GOE 217 (MVA MK.12) AIRFOIL (goe217-il) Xfoil prediction polar at RE=200,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 217 (MVA MK.12) AIRFOIL (goe217-il) Reynolds number: 200,000 Max Cl/Cd: 70.65 at α=6.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe217-il-200000-n5.txt Download as CSV file: xf-goe217-il-200000-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 = 0.200 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-11.750 -0.2368 0.09472 0.09063 -0.0667 0.9527 0.0368
-11.500 -0.3314 0.06994 0.06540 -0.0872 0.9367 0.0358
-11.250 -0.3574 0.06023 0.05534 -0.0987 0.9139 0.0356
-11.000 -0.3700 0.05416 0.04898 -0.1059 0.8905 0.0356
-10.750 -0.3780 0.04973 0.04429 -0.1106 0.8679 0.0356
-10.500 -0.3793 0.04602 0.04033 -0.1154 0.8474 0.0356
-10.250 -0.3694 0.04256 0.03659 -0.1210 0.8288 0.0357
-10.000 -0.3521 0.03958 0.03334 -0.1262 0.8110 0.0357
-9.750 -0.3302 0.03705 0.03054 -0.1306 0.7941 0.0357
-9.500 -0.3055 0.03490 0.02813 -0.1342 0.7779 0.0358
-9.250 -0.2794 0.03309 0.02606 -0.1370 0.7621 0.0359
-9.000 -0.2525 0.03153 0.02428 -0.1392 0.7462 0.0360
-8.750 -0.2252 0.03017 0.02271 -0.1409 0.7319 0.0362
-8.250 -0.1697 0.02793 0.02010 -0.1433 0.7054 0.0365
-8.000 -0.1418 0.02700 0.01899 -0.1441 0.6933 0.0367
-7.750 -0.1136 0.02615 0.01801 -0.1448 0.6806 0.0369
-7.500 -0.0854 0.02540 0.01711 -0.1453 0.6687 0.0371
-7.250 -0.0569 0.02470 0.01630 -0.1458 0.6563 0.0373
-7.000 -0.0283 0.02408 0.01555 -0.1462 0.6452 0.0377
-6.750 -0.0020 0.02347 0.01497 -0.1459 0.6342 0.0382
-6.500 0.0254 0.02297 0.01444 -0.1459 0.6244 0.0386
-6.250 0.0539 0.02248 0.01394 -0.1461 0.6144 0.0391
-6.000 0.0824 0.02205 0.01346 -0.1463 0.6051 0.0395
-5.750 0.1117 0.02163 0.01301 -0.1467 0.5962 0.0398
-5.500 0.1415 0.02122 0.01256 -0.1472 0.5870 0.0402
-5.250 0.1720 0.02084 0.01212 -0.1479 0.5788 0.0405
-5.000 0.2038 0.02042 0.01168 -0.1490 0.5705 0.0409
-4.750 0.2363 0.02001 0.01121 -0.1504 0.5628 0.0414
-4.500 0.2700 0.01959 0.01071 -0.1521 0.5563 0.0418
-4.250 0.3054 0.01906 0.01015 -0.1543 0.5496 0.0423
-4.000 0.3411 0.01855 0.00956 -0.1566 0.5432 0.0430
-3.750 0.3755 0.01818 0.00907 -0.1584 0.5375 0.0438
-3.500 0.4093 0.01786 0.00866 -0.1600 0.5322 0.0448
-3.250 0.4424 0.01762 0.00834 -0.1612 0.5265 0.0462
-3.000 0.4752 0.01738 0.00801 -0.1623 0.5210 0.0479
-2.750 0.5072 0.01723 0.00775 -0.1632 0.5161 0.0497
-2.500 0.5391 0.01712 0.00755 -0.1639 0.5117 0.0515
-2.250 0.5712 0.01696 0.00739 -0.1648 0.5073 0.0543
-2.000 0.6031 0.01683 0.00724 -0.1655 0.5030 0.0604
-1.750 0.6408 0.01600 0.00690 -0.1685 0.4988 0.2164
-1.500 0.6725 0.01589 0.00687 -0.1694 0.4952 0.2588
-1.250 0.7035 0.01587 0.00692 -0.1700 0.4919 0.2987
-1.000 0.7340 0.01589 0.00706 -0.1704 0.4883 0.3282
-0.750 0.7639 0.01598 0.00721 -0.1706 0.4845 0.3503
-0.500 0.7934 0.01611 0.00736 -0.1707 0.4807 0.3694
-0.250 0.8226 0.01628 0.00754 -0.1707 0.4772 0.3877
0.000 0.8517 0.01649 0.00771 -0.1707 0.4742 0.4043
0.250 0.8807 0.01676 0.00792 -0.1707 0.4715 0.4197
0.500 0.9093 0.01699 0.00821 -0.1705 0.4688 0.4295
0.750 0.9384 0.01717 0.00840 -0.1705 0.4659 0.4376
1.000 0.9678 0.01732 0.00852 -0.1707 0.4629 0.4440
1.250 0.9961 0.01751 0.00874 -0.1705 0.4597 0.4484
1.500 1.0245 0.01770 0.00892 -0.1704 0.4563 0.4537
1.750 1.0529 0.01789 0.00904 -0.1703 0.4524 0.4599
2.000 1.0813 0.01808 0.00915 -0.1703 0.4480 0.4658
2.250 1.1085 0.01821 0.00938 -0.1700 0.4428 0.4697
2.500 1.1359 0.01837 0.00956 -0.1697 0.4378 0.4743
2.750 1.1632 0.01856 0.00971 -0.1694 0.4331 0.4805
3.000 1.1909 0.01880 0.00983 -0.1693 0.4289 0.4877
3.250 1.2173 0.01898 0.01015 -0.1689 0.4242 0.4925
3.500 1.2439 0.01917 0.01041 -0.1685 0.4197 0.4973
3.750 1.2709 0.01936 0.01060 -0.1682 0.4157 0.5017
4.000 1.2978 0.01956 0.01076 -0.1680 0.4118 0.5062
4.250 1.3248 0.01979 0.01092 -0.1678 0.4083 0.5105
4.500 1.3508 0.01997 0.01123 -0.1674 0.4043 0.5134
4.750 1.3766 0.02018 0.01151 -0.1670 0.3998 0.5164
5.000 1.4019 0.02039 0.01174 -0.1665 0.3951 0.5197
5.250 1.4269 0.02063 0.01196 -0.1659 0.3908 0.5236
5.500 1.4520 0.02087 0.01224 -0.1655 0.3862 0.5279
5.750 1.4771 0.02110 0.01252 -0.1650 0.3810 0.5319
6.000 1.5009 0.02134 0.01278 -0.1643 0.3756 0.5347
6.250 1.5235 0.02162 0.01306 -0.1634 0.3705 0.5374
6.500 1.5465 0.02189 0.01346 -0.1626 0.3640 0.5407
6.750 1.5680 0.02220 0.01380 -0.1615 0.3571 0.5443
7.000 1.5886 0.02254 0.01416 -0.1604 0.3505 0.5481
7.250 1.6092 0.02288 0.01455 -0.1593 0.3425 0.5519
7.500 1.6270 0.02330 0.01494 -0.1577 0.3345 0.5554
7.750 1.6445 0.02372 0.01544 -0.1561 0.3245 0.5582
8.000 1.6572 0.02426 0.01600 -0.1538 0.3138 0.5610
8.250 1.6628 0.02494 0.01667 -0.1503 0.3018 0.5640
8.500 1.6705 0.02581 0.01753 -0.1475 0.2875 0.5673
8.750 1.6755 0.02693 0.01861 -0.1446 0.2730 0.5707
9.000 1.6787 0.02830 0.01993 -0.1419 0.2599 0.5740
9.250 1.6805 0.02989 0.02148 -0.1393 0.2489 0.5771
9.500 1.6817 0.03168 0.02325 -0.1370 0.2394 0.5797
9.750 1.6842 0.03349 0.02510 -0.1350 0.2317 0.5821
10.000 1.6849 0.03557 0.02720 -0.1331 0.2248 0.5848
10.250 1.6854 0.03779 0.02945 -0.1314 0.2192 0.5879
10.500 1.6880 0.03994 0.03167 -0.1301 0.2139 0.5914
10.750 1.6875 0.04246 0.03422 -0.1288 0.2091 0.5948
11.000 1.6856 0.04521 0.03698 -0.1276 0.2051 0.5982
11.250 1.6890 0.04751 0.03936 -0.1268 0.2013 0.6011
11.500 1.6898 0.05010 0.04203 -0.1259 0.1975 0.6035
11.750 1.6882 0.05296 0.04494 -0.1250 0.1941 0.6061
12.000 1.6853 0.05599 0.04800 -0.1242 0.1910 0.6088
12.250 1.6877 0.05857 0.05066 -0.1236 0.1882 0.6122
12.500 1.6900 0.06120 0.05338 -0.1231 0.1852 0.6161
12.750 1.6912 0.06399 0.05622 -0.1227 0.1824 0.6200
13.000 1.6911 0.06691 0.05921 -0.1223 0.1798 0.6229
13.250 1.6912 0.06982 0.06215 -0.1218 0.1775 0.6259
13.500 1.6924 0.07261 0.06499 -0.1215 0.1753 0.6294
13.750 1.6963 0.07520 0.06768 -0.1213 0.1730 0.6332
14.000 1.6988 0.07798 0.07056 -0.1211 0.1706 0.6370
14.250 1.7010 0.08077 0.07341 -0.1210 0.1683 0.6404
14.500 1.7026 0.08362 0.07632 -0.1208 0.1662 0.6434
14.750 1.7052 0.08633 0.07907 -0.1207 0.1643 0.6469
15.000 1.7085 0.08889 0.08164 -0.1205 0.1625 0.6510
15.250 1.7115 0.09165 0.08449 -0.1206 0.1607 0.6554
15.500 1.7144 0.09443 0.08739 -0.1207 0.1586 0.6591
15.750 1.7167 0.09728 0.09035 -0.1208 0.1565 0.6632
16.000 1.7183 0.10025 0.09340 -0.1211 0.1545 0.6677
16.250 1.7206 0.10309 0.09629 -0.1213 0.1524 0.6723
16.500 1.7236 0.10578 0.09899 -0.1216 0.1504 0.6761
16.750 1.7269 0.10845 0.10172 -0.1218 0.1487 0.6803
17.000 1.7280 0.11158 0.10499 -0.1224 0.1467 0.6847
17.500 1.7282 0.11818 0.11181 -0.1239 0.1421 0.6931
17.750 1.7295 0.12124 0.11492 -0.1246 0.1398 0.6979
18.000 1.7327 0.12396 0.11766 -0.1253 0.1379 0.7034
18.250 1.7335 0.12717 0.12098 -0.1262 0.1360 0.7087
18.500 1.7328 0.13068 0.12465 -0.1274 0.1338 0.7146
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