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GOE 229 (MVA H.39) AIRFOIL (goe229-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 229 (MVA H.39) AIRFOIL (goe229-il)
Reynolds number: 1,000,000
Max Cl/Cd: 59.55 at α=3°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe229-il-1000000.txt
Download as CSV file: xf-goe229-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 229 (MVA H.39) 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
  ------ -------- --------- --------- -------- -------- --------
 -17.000  -0.5881   0.09432   0.09206  -0.0827   1.0000   0.0119
 -16.750  -0.6172   0.08609   0.08368  -0.0871   1.0000   0.0120
 -16.500  -0.6376   0.07992   0.07739  -0.0900   1.0000   0.0120
 -16.250  -0.6535   0.07492   0.07229  -0.0921   0.9998   0.0121
 -16.000  -0.6562   0.06944   0.06669  -0.0970   0.9975   0.0122
 -15.750  -0.6552   0.06457   0.06170  -0.1018   0.9950   0.0124
 -15.500  -0.6516   0.06028   0.05729  -0.1061   0.9906   0.0126
 -15.250  -0.6454   0.05642   0.05333  -0.1101   0.9841   0.0127
 -15.000  -0.6386   0.05308   0.04989  -0.1133   0.9743   0.0128
 -14.750  -0.6338   0.05017   0.04686  -0.1155   0.9609   0.0129
 -14.500  -0.6346   0.04728   0.04384  -0.1167   0.9460   0.0131
 -14.250  -0.6423   0.04406   0.04046  -0.1175   0.9316   0.0134
 -14.000  -0.6410   0.04169   0.03799  -0.1183   0.9193   0.0136
 -13.750  -0.6361   0.03956   0.03577  -0.1194   0.9079   0.0138
 -13.500  -0.6281   0.03765   0.03379  -0.1205   0.8975   0.0140
 -13.250  -0.6194   0.03582   0.03187  -0.1216   0.8875   0.0142
 -13.000  -0.6089   0.03403   0.03002  -0.1230   0.8782   0.0144
 -12.750  -0.5976   0.03235   0.02826  -0.1242   0.8699   0.0146
 -12.500  -0.5848   0.03071   0.02655  -0.1256   0.8615   0.0149
 -12.250  -0.5716   0.02912   0.02486  -0.1269   0.8534   0.0152
 -12.000  -0.5569   0.02759   0.02325  -0.1284   0.8451   0.0156
 -11.750  -0.5418   0.02619   0.02174  -0.1300   0.8373   0.0159
 -11.500  -0.5203   0.02486   0.02033  -0.1323   0.8301   0.0162
 -11.250  -0.5031   0.02295   0.01830  -0.1349   0.8226   0.0167
 -11.000  -0.4785   0.02155   0.01686  -0.1378   0.8159   0.0172
 -10.750  -0.4507   0.02049   0.01575  -0.1406   0.8089   0.0176
 -10.500  -0.4220   0.01958   0.01476  -0.1432   0.8024   0.0180
 -10.250  -0.3940   0.01881   0.01392  -0.1451   0.7954   0.0186
 -10.000  -0.3671   0.01819   0.01320  -0.1463   0.7887   0.0192
  -9.750  -0.3394   0.01764   0.01258  -0.1474   0.7826   0.0197
  -9.500  -0.3113   0.01724   0.01210  -0.1483   0.7761   0.0201
  -9.250  -0.2870   0.01616   0.01095  -0.1494   0.7701   0.0210
  -9.000  -0.2588   0.01575   0.01054  -0.1503   0.7640   0.0216
  -8.750  -0.2308   0.01543   0.01016  -0.1510   0.7578   0.0223
  -8.500  -0.2026   0.01505   0.00973  -0.1517   0.7519   0.0231
  -8.250  -0.1744   0.01468   0.00930  -0.1523   0.7452   0.0238
  -8.000  -0.1464   0.01441   0.00895  -0.1528   0.7369   0.0244
  -7.750  -0.1191   0.01379   0.00826  -0.1535   0.7280   0.0252
  -7.500  -0.0918   0.01319   0.00761  -0.1542   0.7199   0.0262
  -7.250  -0.0631   0.01288   0.00727  -0.1548   0.7127   0.0271
  -7.000  -0.0348   0.01259   0.00692  -0.1553   0.7057   0.0280
  -6.750  -0.0058   0.01227   0.00657  -0.1559   0.6990   0.0289
  -6.500   0.0228   0.01206   0.00629  -0.1563   0.6913   0.0296
  -6.250   0.0518   0.01194   0.00613  -0.1567   0.6841   0.0302
  -6.000   0.0800   0.01120   0.00528  -0.1576   0.6751   0.0317
  -5.750   0.1087   0.01091   0.00493  -0.1581   0.6640   0.0328
  -5.500   0.1369   0.01071   0.00465  -0.1585   0.6504   0.0339
  -5.250   0.1650   0.01057   0.00442  -0.1587   0.6363   0.0351
  -5.000   0.1932   0.01045   0.00420  -0.1590   0.6227   0.0360
  -4.750   0.2216   0.01035   0.00402  -0.1592   0.6085   0.0367
  -4.500   0.2492   0.01018   0.00371  -0.1594   0.5898   0.0385
  -4.250   0.2766   0.01010   0.00352  -0.1596   0.5697   0.0408
  -4.000   0.3042   0.01007   0.00338  -0.1597   0.5529   0.0428
  -3.750   0.3318   0.01007   0.00328  -0.1598   0.5379   0.0447
  -3.500   0.3593   0.01003   0.00315  -0.1599   0.5212   0.0526
  -3.250   0.3871   0.00901   0.00266  -0.1612   0.5037   0.2405
  -3.000   0.4147   0.00876   0.00261  -0.1616   0.4896   0.3279
  -2.750   0.4425   0.00882   0.00266  -0.1617   0.4750   0.3492
  -2.500   0.4695   0.00899   0.00272  -0.1617   0.4562   0.3606
  -2.250   0.4952   0.00923   0.00282  -0.1614   0.4254   0.3707
  -2.000   0.5020   0.01080   0.00353  -0.1580   0.2579   0.3754
  -1.750   0.5205   0.01153   0.00394  -0.1566   0.1867   0.3816
  -1.500   0.5392   0.01226   0.00436  -0.1552   0.1080   0.3879
  -1.250   0.5655   0.01245   0.00449  -0.1550   0.0995   0.3936
  -1.000   0.5921   0.01260   0.00463  -0.1549   0.0958   0.3997
  -0.750   0.6181   0.01279   0.00477  -0.1547   0.0911   0.4043
  -0.500   0.6445   0.01295   0.00489  -0.1545   0.0882   0.4079
  -0.250   0.6699   0.01314   0.00503  -0.1543   0.0817   0.4134
   0.000   0.6934   0.01344   0.00525  -0.1537   0.0591   0.4180
   0.250   0.7187   0.01363   0.00542  -0.1533   0.0561   0.4209
   0.500   0.7440   0.01381   0.00557  -0.1530   0.0548   0.4235
   0.750   0.7689   0.01400   0.00574  -0.1526   0.0539   0.4257
   1.000   0.7935   0.01417   0.00592  -0.1522   0.0531   0.4291
   1.250   0.8172   0.01437   0.00614  -0.1516   0.0522   0.4325
   1.500   0.8389   0.01459   0.00637  -0.1507   0.0512   0.4360
   1.750   0.8592   0.01484   0.00664  -0.1494   0.0501   0.4395
   2.000   0.8807   0.01510   0.00689  -0.1485   0.0496   0.4421
   2.250   0.9030   0.01537   0.00716  -0.1477   0.0492   0.4445
   2.500   0.9255   0.01564   0.00745  -0.1470   0.0489   0.4480
   2.750   0.9474   0.01594   0.00778  -0.1463   0.0487   0.4510
   3.000   0.9689   0.01627   0.00813  -0.1455   0.0484   0.4540
   3.250   0.9898   0.01663   0.00850  -0.1446   0.0482   0.4570
   3.500   1.0101   0.01702   0.00889  -0.1436   0.0480   0.4598
   3.750   1.0303   0.01743   0.00931  -0.1427   0.0478   0.4630
   4.000   1.0501   0.01785   0.00976  -0.1418   0.0477   0.4666
   4.250   1.0694   0.01830   0.01025  -0.1408   0.0475   0.4700
   4.500   1.0881   0.01880   0.01077  -0.1398   0.0473   0.4734
   4.750   1.1062   0.01935   0.01133  -0.1387   0.0472   0.4765
   5.000   1.1239   0.01994   0.01194  -0.1376   0.0471   0.4796
   5.250   1.1412   0.02055   0.01260  -0.1365   0.0469   0.4841
   5.500   1.1580   0.02122   0.01331  -0.1354   0.0468   0.4883
   5.750   1.1740   0.02195   0.01407  -0.1342   0.0466   0.4924
   6.000   1.1891   0.02277   0.01491  -0.1330   0.0460   0.4958
   6.250   1.2027   0.02370   0.01590  -0.1317   0.0454   0.5004
   6.500   1.2116   0.02498   0.01726  -0.1299   0.0446   0.5048
   6.750   1.2164   0.02659   0.01895  -0.1278   0.0441   0.5089
   7.000   1.2365   0.02714   0.01951  -0.1274   0.0438   0.5136
   7.250   1.2525   0.02799   0.02042  -0.1265   0.0434   0.5195
   7.500   1.2670   0.02897   0.02145  -0.1256   0.0431   0.5254
   7.750   1.2818   0.02996   0.02247  -0.1247   0.0426   0.5315
   8.000   1.2967   0.03096   0.02353  -0.1240   0.0417   0.5393
   8.250   1.3105   0.03204   0.02466  -0.1231   0.0409   0.5473
   8.500   1.3234   0.03322   0.02590  -0.1222   0.0402   0.5565
   8.750   1.3359   0.03445   0.02720  -0.1214   0.0395   0.5666
   9.000   1.3459   0.03594   0.02876  -0.1204   0.0389   0.5785
   9.250   1.3457   0.03836   0.03130  -0.1188   0.0381   0.5899
   9.500   1.3728   0.03839   0.03134  -0.1191   0.0374   0.6084
   9.750   1.3957   0.03878   0.03177  -0.1192   0.0359   0.6270
  10.000   1.4214   0.03891   0.03189  -0.1194   0.0338   0.6461
  10.250   1.4431   0.03942   0.03238  -0.1195   0.0318   0.6636
  10.500   1.4622   0.04014   0.03310  -0.1193   0.0258   0.6801
  10.750   1.4669   0.04220   0.03512  -0.1182   0.0137   0.6942
  11.000   1.4733   0.04416   0.03719  -0.1173   0.0128   0.7107
  11.250   1.4791   0.04621   0.03937  -0.1164   0.0121   0.7347
  11.500   1.4825   0.04791   0.04156  -0.1150   0.0114   1.0000
  11.750   1.4879   0.05007   0.04377  -0.1142   0.0110   1.0000
  12.000   1.4941   0.05219   0.04594  -0.1135   0.0107   1.0000
  12.250   1.4990   0.05449   0.04829  -0.1128   0.0105   1.0000
  12.500   1.5033   0.05688   0.05073  -0.1121   0.0102   1.0000
  12.750   1.5067   0.05937   0.05328  -0.1114   0.0099   1.0000
  13.000   1.5085   0.06207   0.05604  -0.1108   0.0096   1.0000
  13.250   1.5090   0.06497   0.05900  -0.1102   0.0094   1.0000
  13.500   1.5084   0.06804   0.06214  -0.1096   0.0091   1.0000
  13.750   1.5044   0.07156   0.06575  -0.1090   0.0089   1.0000
  14.000   1.5035   0.07473   0.06900  -0.1086   0.0087   1.0000
  14.250   1.5046   0.07769   0.07202  -0.1083   0.0086   1.0000
  14.500   1.5054   0.08070   0.07510  -0.1080   0.0084   1.0000
  14.750   1.5043   0.08401   0.07848  -0.1078   0.0082   1.0000
  15.000   1.5032   0.08733   0.08187  -0.1077   0.0081   1.0000
  15.250   1.5009   0.09081   0.08542  -0.1076   0.0079   1.0000
  15.500   1.4971   0.09453   0.08922  -0.1076   0.0078   1.0000
  15.750   1.4940   0.09819   0.09296  -0.1076   0.0076   1.0000
  16.000   1.4893   0.10212   0.09697  -0.1078   0.0075   1.0000
  16.250   1.4838   0.10620   0.10113  -0.1081   0.0074   1.0000
  16.500   1.4784   0.11027   0.10528  -0.1085   0.0073   1.0000
  16.750   1.4703   0.11478   0.10988  -0.1091   0.0072   1.0000
  17.000   1.4615   0.11949   0.11468  -0.1098   0.0071   1.0000
  17.250   1.4509   0.12455   0.11983  -0.1108   0.0070   1.0000
  17.500   1.4383   0.13001   0.12539  -0.1120   0.0069   1.0000
  17.750   1.4233   0.13591   0.13141  -0.1136   0.0069   1.0000
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