GOE 648 AIRFOIL (goe648-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 648 AIRFOIL (goe648-il) Reynolds number: 1,000,000 Max Cl/Cd: 101.91 at α=6.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe648-il-1000000-n5.txt Download as CSV file: xf-goe648-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: GOE 648 AIRFOIL
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
------ -------- --------- --------- -------- -------- --------
-18.250 -0.8354 0.09913 0.09631 -0.0609 1.0000 0.0149
-18.000 -0.9304 0.08061 0.07753 -0.0721 1.0000 0.0146
-17.750 -1.0244 0.06337 0.05998 -0.0828 1.0000 0.0143
-17.500 -1.0788 0.05212 0.04849 -0.0900 1.0000 0.0142
-17.250 -1.1111 0.04444 0.04063 -0.0950 1.0000 0.0142
-17.000 -1.1307 0.03908 0.03513 -0.0980 1.0000 0.0143
-16.750 -1.1435 0.03508 0.03102 -0.0998 1.0000 0.0144
-16.500 -1.1530 0.03197 0.02780 -0.1004 1.0000 0.0146
-16.250 -1.1610 0.02958 0.02533 -0.0999 1.0000 0.0147
-16.000 -1.1698 0.02770 0.02337 -0.0981 1.0000 0.0149
-15.750 -1.1713 0.02624 0.02182 -0.0966 0.9996 0.0151
-15.500 -1.1543 0.02495 0.02046 -0.0974 0.9979 0.0154
-15.250 -1.1356 0.02390 0.01934 -0.0978 0.9956 0.0157
-15.000 -1.1149 0.02302 0.01838 -0.0981 0.9932 0.0161
-14.750 -1.0993 0.02218 0.01747 -0.0972 0.9899 0.0164
-14.500 -1.0778 0.02131 0.01657 -0.0972 0.9871 0.0169
-14.250 -1.0532 0.02053 0.01575 -0.0975 0.9849 0.0173
-14.000 -1.0265 0.01983 0.01500 -0.0981 0.9832 0.0180
-13.750 -0.9986 0.01918 0.01431 -0.0989 0.9818 0.0184
-13.500 -0.9781 0.01864 0.01372 -0.0980 0.9779 0.0190
-13.250 -0.9540 0.01806 0.01309 -0.0977 0.9748 0.0195
-13.000 -0.9272 0.01747 0.01249 -0.0980 0.9724 0.0201
-12.750 -0.8986 0.01693 0.01191 -0.0986 0.9706 0.0207
-12.500 -0.8684 0.01643 0.01138 -0.0994 0.9691 0.0214
-12.250 -0.8463 0.01601 0.01091 -0.0984 0.9631 0.0219
-12.000 -0.8154 0.01555 0.01041 -0.0993 0.9588 0.0224
-11.500 -0.7504 0.01456 0.00938 -0.1016 0.9484 0.0238
-11.250 -0.7172 0.01416 0.00894 -0.1028 0.9431 0.0247
-11.000 -0.6845 0.01378 0.00851 -0.1039 0.9373 0.0254
-10.750 -0.6546 0.01344 0.00811 -0.1044 0.9288 0.0259
-10.500 -0.6248 0.01303 0.00767 -0.1049 0.9206 0.0267
-10.250 -0.5969 0.01270 0.00730 -0.1049 0.9100 0.0274
-10.000 -0.5701 0.01241 0.00696 -0.1047 0.8997 0.0282
-9.750 -0.5434 0.01217 0.00665 -0.1044 0.8887 0.0290
-9.500 -0.5183 0.01195 0.00636 -0.1037 0.8773 0.0296
-9.250 -0.4940 0.01168 0.00604 -0.1029 0.8666 0.0304
-9.000 -0.4700 0.01145 0.00575 -0.1020 0.8533 0.0313
-8.750 -0.4460 0.01125 0.00549 -0.1011 0.8398 0.0322
-8.500 -0.4218 0.01108 0.00524 -0.1002 0.8275 0.0331
-8.250 -0.3973 0.01092 0.00502 -0.0993 0.8177 0.0338
-8.000 -0.3730 0.01069 0.00476 -0.0985 0.8076 0.0350
-7.750 -0.3487 0.01052 0.00454 -0.0976 0.7972 0.0362
-7.500 -0.3239 0.01036 0.00433 -0.0968 0.7862 0.0374
-7.250 -0.2990 0.01020 0.00413 -0.0959 0.7757 0.0388
-7.000 -0.2745 0.01004 0.00393 -0.0951 0.7643 0.0406
-6.750 -0.2494 0.00989 0.00376 -0.0943 0.7530 0.0425
-6.500 -0.2247 0.00976 0.00358 -0.0934 0.7400 0.0448
-6.250 -0.2003 0.00965 0.00342 -0.0925 0.7240 0.0475
-6.000 -0.1758 0.00956 0.00327 -0.0916 0.7073 0.0502
-5.750 -0.1512 0.00947 0.00314 -0.0907 0.6908 0.0535
-5.500 -0.1270 0.00943 0.00302 -0.0897 0.6698 0.0565
-5.250 -0.1032 0.00940 0.00292 -0.0887 0.6459 0.0601
-5.000 -0.0788 0.00939 0.00282 -0.0878 0.6252 0.0630
-4.750 -0.0541 0.00935 0.00273 -0.0869 0.6075 0.0661
-4.500 -0.0287 0.00933 0.00265 -0.0862 0.5925 0.0687
-4.250 -0.0033 0.00930 0.00256 -0.0855 0.5798 0.0710
-4.000 0.0223 0.00925 0.00247 -0.0848 0.5667 0.0739
-3.750 0.0480 0.00922 0.00240 -0.0841 0.5532 0.0766
-3.500 0.0736 0.00922 0.00234 -0.0834 0.5395 0.0787
-3.250 0.0987 0.00919 0.00226 -0.0827 0.5246 0.0823
-3.000 0.1243 0.00917 0.00220 -0.0820 0.5107 0.0854
-2.750 0.1500 0.00916 0.00215 -0.0813 0.4971 0.0886
-2.500 0.1751 0.00914 0.00210 -0.0806 0.4821 0.0950
-2.250 0.1997 0.00911 0.00205 -0.0798 0.4650 0.1077
-2.000 0.2237 0.00908 0.00202 -0.0789 0.4450 0.1287
-1.750 0.2469 0.00911 0.00201 -0.0778 0.4190 0.1495
-1.500 0.2697 0.00919 0.00202 -0.0767 0.3870 0.1694
-1.250 0.2929 0.00926 0.00204 -0.0757 0.3637 0.1908
-1.000 0.3168 0.00928 0.00207 -0.0748 0.3475 0.2143
-0.750 0.3415 0.00928 0.00209 -0.0740 0.3364 0.2378
-0.500 0.3664 0.00928 0.00211 -0.0732 0.3282 0.2616
-0.250 0.3913 0.00927 0.00214 -0.0725 0.3207 0.2860
0.000 0.4159 0.00928 0.00218 -0.0717 0.3134 0.3105
0.250 0.4409 0.00923 0.00221 -0.0710 0.3087 0.3439
0.500 0.4657 0.00919 0.00224 -0.0703 0.3045 0.3773
0.750 0.4897 0.00914 0.00230 -0.0694 0.2996 0.4221
1.000 0.5133 0.00910 0.00237 -0.0685 0.2945 0.4735
1.250 0.5380 0.00906 0.00244 -0.0677 0.2912 0.5137
1.500 0.5630 0.00908 0.00250 -0.0670 0.2872 0.5382
1.750 0.5875 0.00912 0.00258 -0.0661 0.2829 0.5632
2.000 0.6116 0.00917 0.00266 -0.0653 0.2786 0.5872
2.250 0.6351 0.00914 0.00274 -0.0642 0.2760 0.6268
2.500 0.6579 0.00909 0.00284 -0.0631 0.2735 0.6759
2.750 0.6805 0.00907 0.00294 -0.0619 0.2706 0.7193
3.000 0.7034 0.00910 0.00303 -0.0607 0.2671 0.7526
3.250 0.7260 0.00915 0.00314 -0.0595 0.2640 0.7790
3.500 0.7481 0.00921 0.00324 -0.0582 0.2607 0.8053
3.750 0.7696 0.00920 0.00335 -0.0567 0.2585 0.8402
4.000 0.8050 0.00914 0.00352 -0.0582 0.2553 0.9181
4.250 0.9089 0.00949 0.00384 -0.0749 0.2490 0.9795
4.500 0.9408 0.00971 0.00402 -0.0758 0.2448 0.9994
4.750 0.9657 0.00985 0.00414 -0.0752 0.2420 1.0000
5.000 0.9877 0.00997 0.00426 -0.0739 0.2392 1.0000
5.250 1.0094 0.01010 0.00438 -0.0726 0.2363 1.0000
5.500 1.0307 0.01026 0.00451 -0.0713 0.2331 1.0000
5.750 1.0516 0.01043 0.00466 -0.0699 0.2295 1.0000
6.000 1.0720 0.01059 0.00481 -0.0684 0.2262 1.0000
6.250 1.0918 0.01073 0.00495 -0.0667 0.2226 1.0000
6.500 1.1108 0.01090 0.00509 -0.0650 0.2184 1.0000
6.750 1.1289 0.01112 0.00527 -0.0631 0.2129 1.0000
7.000 1.1486 0.01130 0.00544 -0.0615 0.2083 1.0000
7.250 1.1681 0.01150 0.00563 -0.0599 0.2037 1.0000
7.500 1.1871 0.01174 0.00584 -0.0583 0.1989 1.0000
7.750 1.2068 0.01196 0.00606 -0.0569 0.1946 1.0000
8.000 1.2266 0.01220 0.00628 -0.0554 0.1900 1.0000
8.250 1.2454 0.01248 0.00654 -0.0539 0.1850 1.0000
8.500 1.2651 0.01275 0.00680 -0.0526 0.1811 1.0000
8.750 1.2847 0.01302 0.00707 -0.0512 0.1770 1.0000
9.000 1.3030 0.01336 0.00738 -0.0497 0.1717 1.0000
9.250 1.3218 0.01369 0.00770 -0.0484 0.1672 1.0000
9.500 1.3407 0.01402 0.00803 -0.0470 0.1629 1.0000
9.750 1.3587 0.01440 0.00840 -0.0456 0.1585 1.0000
10.000 1.3767 0.01479 0.00879 -0.0442 0.1548 1.0000
10.250 1.3958 0.01514 0.00915 -0.0431 0.1522 1.0000
10.500 1.4141 0.01553 0.00955 -0.0418 0.1489 1.0000
10.750 1.4316 0.01597 0.00999 -0.0405 0.1459 1.0000
11.000 1.4482 0.01647 0.01049 -0.0391 0.1423 1.0000
11.250 1.4663 0.01689 0.01094 -0.0380 0.1397 1.0000
11.500 1.4833 0.01738 0.01144 -0.0367 0.1363 1.0000
11.750 1.4987 0.01798 0.01204 -0.0354 0.1323 1.0000
12.000 1.5140 0.01860 0.01266 -0.0340 0.1285 1.0000
12.250 1.5303 0.01916 0.01325 -0.0329 0.1258 1.0000
12.500 1.5445 0.01987 0.01396 -0.0316 0.1212 1.0000
12.750 1.5573 0.02068 0.01477 -0.0302 0.1170 1.0000
13.000 1.5697 0.02153 0.01561 -0.0288 0.1107 1.0000
13.250 1.5801 0.02254 0.01661 -0.0273 0.1051 1.0000
13.500 1.5885 0.02371 0.01776 -0.0258 0.0973 1.0000
13.750 1.5976 0.02486 0.01891 -0.0245 0.0915 1.0000
14.000 1.5997 0.02655 0.02056 -0.0227 0.0806 1.0000
14.250 1.5998 0.02847 0.02243 -0.0210 0.0708 1.0000
14.500 1.6001 0.03045 0.02440 -0.0195 0.0638 1.0000
14.750 1.6005 0.03251 0.02648 -0.0183 0.0590 1.0000
15.000 1.6031 0.03448 0.02848 -0.0173 0.0560 1.0000
15.250 1.6048 0.03660 0.03065 -0.0165 0.0537 1.0000
15.500 1.6085 0.03862 0.03272 -0.0159 0.0520 1.0000
15.750 1.6121 0.04073 0.03489 -0.0154 0.0509 1.0000
16.000 1.6117 0.04330 0.03752 -0.0150 0.0492 1.0000
16.250 1.6129 0.04578 0.04006 -0.0148 0.0486 1.0000
16.500 1.6115 0.04860 0.04295 -0.0147 0.0475 1.0000
16.750 1.6107 0.05145 0.04588 -0.0148 0.0467 1.0000
17.000 1.6097 0.05437 0.04888 -0.0149 0.0459 1.0000
17.250 1.6075 0.05748 0.05207 -0.0152 0.0455 1.0000
17.500 1.6027 0.06098 0.05565 -0.0156 0.0448 1.0000
17.750 1.5956 0.06482 0.05959 -0.0162 0.0441 1.0000
18.000 1.5861 0.06903 0.06389 -0.0170 0.0434 1.0000
18.250 1.5759 0.07339 0.06835 -0.0179 0.0430 1.0000
18.500 1.5620 0.07836 0.07341 -0.0191 0.0424 1.0000
18.750 1.5474 0.08351 0.07868 -0.0205 0.0421 1.0000
19.000 1.5294 0.08921 0.08448 -0.0221 0.0415 1.0000
19.250 1.5116 0.09499 0.09037 -0.0238 0.0408 1.0000
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