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GOE 527 AIRFOIL (goe527-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: GOE 527 AIRFOIL (goe527-il)
Reynolds number: 500,000
Max Cl/Cd: 102.34 at α=6°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe527-il-500000.txt
Download as CSV file: xf-goe527-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 527 AIRFOIL                                 
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.250  -0.1845   0.11133   0.10897  -0.0690   0.9772   0.0429
 -12.000  -0.1623   0.10889   0.10652  -0.0708   0.9695   0.0432
 -11.750  -0.4754   0.03257   0.02892  -0.1374   0.9316   0.0364
 -11.500  -0.4728   0.02929   0.02520  -0.1383   0.9100   0.0368
 -11.250  -0.4680   0.02729   0.02283  -0.1369   0.8909   0.0372
 -11.000  -0.4613   0.02574   0.02096  -0.1349   0.8742   0.0375
 -10.750  -0.4502   0.02475   0.01966  -0.1329   0.8597   0.0378
 -10.500  -0.4393   0.02300   0.01769  -0.1311   0.8468   0.0383
 -10.250  -0.4220   0.02208   0.01669  -0.1297   0.8346   0.0387
 -10.000  -0.4025   0.02145   0.01598  -0.1285   0.8240   0.0393
  -9.750  -0.3834   0.02077   0.01516  -0.1273   0.8134   0.0397
  -9.500  -0.3640   0.02006   0.01432  -0.1260   0.8033   0.0402
  -9.250  -0.3438   0.01935   0.01344  -0.1248   0.7935   0.0407
  -9.000  -0.3232   0.01867   0.01263  -0.1236   0.7836   0.0413
  -8.750  -0.3017   0.01808   0.01186  -0.1225   0.7746   0.0419
  -8.500  -0.2796   0.01754   0.01118  -0.1214   0.7656   0.0424
  -8.250  -0.2579   0.01683   0.01032  -0.1203   0.7572   0.0430
  -8.000  -0.2355   0.01619   0.00967  -0.1194   0.7488   0.0438
  -7.750  -0.2121   0.01578   0.00920  -0.1186   0.7403   0.0446
  -7.500  -0.1883   0.01539   0.00874  -0.1177   0.7320   0.0453
  -7.250  -0.1645   0.01500   0.00827  -0.1168   0.7234   0.0462
  -7.000  -0.1404   0.01464   0.00779  -0.1160   0.7157   0.0471
  -6.750  -0.1158   0.01433   0.00739  -0.1152   0.7074   0.0479
  -6.250  -0.0684   0.01351   0.00652  -0.1135   0.6918   0.0503
  -6.000  -0.0436   0.01329   0.00623  -0.1128   0.6837   0.0518
  -5.750  -0.0184   0.01307   0.00594  -0.1121   0.6759   0.0534
  -5.500   0.0055   0.01271   0.00555  -0.1112   0.6680   0.0552
  -5.250   0.0307   0.01253   0.00534  -0.1106   0.6609   0.0574
  -5.000   0.0563   0.01236   0.00512  -0.1099   0.6531   0.0600
  -4.750   0.0809   0.01214   0.00487  -0.1092   0.6458   0.0631
  -4.500   0.1071   0.01203   0.00473  -0.1087   0.6385   0.0673
  -4.250   0.1325   0.01188   0.00459  -0.1081   0.6313   0.0722
  -4.000   0.1585   0.01179   0.00446  -0.1075   0.6249   0.0779
  -3.750   0.1851   0.01174   0.00441  -0.1071   0.6181   0.0833
  -3.500   0.2106   0.01163   0.00426  -0.1065   0.6117   0.0885
  -3.250   0.2371   0.01161   0.00421  -0.1061   0.6056   0.0933
  -3.000   0.2629   0.01147   0.00406  -0.1056   0.5995   0.0982
  -2.750   0.2889   0.01141   0.00397  -0.1051   0.5939   0.1030
  -2.500   0.3155   0.01141   0.00391  -0.1047   0.5886   0.1071
  -2.250   0.3408   0.01121   0.00375  -0.1041   0.5831   0.1124
  -2.000   0.3667   0.01115   0.00366  -0.1036   0.5778   0.1174
  -1.750   0.3931   0.01115   0.00358  -0.1032   0.5730   0.1222
  -1.500   0.4187   0.01100   0.00350  -0.1027   0.5685   0.1303
  -1.250   0.4447   0.01092   0.00343  -0.1022   0.5636   0.1394
  -1.000   0.4705   0.01084   0.00337  -0.1017   0.5590   0.1526
  -0.750   0.4958   0.01071   0.00336  -0.1012   0.5546   0.1931
  -0.500   0.5193   0.01037   0.00337  -0.1005   0.5505   0.2919
  -0.250   0.5422   0.01007   0.00339  -0.0996   0.5456   0.3965
   0.000   0.5651   0.00987   0.00343  -0.0986   0.5405   0.4899
   0.250   0.5882   0.00973   0.00350  -0.0976   0.5357   0.5716
   0.500   0.6086   0.00945   0.00356  -0.0960   0.5310   0.6691
   0.750   0.6267   0.00912   0.00364  -0.0937   0.5262   0.8015
   1.000   0.6810   0.00920   0.00389  -0.0986   0.5199   0.9505
   1.250   0.7397   0.00934   0.00401  -0.1050   0.5142   0.9772
   1.500   0.7905   0.00947   0.00408  -0.1097   0.5092   0.9889
   1.750   0.8410   0.00963   0.00414  -0.1145   0.5045   0.9976
   2.000   0.8749   0.00976   0.00421  -0.1159   0.5004   1.0000
   2.250   0.8959   0.00982   0.00427  -0.1145   0.4965   1.0000
   2.500   0.9168   0.00991   0.00434  -0.1132   0.4925   1.0000
   2.750   0.9376   0.01002   0.00440  -0.1117   0.4885   1.0000
   3.000   0.9589   0.01020   0.00450  -0.1105   0.4843   1.0000
   3.250   0.9795   0.01027   0.00459  -0.1090   0.4806   1.0000
   3.500   1.0000   0.01035   0.00467  -0.1075   0.4761   1.0000
   3.750   1.0200   0.01046   0.00475  -0.1060   0.4712   1.0000
   4.000   1.0403   0.01064   0.00485  -0.1045   0.4663   1.0000
   4.250   1.0602   0.01070   0.00495  -0.1029   0.4612   1.0000
   4.500   1.0801   0.01081   0.00505  -0.1014   0.4561   1.0000
   4.750   1.0997   0.01097   0.00516  -0.0998   0.4513   1.0000
   5.000   1.1197   0.01110   0.00529  -0.0983   0.4466   1.0000
   5.250   1.1393   0.01121   0.00541  -0.0967   0.4412   1.0000
   5.500   1.1574   0.01137   0.00553  -0.0949   0.4356   1.0000
   5.750   1.1759   0.01153   0.00569  -0.0931   0.4301   1.0000
   6.000   1.1933   0.01166   0.00583  -0.0911   0.4239   1.0000
   6.250   1.2077   0.01185   0.00598  -0.0886   0.4180   1.0000
   6.500   1.2240   0.01201   0.00616  -0.0864   0.4119   1.0000
   6.750   1.2396   0.01220   0.00634  -0.0842   0.4046   1.0000
   7.000   1.2542   0.01246   0.00656  -0.0819   0.3979   1.0000
   7.250   1.2714   0.01267   0.00679  -0.0800   0.3904   1.0000
   7.750   1.3017   0.01327   0.00736  -0.0759   0.3743   1.0000
   8.000   1.3139   0.01368   0.00773  -0.0734   0.3652   1.0000
   8.250   1.3285   0.01406   0.00810  -0.0714   0.3552   1.0000
   8.500   1.3412   0.01453   0.00854  -0.0693   0.3458   1.0000
   8.750   1.3528   0.01507   0.00905  -0.0670   0.3363   1.0000
   9.000   1.3661   0.01560   0.00957  -0.0651   0.3273   1.0000
   9.500   1.3886   0.01691   0.01085  -0.0610   0.3094   1.0000
   9.750   1.3971   0.01776   0.01165  -0.0587   0.3009   1.0000
  10.000   1.4094   0.01848   0.01238  -0.0571   0.2930   1.0000
  10.250   1.4171   0.01946   0.01333  -0.0550   0.2859   1.0000
  10.500   1.4305   0.02021   0.01411  -0.0537   0.2799   1.0000
  10.750   1.4401   0.02118   0.01508  -0.0520   0.2742   1.0000
  11.000   1.4493   0.02223   0.01612  -0.0504   0.2692   1.0000
  11.250   1.4622   0.02309   0.01703  -0.0493   0.2646   1.0000
  11.500   1.4721   0.02417   0.01812  -0.0479   0.2601   1.0000
  11.750   1.4790   0.02546   0.01940  -0.0464   0.2557   1.0000
  12.000   1.4913   0.02644   0.02043  -0.0454   0.2523   1.0000
  12.250   1.5027   0.02751   0.02156  -0.0444   0.2486   1.0000
  12.500   1.5120   0.02875   0.02282  -0.0434   0.2448   1.0000
  12.750   1.5181   0.03022   0.02429  -0.0421   0.2410   1.0000
  13.000   1.5276   0.03151   0.02562  -0.0412   0.2378   1.0000
  13.250   1.5389   0.03269   0.02688  -0.0404   0.2345   1.0000
  13.500   1.5475   0.03409   0.02834  -0.0396   0.2310   1.0000
  13.750   1.5531   0.03576   0.03001  -0.0387   0.2271   1.0000
  14.000   1.5583   0.03748   0.03175  -0.0377   0.2228   1.0000
  14.250   1.5666   0.03906   0.03342  -0.0372   0.2182   1.0000
  14.500   1.5717   0.04091   0.03530  -0.0365   0.2138   1.0000
  14.750   1.5725   0.04311   0.03748  -0.0357   0.2092   1.0000
  15.000   1.5803   0.04485   0.03932  -0.0353   0.2047   1.0000
  15.250   1.5845   0.04688   0.04141  -0.0348   0.1998   1.0000
  15.500   1.5838   0.04939   0.04391  -0.0342   0.1952   1.0000
  15.750   1.5892   0.05141   0.04603  -0.0339   0.1906   1.0000
  16.000   1.5915   0.05374   0.04840  -0.0336   0.1852   1.0000
  16.250   1.5879   0.05667   0.05132  -0.0332   0.1801   1.0000
  16.500   1.5922   0.05889   0.05363  -0.0330   0.1746   1.0000
  16.750   1.5899   0.06179   0.05655  -0.0328   0.1689   1.0000
  17.000   1.5885   0.06462   0.05942  -0.0327   0.1637   1.0000
  17.250   1.5876   0.06741   0.06226  -0.0326   0.1587   1.0000
  17.500   1.5815   0.07079   0.06564  -0.0325   0.1538   1.0000
  17.750   1.5814   0.07356   0.06847  -0.0325   0.1493   1.0000
  18.000   1.5784   0.07666   0.07160  -0.0326   0.1452   1.0000
  18.250   1.5712   0.08026   0.07520  -0.0327   0.1411   1.0000
  18.500   1.5724   0.08289   0.07791  -0.0329   0.1384   1.0000
  18.750   1.5700   0.08600   0.08107  -0.0331   0.1349   1.0000
  19.000   1.5646   0.08949   0.08457  -0.0335   0.1316   1.0000
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