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GOE 217 (MVA MK.12) AIRFOIL (goe217-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
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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