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GOE 217 (MVA MK.12) AIRFOIL (goe217-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
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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