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GOE 692 AIRFOIL (goe692-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: GOE 692 AIRFOIL (goe692-il)
Reynolds number: 500,000
Max Cl/Cd: 108.95 at α=5.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe692-il-500000.txt
Download as CSV file: xf-goe692-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 692 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
  ------ -------- --------- --------- -------- -------- --------
 -13.750  -0.7615   0.04335   0.03976  -0.1199   0.9913   0.0363
 -13.500  -0.7632   0.03774   0.03384  -0.1279   0.9845   0.0365
 -13.250  -0.7571   0.03448   0.03033  -0.1311   0.9783   0.0368
 -13.000  -0.7450   0.03203   0.02765  -0.1327   0.9722   0.0372
 -12.750  -0.7284   0.03010   0.02550  -0.1338   0.9671   0.0376
 -12.500  -0.7124   0.02867   0.02385  -0.1338   0.9595   0.0379
 -12.250  -0.6959   0.02673   0.02172  -0.1340   0.9541   0.0384
 -12.000  -0.6800   0.02534   0.02025  -0.1332   0.9459   0.0388
 -11.750  -0.6576   0.02429   0.01913  -0.1333   0.9409   0.0393
 -11.500  -0.6390   0.02347   0.01824  -0.1324   0.9327   0.0397
 -11.250  -0.6172   0.02262   0.01730  -0.1320   0.9267   0.0403
 -11.000  -0.5966   0.02185   0.01642  -0.1313   0.9198   0.0408
 -10.750  -0.5751   0.02107   0.01552  -0.1306   0.9131   0.0414
 -10.500  -0.5523   0.02033   0.01463  -0.1302   0.9078   0.0420
 -10.250  -0.5302   0.01969   0.01386  -0.1295   0.9011   0.0426
 -10.000  -0.5064   0.01913   0.01316  -0.1290   0.8955   0.0431
  -9.750  -0.4846   0.01816   0.01215  -0.1285   0.8902   0.0441
  -9.500  -0.4611   0.01765   0.01161  -0.1280   0.8840   0.0449
  -9.250  -0.4363   0.01717   0.01107  -0.1276   0.8785   0.0457
  -9.000  -0.4109   0.01672   0.01053  -0.1273   0.8736   0.0467
  -8.750  -0.3861   0.01628   0.01001  -0.1269   0.8681   0.0477
  -8.500  -0.3603   0.01590   0.00951  -0.1266   0.8628   0.0486
  -8.250  -0.3357   0.01526   0.00885  -0.1262   0.8580   0.0500
  -8.000  -0.3101   0.01492   0.00849  -0.1259   0.8527   0.0514
  -7.750  -0.2838   0.01461   0.00814  -0.1257   0.8471   0.0531
  -7.500  -0.2567   0.01434   0.00775  -0.1255   0.8420   0.0549
  -7.250  -0.2309   0.01392   0.00735  -0.1252   0.8371   0.0572
  -7.000  -0.2042   0.01368   0.00709  -0.1250   0.8316   0.0597
  -6.750  -0.1775   0.01336   0.00670  -0.1248   0.8263   0.0625
  -6.500  -0.1500   0.01313   0.00644  -0.1248   0.8213   0.0657
  -6.250  -0.1227   0.01297   0.00623  -0.1246   0.8155   0.0691
  -6.000  -0.0965   0.01260   0.00589  -0.1244   0.8097   0.0731
  -5.750  -0.0681   0.01249   0.00568  -0.1244   0.8047   0.0771
  -5.500  -0.0418   0.01216   0.00539  -0.1242   0.7988   0.0814
  -5.250  -0.0143   0.01200   0.00520  -0.1241   0.7927   0.0854
  -5.000   0.0133   0.01177   0.00491  -0.1240   0.7872   0.0895
  -4.750   0.0404   0.01158   0.00474  -0.1239   0.7811   0.0937
  -4.500   0.0682   0.01145   0.00456  -0.1238   0.7746   0.0975
  -4.250   0.0958   0.01123   0.00433  -0.1238   0.7688   0.1028
  -4.000   0.1232   0.01110   0.00420  -0.1236   0.7621   0.1078
  -3.750   0.1506   0.01091   0.00402  -0.1235   0.7553   0.1137
  -3.500   0.1788   0.01082   0.00389  -0.1235   0.7492   0.1206
  -3.250   0.2060   0.01066   0.00379  -0.1234   0.7419   0.1295
  -3.000   0.2339   0.01056   0.00367  -0.1233   0.7355   0.1401
  -2.750   0.2619   0.01050   0.00360  -0.1233   0.7291   0.1509
  -2.500   0.2894   0.01036   0.00352  -0.1232   0.7223   0.1631
  -2.250   0.3175   0.01030   0.00342  -0.1233   0.7164   0.1738
  -2.000   0.3453   0.01025   0.00338  -0.1232   0.7098   0.1836
  -1.750   0.3729   0.01015   0.00331  -0.1232   0.7035   0.1941
  -1.500   0.4012   0.01015   0.00324  -0.1232   0.6979   0.2032
  -1.250   0.4286   0.01005   0.00321  -0.1231   0.6916   0.2146
  -1.000   0.4563   0.01000   0.00316  -0.1231   0.6857   0.2265
  -0.750   0.4844   0.00998   0.00312  -0.1232   0.6803   0.2402
  -0.250   0.5391   0.00980   0.00310  -0.1231   0.6688   0.2852
   0.000   0.5666   0.00970   0.00310  -0.1231   0.6637   0.3329
   0.250   0.5923   0.00939   0.00315  -0.1229   0.6581   0.4343
   0.500   0.6160   0.00892   0.00322  -0.1223   0.6526   0.6086
   0.750   0.6371   0.00852   0.00335  -0.1207   0.6477   0.7890
   1.000   0.6581   0.00839   0.00353  -0.1185   0.6427   0.9045
   1.250   0.6925   0.00846   0.00363  -0.1196   0.6370   0.9570
   1.500   0.7316   0.00861   0.00369  -0.1219   0.6316   0.9793
   1.750   0.7767   0.00873   0.00378  -0.1256   0.6258   0.9907
   2.000   0.8236   0.00883   0.00383  -0.1298   0.6182   0.9981
   2.250   0.8529   0.00896   0.00386  -0.1303   0.6106   1.0000
   2.500   0.8738   0.00900   0.00390  -0.1289   0.6030   1.0000
   2.750   0.8958   0.00911   0.00393  -0.1277   0.5962   1.0000
   3.000   0.9178   0.00919   0.00400  -0.1266   0.5895   1.0000
   3.250   0.9398   0.00928   0.00406  -0.1254   0.5825   1.0000
   3.500   0.9624   0.00942   0.00413  -0.1243   0.5762   1.0000
   3.750   0.9847   0.00949   0.00422  -0.1232   0.5688   1.0000
   4.000   1.0070   0.00962   0.00429  -0.1221   0.5612   1.0000
   4.250   1.0298   0.00972   0.00439  -0.1212   0.5532   1.0000
   4.500   1.0523   0.00986   0.00448  -0.1201   0.5449   1.0000
   4.750   1.0753   0.00999   0.00460  -0.1192   0.5367   1.0000
   5.000   1.0974   0.01015   0.00472  -0.1181   0.5277   1.0000
   5.250   1.1198   0.01029   0.00486  -0.1171   0.5183   1.0000
   5.750   1.1625   0.01067   0.00517  -0.1147   0.4980   1.0000
   6.000   1.1830   0.01089   0.00536  -0.1134   0.4884   1.0000
   6.250   1.2030   0.01112   0.00555  -0.1119   0.4779   1.0000
   6.500   1.2219   0.01135   0.00577  -0.1103   0.4677   1.0000
   6.750   1.2379   0.01166   0.00602  -0.1081   0.4573   1.0000
   7.000   1.2563   0.01193   0.00628  -0.1065   0.4464   1.0000
   7.250   1.2737   0.01226   0.00659  -0.1046   0.4359   1.0000
   7.500   1.2897   0.01266   0.00693  -0.1026   0.4247   1.0000
   7.750   1.3079   0.01301   0.00728  -0.1011   0.4133   1.0000
   8.000   1.3244   0.01344   0.00768  -0.0993   0.4020   1.0000
   8.250   1.3390   0.01395   0.00814  -0.0972   0.3898   1.0000
   8.500   1.3551   0.01443   0.00860  -0.0955   0.3766   1.0000
   8.750   1.3701   0.01499   0.00913  -0.0936   0.3630   1.0000
   9.000   1.3840   0.01561   0.00971  -0.0917   0.3490   1.0000
   9.250   1.3969   0.01631   0.01036  -0.0897   0.3347   1.0000
   9.500   1.4087   0.01710   0.01110  -0.0876   0.3201   1.0000
   9.750   1.4197   0.01796   0.01191  -0.0855   0.3053   1.0000
  10.000   1.4297   0.01892   0.01281  -0.0833   0.2907   1.0000
  10.250   1.4404   0.01989   0.01374  -0.0814   0.2769   1.0000
  10.500   1.4509   0.02090   0.01473  -0.0795   0.2642   1.0000
  10.750   1.4606   0.02200   0.01579  -0.0776   0.2525   1.0000
  11.000   1.4685   0.02324   0.01699  -0.0756   0.2412   1.0000
  11.250   1.4770   0.02448   0.01820  -0.0738   0.2299   1.0000
  11.500   1.4860   0.02571   0.01942  -0.0721   0.2194   1.0000
  11.750   1.4925   0.02715   0.02082  -0.0702   0.2095   1.0000
  12.000   1.5005   0.02852   0.02218  -0.0686   0.2000   1.0000
  12.250   1.5085   0.02993   0.02359  -0.0671   0.1916   1.0000
  12.500   1.5141   0.03155   0.02519  -0.0654   0.1834   1.0000
  12.750   1.5231   0.03295   0.02661  -0.0641   0.1761   1.0000
  13.000   1.5283   0.03470   0.02834  -0.0626   0.1692   1.0000
  13.250   1.5366   0.03623   0.02990  -0.0614   0.1636   1.0000
  13.500   1.5440   0.03785   0.03154  -0.0603   0.1585   1.0000
  13.750   1.5478   0.03983   0.03352  -0.0589   0.1539   1.0000
  14.000   1.5570   0.04136   0.03511  -0.0580   0.1503   1.0000
  14.250   1.5648   0.04307   0.03686  -0.0571   0.1464   1.0000
  14.500   1.5693   0.04510   0.03890  -0.0561   0.1427   1.0000
  14.750   1.5727   0.04724   0.04106  -0.0550   0.1392   1.0000
  15.000   1.5825   0.04883   0.04274  -0.0544   0.1363   1.0000
  15.250   1.5892   0.05074   0.04469  -0.0537   0.1331   1.0000
  15.500   1.5931   0.05295   0.04693  -0.0530   0.1301   1.0000
  15.750   1.5947   0.05541   0.04942  -0.0521   0.1273   1.0000
  16.000   1.6025   0.05726   0.05134  -0.0516   0.1251   1.0000
  16.250   1.6096   0.05920   0.05338  -0.0512   0.1225   1.0000
  16.500   1.6143   0.06141   0.05563  -0.0507   0.1196   1.0000
  16.750   1.6152   0.06407   0.05833  -0.0502   0.1167   1.0000
  17.000   1.6168   0.06666   0.06096  -0.0497   0.1138   1.0000
  17.250   1.6243   0.06866   0.06306  -0.0495   0.1108   1.0000
  17.500   1.6274   0.07112   0.06559  -0.0492   0.1074   1.0000
  17.750   1.6256   0.07420   0.06869  -0.0489   0.1039   1.0000
  18.000   1.6297   0.07662   0.07120  -0.0488   0.1004   1.0000
  18.250   1.6318   0.07931   0.07394  -0.0488   0.0954   1.0000
  18.500   1.6300   0.08251   0.07718  -0.0488   0.0900   1.0000
  18.750   1.6268   0.08592   0.08060  -0.0489   0.0807   1.0000
  19.000   1.6146   0.09048   0.08510  -0.0491   0.0676   1.0000
  19.250   1.5958   0.09597   0.09055  -0.0496   0.0573   1.0000
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