0000 0.0267
-14.500 -1.0518 0.05572 0.05145 -0.0670 1.0000 0.0268
-14.250 -1.0681 0.05225 0.04781 -0.0668 1.0000 0.0268
-14.000 -1.0844 0.04897 0.04437 -0.0659 1.0000 0.0269
-13.750 -1.0999 0.04559 0.04083 -0.0645 1.0000 0.0271
-13.500 -1.1085 0.04304 0.03816 -0.0627 1.0000 0.0273
-13.250 -1.1134 0.04103 0.03606 -0.0607 1.0000 0.0274
-13.000 -1.1172 0.03929 0.03425 -0.0585 1.0000 0.0276
-12.750 -1.1209 0.03779 0.03267 -0.0559 1.0000 0.0277
-12.500 -1.1263 0.03646 0.03126 -0.0528 1.0000 0.0279
-12.250 -1.1331 0.03527 0.03001 -0.0492 1.0000 0.0280
-12.000 -1.1304 0.03393 0.02858 -0.0473 1.0000 0.0282
-11.750 -1.1234 0.03257 0.02713 -0.0460 1.0000 0.0285
-11.500 -1.1133 0.03122 0.02568 -0.0450 1.0000 0.0288
-11.250 -1.1004 0.02992 0.02428 -0.0444 1.0000 0.0292
-11.000 -1.0852 0.02868 0.02294 -0.0439 1.0000 0.0296
-10.750 -1.0682 0.02750 0.02164 -0.0436 1.0000 0.0300
-10.500 -1.0495 0.02639 0.02042 -0.0434 1.0000 0.0305
-10.250 -1.0292 0.02541 0.01931 -0.0433 1.0000 0.0309
-10.000 -1.0072 0.02458 0.01835 -0.0434 1.0000 0.0313
-9.750 -0.9894 0.02316 0.01692 -0.0425 1.0000 0.0320
-9.500 -0.9666 0.02237 0.01614 -0.0426 1.0000 0.0328
-9.250 -0.9425 0.02170 0.01544 -0.0428 1.0000 0.0336
-9.000 -0.9178 0.02105 0.01475 -0.0431 1.0000 0.0345
-8.750 -0.8927 0.02041 0.01404 -0.0434 1.0000 0.0354
-8.500 -0.8667 0.01988 0.01343 -0.0437 1.0000 0.0362
-8.250 -0.8414 0.01883 0.01240 -0.0441 1.0000 0.0375
-8.000 -0.8142 0.01827 0.01185 -0.0448 1.0000 0.0388
-7.750 -0.7865 0.01777 0.01133 -0.0454 1.0000 0.0402
-7.500 -0.7585 0.01736 0.01085 -0.0460 1.0000 0.0417
-7.250 -0.7283 0.01657 0.01010 -0.0474 1.0000 0.0438
-7.000 -0.6991 0.01618 0.00972 -0.0482 1.0000 0.0460
-6.750 -0.6701 0.01589 0.00938 -0.0489 1.0000 0.0481
-6.500 -0.6376 0.01526 0.00881 -0.0506 1.0000 0.0513
-6.250 -0.6074 0.01495 0.00850 -0.0516 1.0000 0.0542
-6.000 -0.5751 0.01451 0.00807 -0.0531 1.0000 0.0578
-5.750 -0.5440 0.01423 0.00782 -0.0542 1.0000 0.0619
-5.500 -0.5115 0.01389 0.00751 -0.0557 1.0000 0.0671
-5.250 -0.4804 0.01367 0.00731 -0.0568 1.0000 0.0731
-5.000 -0.4468 0.01334 0.00706 -0.0585 1.0000 0.0827
-4.750 -0.4132 0.01305 0.00685 -0.0601 1.0000 0.0957
-4.500 -0.3784 0.01274 0.00666 -0.0621 1.0000 0.1140
-4.250 -0.3433 0.01246 0.00652 -0.0641 1.0000 0.1386
-4.000 -0.3067 0.01215 0.00639 -0.0665 1.0000 0.1729
-3.750 -0.2679 0.01181 0.00627 -0.0694 1.0000 0.2180
-3.500 -0.2234 0.01133 0.00611 -0.0738 1.0000 0.2886
-3.250 -0.1388 0.00983 0.00570 -0.0877 1.0000 0.5377
-3.000 -0.1243 0.01043 0.00665 -0.0843 1.0000 0.6148
-2.750 -0.0973 0.01068 0.00682 -0.0841 1.0000 0.6393
-2.500 -0.0787 0.01116 0.00732 -0.0819 1.0000 0.6487
-2.250 -0.0565 0.01164 0.00780 -0.0804 0.9995 0.6584
-2.000 -0.0183 0.01225 0.00843 -0.0818 0.9955 0.6660
-1.750 0.0244 0.01254 0.00869 -0.0845 0.9909 0.6725
-1.500 0.0754 0.01290 0.00910 -0.0882 0.9844 0.6755
-1.250 0.1178 0.01297 0.00922 -0.0902 0.9751 0.6792
-1.000 0.1628 0.01299 0.00921 -0.0931 0.9684 0.6877
-0.750 0.2021 0.01286 0.00915 -0.0944 0.9621 0.6896
-0.500 0.2273 0.01297 0.00932 -0.0927 0.9555 0.6919
-0.250 0.2603 0.01297 0.00939 -0.0923 0.9492 0.6954
0.000 0.3061 0.01254 0.00893 -0.0956 0.9389 0.7039
0.250 0.3389 0.01220 0.00868 -0.0950 0.9311 0.7059
0.500 0.3620 0.01196 0.00849 -0.0927 0.9181 0.7077
0.750 0.3787 0.01186 0.00843 -0.0895 0.8956 0.7100
1.000 0.4455 0.01261 0.00781 -0.0962 0.5812 0.7114
1.250 0.4608 0.01359 0.00805 -0.0939 0.4166 0.7143
1.500 0.4936 0.01420 0.00808 -0.0960 0.3014 0.7187
1.750 0.5208 0.01458 0.00810 -0.0962 0.2222 0.7207
2.000 0.5441 0.01490 0.00820 -0.0952 0.1726 0.7215
2.250 0.5690 0.01520 0.00831 -0.0946 0.1335 0.7222
2.500 0.5937 0.01550 0.00847 -0.0938 0.1061 0.7231
2.750 0.6189 0.01582 0.00866 -0.0932 0.0879 0.7241
3.000 0.6456 0.01608 0.00885 -0.0929 0.0761 0.7251
3.250 0.6737 0.01627 0.00901 -0.0929 0.0690 0.7260
3.500 0.7018 0.01654 0.00924 -0.0930 0.0633 0.7269
3.750 0.7297 0.01679 0.00946 -0.0930 0.0588 0.7282
4.000 0.7579 0.01710 0.00976 -0.0932 0.0550 0.7295
4.250 0.7873 0.01733 0.00997 -0.0936 0.0519 0.7305
4.500 0.8153 0.01782 0.01041 -0.0938 0.0490 0.7314
4.750 0.8450 0.01805 0.01067 -0.0943 0.0469 0.7322
5.000 0.8746 0.01836 0.01095 -0.0948 0.0447 0.7335
5.250 0.9024 0.01902 0.01157 -0.0950 0.0425 0.7346
5.500 0.9319 0.01932 0.01190 -0.0954 0.0410 0.7352
5.750 0.9604 0.01972 0.01231 -0.0957 0.0396 0.7358
6.000 0.9878 0.02012 0.01269 -0.0957 0.0383 0.7363
6.250 1.0120 0.02106 0.01362 -0.0951 0.0369 0.7367
6.500 1.0382 0.02141 0.01406 -0.0947 0.0362 0.7374
6.750 1.0636 0.02193 0.01464 -0.0942 0.0354 0.7381
7.000 1.0890 0.02248 0.01526 -0.0936 0.0345 0.7386
7.250 1.1145 0.02300 0.01580 -0.0932 0.0336 0.7390
7.500 1.1395 0.02357 0.01638 -0.0928 0.0328 0.7394
7.750 1.1631 0.02495 0.01778 -0.0923 0.0320 0.7398
8.000 1.1878 0.02566 0.01861 -0.0917 0.0315 0.7402
8.250 1.2120 0.02645 0.01953 -0.0910 0.0310 0.7406
8.500 1.2356 0.02738 0.02060 -0.0903 0.0305 0.7411
8.750 1.2585 0.02838 0.02173 -0.0895 0.0300 0.7415
9.000 1.2807 0.02939 0.02286 -0.0886 0.0295 0.7420
9.250 1.3019 0.03043 0.02401 -0.0876 0.0291 0.7427
9.500 1.3224 0.03152 0.02522 -0.0864 0.0287 0.7434
9.750 1.3423 0.03264 0.02644 -0.0853 0.0284 0.7438
10.000 1.3612 0.03393 0.02784 -0.0841 0.0281 0.7442
10.250 1.3781 0.03558 0.02960 -0.0827 0.0278 0.7446
10.500 1.3894 0.03830 0.03253 -0.0807 0.0275 0.7449
10.750 1.3961 0.04069 0.03523 -0.0779 0.0273 0.7453
11.000 1.4020 0.04256 0.03740 -0.0749 0.0271 0.7456
11.250 1.4023 0.04498 0.04014 -0.0714 0.0268 0.7460
11.500 1.3948 0.04795 0.04343 -0.0672 0.0267 0.7463
11.750 1.3762 0.05089 0.04666 -0.0615 0.0266 0.7465
12.000 1.3544 0.05449 0.05054 -0.0566 0.0266 0.7467
12.250 1.3264 0.05885 0.05519 -0.0524 0.0266 0.7469
12.500 1.2949 0.06407 0.06069 -0.0499 0.0266 0.7471
12.750 1.2588 0.07077 0.06765 -0.0500 0.0267 0.7473
13.000 1.2199 0.07982 0.07695 -0.0546 0.0269 0.7475
13.250 1.1694 0.09579 0.09317 -0.0681 0.0271 0.7475
13.500 0.9198 0.18044 0.17810 -0.1210 0.0332 0.7452
13.750 0.9279 0.18345 0.18111 -0.1224 0.0328 0.7454
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