GOE 217 (MVA MK.12) AIRFOIL (goe217-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 217 (MVA MK.12) AIRFOIL (goe217-il) Reynolds number: 1,000,000 Max Cl/Cd: 119.06 at α=4.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe217-il-1000000-n5.txt Download as CSV file: xf-goe217-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: GOE 217 (MVA MK.12) 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
------ -------- --------- --------- -------- -------- --------
-15.750 -0.6238 0.08635 0.08348 -0.0694 1.0000 0.0218
-15.500 -0.6468 0.07890 0.07587 -0.0743 1.0000 0.0218
-15.250 -0.6610 0.07306 0.06991 -0.0782 1.0000 0.0219
-15.000 -0.6709 0.06810 0.06483 -0.0815 1.0000 0.0219
-14.750 -0.6758 0.06362 0.06025 -0.0848 0.9973 0.0219
-14.500 -0.6711 0.05927 0.05579 -0.0896 0.9770 0.0220
-14.250 -0.6611 0.05538 0.05166 -0.0944 0.9146 0.0220
-14.000 -0.6596 0.05243 0.04851 -0.0962 0.8859 0.0220
-13.750 -0.6562 0.04964 0.04557 -0.0980 0.8648 0.0221
-13.500 -0.6532 0.04692 0.04270 -0.0997 0.8452 0.0222
-13.250 -0.6485 0.04448 0.04012 -0.1012 0.8256 0.0223
-13.000 -0.6404 0.04242 0.03794 -0.1024 0.8055 0.0224
-12.750 -0.6313 0.04048 0.03588 -0.1037 0.7845 0.0225
-12.500 -0.6218 0.03862 0.03391 -0.1049 0.7635 0.0225
-12.250 -0.6121 0.03692 0.03210 -0.1058 0.7445 0.0226
-12.000 -0.6016 0.03525 0.03033 -0.1072 0.7279 0.0226
-11.750 -0.5846 0.03370 0.02869 -0.1091 0.7130 0.0227
-11.500 -0.5652 0.03215 0.02706 -0.1114 0.6993 0.0228
-11.250 -0.5434 0.03069 0.02552 -0.1138 0.6882 0.0228
-11.000 -0.5194 0.02935 0.02411 -0.1163 0.6761 0.0229
-10.750 -0.4939 0.02805 0.02273 -0.1189 0.6652 0.0230
-10.500 -0.4668 0.02688 0.02147 -0.1214 0.6522 0.0231
-10.250 -0.4386 0.02578 0.02030 -0.1238 0.6403 0.0232
-10.000 -0.4094 0.02475 0.01917 -0.1263 0.6266 0.0233
-9.750 -0.3791 0.02378 0.01813 -0.1287 0.6156 0.0234
-9.500 -0.3484 0.02290 0.01717 -0.1310 0.6035 0.0235
-9.250 -0.3168 0.02203 0.01624 -0.1333 0.5933 0.0237
-9.000 -0.2849 0.02124 0.01536 -0.1355 0.5817 0.0238
-8.750 -0.2524 0.02048 0.01455 -0.1377 0.5722 0.0239
-8.500 -0.2196 0.01978 0.01377 -0.1398 0.5611 0.0240
-8.250 -0.1862 0.01909 0.01301 -0.1420 0.5517 0.0242
-8.000 -0.1526 0.01844 0.01228 -0.1441 0.5416 0.0243
-7.750 -0.1188 0.01782 0.01160 -0.1462 0.5333 0.0245
-7.500 -0.0844 0.01720 0.01092 -0.1483 0.5263 0.0246
-7.250 -0.0500 0.01662 0.01028 -0.1504 0.5187 0.0247
-7.000 -0.0154 0.01607 0.00966 -0.1525 0.5123 0.0249
-6.750 0.0193 0.01553 0.00907 -0.1545 0.5068 0.0250
-6.500 0.0539 0.01502 0.00852 -0.1564 0.5008 0.0252
-6.250 0.0882 0.01458 0.00801 -0.1581 0.4945 0.0253
-6.000 0.1225 0.01415 0.00753 -0.1598 0.4897 0.0254
-5.750 0.1563 0.01378 0.00711 -0.1612 0.4847 0.0255
-5.500 0.1896 0.01347 0.00675 -0.1625 0.4791 0.0256
-5.250 0.2241 0.01302 0.00622 -0.1642 0.4733 0.0260
-5.000 0.2574 0.01271 0.00588 -0.1654 0.4693 0.0263
-4.750 0.2901 0.01246 0.00561 -0.1664 0.4658 0.0266
-4.500 0.3225 0.01225 0.00537 -0.1672 0.4619 0.0269
-4.250 0.3546 0.01207 0.00515 -0.1680 0.4578 0.0271
-4.000 0.3866 0.01192 0.00495 -0.1687 0.4536 0.0274
-3.750 0.4183 0.01178 0.00478 -0.1693 0.4494 0.0277
-3.500 0.4502 0.01163 0.00461 -0.1700 0.4471 0.0281
-3.250 0.4819 0.01150 0.00447 -0.1706 0.4443 0.0284
-3.000 0.5134 0.01139 0.00433 -0.1711 0.4410 0.0287
-2.750 0.5447 0.01131 0.00422 -0.1716 0.4375 0.0290
-2.500 0.5757 0.01126 0.00413 -0.1720 0.4336 0.0293
-2.250 0.6069 0.01119 0.00402 -0.1725 0.4297 0.0298
-2.000 0.6382 0.01110 0.00393 -0.1729 0.4276 0.0303
-1.750 0.6693 0.01103 0.00386 -0.1733 0.4255 0.0310
-1.500 0.7003 0.01098 0.00381 -0.1737 0.4232 0.0316
-1.250 0.7310 0.01095 0.00377 -0.1741 0.4207 0.0324
-1.000 0.7616 0.01094 0.00374 -0.1744 0.4182 0.0332
-0.750 0.7922 0.01092 0.00372 -0.1747 0.4155 0.0347
-0.500 0.8224 0.01095 0.00372 -0.1749 0.4113 0.0366
-0.250 0.8527 0.01095 0.00371 -0.1752 0.4069 0.0399
0.000 0.8872 0.01041 0.00352 -0.1768 0.4022 0.1967
0.250 0.9178 0.01036 0.00353 -0.1772 0.3982 0.2266
0.500 0.9481 0.01033 0.00355 -0.1776 0.3947 0.2544
0.750 0.9783 0.01030 0.00360 -0.1780 0.3908 0.2902
1.000 1.0086 0.01027 0.00365 -0.1783 0.3879 0.3252
1.250 1.0386 0.01027 0.00372 -0.1786 0.3850 0.3488
1.500 1.0683 0.01032 0.00379 -0.1787 0.3813 0.3659
1.750 1.0976 0.01041 0.00388 -0.1788 0.3769 0.3788
2.000 1.1265 0.01053 0.00399 -0.1788 0.3719 0.3907
2.250 1.1557 0.01061 0.00410 -0.1789 0.3683 0.4032
2.500 1.1849 0.01069 0.00420 -0.1790 0.3651 0.4123
2.750 1.2139 0.01079 0.00430 -0.1790 0.3615 0.4178
3.000 1.2425 0.01093 0.00441 -0.1790 0.3571 0.4215
3.250 1.2708 0.01108 0.00455 -0.1789 0.3522 0.4258
3.500 1.2995 0.01118 0.00466 -0.1789 0.3481 0.4302
3.750 1.3279 0.01131 0.00479 -0.1789 0.3428 0.4344
4.000 1.3556 0.01149 0.00495 -0.1787 0.3367 0.4388
4.250 1.3835 0.01165 0.00509 -0.1786 0.3311 0.4428
4.500 1.4108 0.01185 0.00527 -0.1784 0.3217 0.4489
4.750 1.4370 0.01214 0.00550 -0.1781 0.3072 0.4542
5.000 1.4605 0.01264 0.00585 -0.1774 0.2823 0.4582
5.250 1.4821 0.01329 0.00631 -0.1764 0.2540 0.4619
5.500 1.5044 0.01384 0.00674 -0.1754 0.2345 0.4646
5.750 1.5273 0.01432 0.00714 -0.1746 0.2206 0.4679
6.000 1.5507 0.01472 0.00750 -0.1738 0.2099 0.4708
6.250 1.5738 0.01512 0.00786 -0.1730 0.2013 0.4737
6.500 1.5965 0.01553 0.00824 -0.1722 0.1936 0.4768
6.750 1.6194 0.01589 0.00859 -0.1713 0.1879 0.4800
7.000 1.6422 0.01624 0.00892 -0.1705 0.1829 0.4827
7.250 1.6633 0.01667 0.00932 -0.1694 0.1775 0.4848
7.500 1.6846 0.01704 0.00969 -0.1683 0.1731 0.4866
7.750 1.7049 0.01743 0.01007 -0.1670 0.1686 0.4892
8.000 1.7234 0.01787 0.01051 -0.1655 0.1645 0.4926
8.250 1.7413 0.01829 0.01095 -0.1639 0.1615 0.4959
8.500 1.7561 0.01867 0.01137 -0.1616 0.1593 0.4988
8.750 1.7714 0.01915 0.01187 -0.1596 0.1567 0.5014
9.000 1.7866 0.01971 0.01244 -0.1577 0.1537 0.5040
9.250 1.8007 0.02036 0.01310 -0.1557 0.1508 0.5063
9.500 1.8156 0.02099 0.01375 -0.1539 0.1485 0.5086
9.750 1.8311 0.02162 0.01442 -0.1523 0.1466 0.5110
10.000 1.8455 0.02234 0.01517 -0.1506 0.1445 0.5147
10.250 1.8589 0.02316 0.01604 -0.1490 0.1424 0.5180
10.500 1.8709 0.02411 0.01702 -0.1473 0.1402 0.5210
10.750 1.8820 0.02518 0.01812 -0.1457 0.1380 0.5240
11.000 1.8942 0.02622 0.01921 -0.1442 0.1365 0.5269
11.250 1.9062 0.02733 0.02037 -0.1429 0.1349 0.5296
11.500 1.9168 0.02859 0.02167 -0.1416 0.1328 0.5322
11.750 1.9260 0.03000 0.02312 -0.1402 0.1308 0.5356
12.000 1.9337 0.03161 0.02478 -0.1389 0.1288 0.5395
12.250 1.9397 0.03343 0.02665 -0.1377 0.1268 0.5430
12.500 1.9466 0.03523 0.02852 -0.1366 0.1252 0.5464
12.750 1.9530 0.03713 0.03048 -0.1356 0.1237 0.5497
13.000 1.9576 0.03925 0.03266 -0.1346 0.1218 0.5527
13.250 1.9602 0.04164 0.03510 -0.1337 0.1198 0.5552
13.500 1.9605 0.04429 0.03781 -0.1328 0.1179 0.5582
13.750 1.9589 0.04719 0.04079 -0.1319 0.1161 0.5617
14.000 1.9595 0.04992 0.04359 -0.1312 0.1147 0.5656
14.250 1.9592 0.05282 0.04657 -0.1306 0.1132 0.5696
14.500 1.9565 0.05601 0.04984 -0.1300 0.1114 0.5733
14.750 1.9513 0.05953 0.05343 -0.1294 0.1092 0.5763
15.250 1.9375 0.06713 0.06115 -0.1286 0.1047 0.5820
15.500 1.9326 0.07073 0.06483 -0.1282 0.1027 0.5853
15.750 1.9240 0.07484 0.06901 -0.1280 0.1000 0.5884
16.000 1.9134 0.07922 0.07344 -0.1279 0.0973 0.5914
16.250 1.9075 0.08301 0.07729 -0.1278 0.0946 0.5946
16.500 1.8964 0.08752 0.08185 -0.1278 0.0907 0.5971
16.750 1.8850 0.09207 0.08643 -0.1279 0.0861 0.5994
17.000 1.8686 0.09734 0.09172 -0.1282 0.0790 0.6014
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