GOE 776 AIRFOIL (goe776-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: GOE 776 AIRFOIL (goe776-il) Reynolds number: 1,000,000 Max Cl/Cd: 66.32 at α=9.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-goe776-il-1000000.txt Download as CSV file: xf-goe776-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: GOE 776 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 = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -1.2945 0.07811 0.07350 -0.0449 1.0000 0.0900
-19.500 -1.2920 0.07549 0.07082 -0.0455 1.0000 0.0914
-19.250 -1.3006 0.07166 0.06694 -0.0463 1.0000 0.0931
-19.000 -1.3073 0.06803 0.06328 -0.0469 1.0000 0.0949
-18.750 -1.3079 0.06515 0.06035 -0.0474 1.0000 0.0966
-18.500 -1.3075 0.06237 0.05752 -0.0479 1.0000 0.0982
-18.250 -1.3020 0.06018 0.05527 -0.0482 1.0000 0.0994
-18.000 -1.3078 0.05684 0.05190 -0.0485 1.0000 0.1013
-17.750 -1.3104 0.05385 0.04887 -0.0488 1.0000 0.1030
-17.500 -1.3082 0.05140 0.04639 -0.0489 1.0000 0.1048
-17.250 -1.3042 0.04916 0.04410 -0.0490 1.0000 0.1065
-17.000 -1.2963 0.04733 0.04221 -0.0491 1.0000 0.1079
-16.750 -1.2972 0.04470 0.03955 -0.0489 1.0000 0.1100
-16.500 -1.2956 0.04233 0.03716 -0.0488 1.0000 0.1120
-16.250 -1.2900 0.04038 0.03519 -0.0486 1.0000 0.1140
-16.000 -1.2821 0.03866 0.03343 -0.0484 1.0000 0.1158
-15.750 -1.2727 0.03712 0.03184 -0.0481 1.0000 0.1174
-15.500 -1.2696 0.03509 0.02980 -0.0475 1.0000 0.1199
-15.250 -1.2638 0.03333 0.02802 -0.0470 1.0000 0.1222
-15.000 -1.2547 0.03189 0.02657 -0.0464 1.0000 0.1244
-14.750 -1.2438 0.03066 0.02530 -0.0458 1.0000 0.1263
-14.500 -1.2369 0.02920 0.02382 -0.0449 1.0000 0.1287
-14.250 -1.2304 0.02783 0.02245 -0.0437 1.0000 0.1314
-14.000 -1.2232 0.02665 0.02126 -0.0423 1.0000 0.1340
-13.750 -1.2150 0.02574 0.02033 -0.0406 1.0000 0.1363
-13.500 -1.2116 0.02477 0.01934 -0.0383 1.0000 0.1386
-13.250 -1.2140 0.02378 0.01835 -0.0349 1.0000 0.1413
-13.000 -1.2178 0.02303 0.01759 -0.0309 1.0000 0.1438
-12.750 -1.1929 0.02215 0.01670 -0.0320 0.9986 0.1472
-12.500 -1.1686 0.02119 0.01575 -0.0331 0.9966 0.1513
-12.250 -1.1437 0.02027 0.01485 -0.0343 0.9946 0.1556
-12.000 -1.1146 0.01960 0.01417 -0.0358 0.9930 0.1595
-11.750 -1.0884 0.01870 0.01331 -0.0372 0.9915 0.1647
-11.500 -1.0609 0.01799 0.01261 -0.0384 0.9895 0.1694
-11.250 -1.0349 0.01737 0.01199 -0.0391 0.9851 0.1739
-11.000 -1.0106 0.01664 0.01130 -0.0396 0.9802 0.1794
-10.750 -0.9831 0.01611 0.01077 -0.0404 0.9758 0.1842
-10.500 -0.9666 0.01555 0.01022 -0.0390 0.9659 0.1891
-10.250 -0.9486 0.01501 0.00969 -0.0379 0.9572 0.1945
-10.000 -0.9304 0.01465 0.00930 -0.0365 0.9464 0.1988
-9.750 -0.9151 0.01414 0.00880 -0.0347 0.9356 0.2046
-9.500 -0.8978 0.01374 0.00838 -0.0331 0.9239 0.2099
-9.250 -0.8772 0.01344 0.00806 -0.0320 0.9127 0.2143
-9.000 -0.8603 0.01302 0.00763 -0.0304 0.9003 0.2204
-8.750 -0.8400 0.01271 0.00731 -0.0293 0.8885 0.2258
-8.500 -0.8187 0.01246 0.00701 -0.0282 0.8764 0.2307
-8.250 -0.7991 0.01212 0.00668 -0.0270 0.8637 0.2371
-8.000 -0.7774 0.01188 0.00640 -0.0260 0.8513 0.2426
-7.750 -0.7554 0.01165 0.00614 -0.0251 0.8380 0.2480
-7.500 -0.7345 0.01139 0.00588 -0.0240 0.8254 0.2546
-7.250 -0.7116 0.01122 0.00565 -0.0232 0.8114 0.2603
-7.000 -0.6894 0.01100 0.00542 -0.0222 0.7986 0.2664
-6.750 -0.6674 0.01081 0.00520 -0.0212 0.7846 0.2728
-6.500 -0.6432 0.01067 0.00503 -0.0206 0.7717 0.2782
-6.250 -0.6216 0.01048 0.00482 -0.0194 0.7585 0.2851
-6.000 -0.5987 0.01032 0.00465 -0.0185 0.7452 0.2918
-5.750 -0.5744 0.01024 0.00452 -0.0179 0.7325 0.2968
-5.500 -0.5540 0.01009 0.00435 -0.0164 0.7195 0.3040
-5.250 -0.5326 0.00999 0.00424 -0.0152 0.7077 0.3106
-5.000 -0.5096 0.00995 0.00415 -0.0141 0.6950 0.3158
-4.750 -0.4889 0.00982 0.00403 -0.0127 0.6841 0.3235
-4.500 -0.4649 0.00974 0.00393 -0.0119 0.6726 0.3301
-4.250 -0.4402 0.00969 0.00384 -0.0113 0.6616 0.3361
-4.000 -0.4170 0.00957 0.00374 -0.0104 0.6506 0.3443
-3.750 -0.3923 0.00953 0.00367 -0.0097 0.6400 0.3515
-3.500 -0.3675 0.00944 0.00359 -0.0090 0.6300 0.3589
-3.250 -0.3438 0.00939 0.00351 -0.0082 0.6185 0.3668
-3.000 -0.3172 0.00934 0.00346 -0.0078 0.6096 0.3731
-2.750 -0.2933 0.00927 0.00339 -0.0070 0.5990 0.3813
-2.500 -0.2680 0.00921 0.00333 -0.0064 0.5893 0.3891
-2.250 -0.2417 0.00920 0.00329 -0.0060 0.5787 0.3952
-2.000 -0.2178 0.00914 0.00323 -0.0052 0.5687 0.4041
-1.750 -0.1918 0.00910 0.00319 -0.0048 0.5585 0.4119
-1.500 -0.1668 0.00910 0.00316 -0.0041 0.5473 0.4194
-1.250 -0.1414 0.00903 0.00312 -0.0035 0.5378 0.4285
-1.000 -0.1160 0.00906 0.00310 -0.0030 0.5261 0.4359
-0.750 -0.0906 0.00899 0.00307 -0.0024 0.5167 0.4453
-0.500 -0.0657 0.00901 0.00306 -0.0017 0.5054 0.4545
-0.250 -0.0397 0.00899 0.00304 -0.0013 0.4960 0.4632
0.000 -0.0150 0.00898 0.00303 -0.0006 0.4855 0.4733
0.250 0.0111 0.00900 0.00304 -0.0002 0.4760 0.4821
0.500 0.0357 0.00897 0.00304 0.0006 0.4663 0.4930
0.750 0.0615 0.00902 0.00306 0.0011 0.4569 0.5022
1.000 0.0866 0.00899 0.00306 0.0017 0.4484 0.5137
1.250 0.1115 0.00905 0.00309 0.0023 0.4383 0.5235
1.500 0.1372 0.00903 0.00311 0.0029 0.4312 0.5347
1.750 0.1627 0.00907 0.00315 0.0034 0.4224 0.5450
2.000 0.1874 0.00910 0.00319 0.0041 0.4141 0.5554
2.250 0.2135 0.00912 0.00322 0.0045 0.4069 0.5663
2.500 0.2382 0.00918 0.00327 0.0052 0.3983 0.5759
2.750 0.2635 0.00921 0.00332 0.0058 0.3914 0.5867
3.000 0.2896 0.00926 0.00337 0.0062 0.3841 0.5960
3.250 0.3130 0.00932 0.00344 0.0071 0.3755 0.6070
3.500 0.3394 0.00937 0.00350 0.0075 0.3694 0.6165
3.750 0.3639 0.00941 0.00357 0.0082 0.3619 0.6274
4.000 0.3876 0.00952 0.00366 0.0091 0.3536 0.6379
4.250 0.4132 0.00955 0.00372 0.0096 0.3474 0.6480
4.500 0.4369 0.00964 0.00381 0.0104 0.3397 0.6593
4.750 0.4609 0.00973 0.00391 0.0112 0.3325 0.6699
5.000 0.4852 0.00979 0.00400 0.0119 0.3263 0.6818
5.250 0.5073 0.00990 0.00411 0.0131 0.3192 0.6924
5.500 0.5288 0.00997 0.00422 0.0143 0.3131 0.7052
5.750 0.5511 0.01005 0.00432 0.0154 0.3068 0.7168
6.000 0.5715 0.01019 0.00447 0.0169 0.2998 0.7300
6.250 0.5950 0.01030 0.00462 0.0177 0.2942 0.7424
6.500 0.6185 0.01043 0.00478 0.0185 0.2880 0.7561
6.750 0.6399 0.01063 0.00499 0.0196 0.2807 0.7690
7.000 0.6638 0.01077 0.00516 0.0203 0.2753 0.7826
7.250 0.6866 0.01093 0.00537 0.0212 0.2691 0.7962
7.750 0.7314 0.01134 0.00582 0.0230 0.2571 0.8229
8.000 0.7531 0.01158 0.00607 0.0240 0.2507 0.8357
8.250 0.7739 0.01184 0.00636 0.0251 0.2445 0.8493
8.500 0.7966 0.01205 0.00661 0.0259 0.2395 0.8614
8.750 0.8168 0.01236 0.00692 0.0271 0.2334 0.8744
9.000 0.8370 0.01266 0.00725 0.0283 0.2277 0.8864
9.250 0.8582 0.01294 0.00755 0.0292 0.2226 0.8984
9.500 0.8760 0.01332 0.00795 0.0308 0.2168 0.9105
9.750 0.8954 0.01367 0.00831 0.0320 0.2117 0.9222
10.000 0.9137 0.01403 0.00870 0.0334 0.2067 0.9336
10.250 0.9293 0.01452 0.00918 0.0352 0.2010 0.9446
10.500 0.9471 0.01492 0.00959 0.0366 0.1965 0.9555
10.750 0.9654 0.01540 0.01007 0.0378 0.1914 0.9644
11.000 0.9808 0.01602 0.01067 0.0393 0.1858 0.9746
11.250 1.0080 0.01650 0.01116 0.0387 0.1816 0.9795
11.500 1.0333 0.01715 0.01179 0.0381 0.1764 0.9844
11.750 1.0579 0.01786 0.01248 0.0375 0.1714 0.9891
12.000 1.0862 0.01849 0.01311 0.0362 0.1670 0.9914
12.250 1.1132 0.01934 0.01392 0.0348 0.1619 0.9928
12.500 1.1414 0.02007 0.01465 0.0334 0.1577 0.9945
12.750 1.1679 0.02090 0.01547 0.0321 0.1535 0.9964
13.000 1.1909 0.02194 0.01649 0.0310 0.1489 0.9984
13.250 1.2176 0.02277 0.01733 0.0297 0.1456 1.0000
13.500 1.2153 0.02347 0.01805 0.0335 0.1432 1.0000
13.750 1.2140 0.02438 0.01896 0.0368 0.1405 1.0000
14.000 1.2143 0.02550 0.02008 0.0395 0.1375 1.0000
14.250 1.2234 0.02636 0.02096 0.0411 0.1355 1.0000
14.500 1.2322 0.02743 0.02205 0.0424 0.1330 1.0000
14.750 1.2401 0.02870 0.02332 0.0435 0.1303 1.0000
15.000 1.2448 0.03031 0.02493 0.0445 0.1274 1.0000
15.250 1.2566 0.03148 0.02614 0.0451 0.1255 1.0000
15.500 1.2661 0.03288 0.02757 0.0457 0.1233 1.0000
15.750 1.2736 0.03449 0.02919 0.0462 0.1210 1.0000
16.000 1.2782 0.03638 0.03110 0.0467 0.1185 1.0000
16.250 1.2845 0.03821 0.03296 0.0470 0.1166 1.0000
16.500 1.2939 0.03978 0.03457 0.0472 0.1148 1.0000
16.750 1.2995 0.04173 0.03656 0.0474 0.1128 1.0000
17.000 1.3025 0.04396 0.03880 0.0476 0.1108 1.0000
17.250 1.3024 0.04651 0.04137 0.0477 0.1086 1.0000
17.500 1.3082 0.04856 0.04348 0.0477 0.1070 1.0000
17.750 1.3139 0.05062 0.04558 0.0476 0.1053 1.0000
18.000 1.3154 0.05314 0.04814 0.0475 0.1035 1.0000
18.250 1.3137 0.05604 0.05107 0.0472 0.1017 1.0000
18.500 1.3085 0.05929 0.05436 0.0469 0.0998 1.0000
18.750 1.3127 0.06163 0.05676 0.0466 0.0985 1.0000
19.000 1.3147 0.06423 0.05942 0.0462 0.0969 1.0000
19.250 1.3131 0.06725 0.06247 0.0457 0.0952 1.0000
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