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GOE 624 AIRFOIL (goe624-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 624 AIRFOIL (goe624-il)
Reynolds number: 1,000,000
Max Cl/Cd: 126.86 at α=7.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe624-il-1000000.txt
Download as CSV file: xf-goe624-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 624 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
  ------ -------- --------- --------- -------- -------- --------
 -14.750  -0.7634   0.06563   0.06323  -0.0748   1.0000   0.0251
 -14.500  -0.8345   0.04706   0.04429  -0.0928   1.0000   0.0250
 -14.250  -0.8545   0.03929   0.03628  -0.1019   1.0000   0.0250
 -14.000  -0.8583   0.03517   0.03197  -0.1065   0.9852   0.0251
 -13.750  -0.8582   0.03270   0.02930  -0.1072   0.9604   0.0252
 -13.500  -0.8614   0.03120   0.02762  -0.1046   0.9393   0.0253
 -13.250  -0.8541   0.02988   0.02612  -0.1032   0.9244   0.0254
 -13.000  -0.8415   0.02885   0.02493  -0.1021   0.9120   0.0256
 -12.750  -0.8341   0.02698   0.02282  -0.1008   0.9003   0.0258
 -12.500  -0.8245   0.02498   0.02065  -0.0996   0.8896   0.0261
 -12.250  -0.8070   0.02386   0.01944  -0.0988   0.8811   0.0264
 -12.000  -0.7873   0.02297   0.01847  -0.0981   0.8728   0.0266
 -11.750  -0.7663   0.02218   0.01758  -0.0975   0.8654   0.0268
 -11.500  -0.7444   0.02143   0.01674  -0.0970   0.8579   0.0270
 -11.250  -0.7221   0.02074   0.01594  -0.0965   0.8506   0.0273
 -11.000  -0.6988   0.02003   0.01515  -0.0961   0.8440   0.0275
 -10.750  -0.6754   0.01936   0.01438  -0.0956   0.8370   0.0278
 -10.500  -0.6515   0.01874   0.01364  -0.0952   0.8306   0.0281
 -10.250  -0.6267   0.01811   0.01294  -0.0949   0.8246   0.0283
 -10.000  -0.6018   0.01754   0.01227  -0.0945   0.8179   0.0286
  -9.750  -0.5763   0.01707   0.01170  -0.0942   0.8111   0.0289
  -9.500  -0.5500   0.01664   0.01119  -0.0940   0.8034   0.0292
  -9.250  -0.5239   0.01625   0.01069  -0.0937   0.7955   0.0294
  -9.000  -0.4985   0.01557   0.00993  -0.0934   0.7882   0.0296
  -8.750  -0.4745   0.01470   0.00897  -0.0930   0.7801   0.0301
  -8.500  -0.4485   0.01415   0.00837  -0.0928   0.7724   0.0305
  -8.250  -0.4218   0.01372   0.00789  -0.0926   0.7643   0.0308
  -8.000  -0.3948   0.01336   0.00747  -0.0924   0.7570   0.0312
  -7.750  -0.3673   0.01300   0.00707  -0.0924   0.7497   0.0316
  -7.500  -0.3399   0.01268   0.00668  -0.0922   0.7421   0.0320
  -7.250  -0.3120   0.01236   0.00632  -0.0922   0.7346   0.0325
  -7.000  -0.2842   0.01208   0.00597  -0.0921   0.7263   0.0329
  -6.750  -0.2560   0.01184   0.00567  -0.0921   0.7185   0.0334
  -6.500  -0.2278   0.01160   0.00536  -0.0921   0.7104   0.0338
  -6.250  -0.2006   0.01117   0.00488  -0.0920   0.7030   0.0346
  -6.000  -0.1724   0.01088   0.00456  -0.0920   0.6952   0.0353
  -5.750  -0.1442   0.01068   0.00430  -0.0920   0.6874   0.0360
  -5.500  -0.1155   0.01047   0.00406  -0.0920   0.6800   0.0368
  -5.250  -0.0870   0.01031   0.00384  -0.0921   0.6723   0.0376
  -5.000  -0.0582   0.01013   0.00362  -0.0921   0.6657   0.0385
  -4.750  -0.0297   0.00990   0.00338  -0.0922   0.6590   0.0402
  -4.500  -0.0011   0.00976   0.00320  -0.0923   0.6524   0.0419
  -4.250   0.0280   0.00959   0.00302  -0.0924   0.6466   0.0445
  -4.000   0.0567   0.00943   0.00286  -0.0925   0.6400   0.0493
  -3.750   0.0853   0.00927   0.00274  -0.0926   0.6337   0.0611
  -3.500   0.1144   0.00915   0.00267  -0.0928   0.6276   0.0724
  -3.250   0.1435   0.00911   0.00261  -0.0929   0.6212   0.0789
  -3.000   0.1725   0.00904   0.00255  -0.0931   0.6155   0.0849
  -2.750   0.2020   0.00901   0.00250  -0.0933   0.6096   0.0885
  -2.500   0.2309   0.00893   0.00242  -0.0934   0.6033   0.0939
  -2.250   0.2601   0.00889   0.00237  -0.0936   0.5972   0.0982
  -2.000   0.2893   0.00883   0.00231  -0.0938   0.5905   0.1031
  -1.750   0.3181   0.00880   0.00226  -0.0939   0.5831   0.1089
  -1.500   0.3474   0.00874   0.00220  -0.0942   0.5767   0.1150
  -1.250   0.3763   0.00868   0.00216  -0.0943   0.5692   0.1247
  -1.000   0.4051   0.00862   0.00213  -0.0945   0.5619   0.1402
  -0.750   0.4338   0.00850   0.00210  -0.0947   0.5534   0.1731
  -0.500   0.4621   0.00839   0.00209  -0.0948   0.5446   0.2152
  -0.250   0.4904   0.00827   0.00209  -0.0950   0.5347   0.2647
   0.250   0.5463   0.00802   0.00214  -0.0953   0.5146   0.3932
   0.500   0.5739   0.00782   0.00217  -0.0954   0.5043   0.4900
   0.750   0.6003   0.00758   0.00224  -0.0953   0.4939   0.6156
   1.000   0.6257   0.00730   0.00233  -0.0948   0.4840   0.7529
   1.250   0.6492   0.00714   0.00245  -0.0937   0.4757   0.8611
   1.500   0.6723   0.00713   0.00256  -0.0923   0.4677   0.9280
   1.750   0.7016   0.00724   0.00264  -0.0925   0.4601   0.9658
   2.000   0.7385   0.00736   0.00272  -0.0944   0.4531   0.9844
   2.250   0.7796   0.00755   0.00282  -0.0974   0.4456   0.9959
   2.500   0.8177   0.00765   0.00290  -0.0996   0.4400   1.0000
   2.750   0.8424   0.00778   0.00297  -0.0991   0.4340   1.0000
   3.000   0.8668   0.00793   0.00307  -0.0984   0.4278   1.0000
   3.250   0.8928   0.00802   0.00314  -0.0981   0.4228   1.0000
   3.500   0.9184   0.00816   0.00323  -0.0977   0.4169   1.0000
   3.750   0.9437   0.00834   0.00335  -0.0973   0.4111   1.0000
   4.000   0.9708   0.00842   0.00343  -0.0972   0.4079   1.0000
   4.250   0.9977   0.00854   0.00353  -0.0971   0.4043   1.0000
   4.500   1.0242   0.00868   0.00365  -0.0969   0.4004   1.0000
   4.750   1.0501   0.00886   0.00379  -0.0967   0.3962   1.0000
   5.000   1.0769   0.00899   0.00392  -0.0966   0.3930   1.0000
   5.250   1.1042   0.00909   0.00403  -0.0966   0.3897   1.0000
   5.500   1.1309   0.00923   0.00415  -0.0965   0.3857   1.0000
   5.750   1.1569   0.00941   0.00430  -0.0963   0.3815   1.0000
   6.000   1.1825   0.00961   0.00448  -0.0960   0.3772   1.0000
   6.250   1.2097   0.00971   0.00460  -0.0961   0.3744   1.0000
   6.500   1.2363   0.00984   0.00475  -0.0960   0.3706   1.0000
   6.750   1.2619   0.01002   0.00491  -0.0958   0.3662   1.0000
   7.000   1.2864   0.01026   0.00511  -0.0954   0.3607   1.0000
   7.250   1.3131   0.01037   0.00525  -0.0953   0.3562   1.0000
   7.500   1.3384   0.01055   0.00543  -0.0951   0.3513   1.0000
   7.750   1.3623   0.01079   0.00565  -0.0946   0.3462   1.0000
   8.000   1.3875   0.01096   0.00584  -0.0943   0.3420   1.0000
   8.250   1.4122   0.01115   0.00603  -0.0940   0.3366   1.0000
   8.500   1.4343   0.01144   0.00629  -0.0932   0.3297   1.0000
   8.750   1.4581   0.01164   0.00650  -0.0927   0.3229   1.0000
   9.000   1.4789   0.01195   0.00678  -0.0918   0.3149   1.0000
   9.250   1.4996   0.01221   0.00705  -0.0908   0.3084   1.0000
   9.500   1.5177   0.01255   0.00737  -0.0893   0.3003   1.0000
   9.750   1.5364   0.01291   0.00772  -0.0880   0.2926   1.0000
  10.000   1.5528   0.01338   0.00817  -0.0864   0.2832   1.0000
  10.250   1.5703   0.01384   0.00861  -0.0851   0.2735   1.0000
  10.500   1.5850   0.01445   0.00917  -0.0834   0.2618   1.0000
  10.750   1.5978   0.01518   0.00985  -0.0816   0.2488   1.0000
  11.000   1.6097   0.01601   0.01062  -0.0798   0.2362   1.0000
  11.250   1.6234   0.01676   0.01134  -0.0783   0.2263   1.0000
  11.500   1.6362   0.01760   0.01216  -0.0767   0.2172   1.0000
  12.000   1.6606   0.01944   0.01398  -0.0738   0.2010   1.0000
  12.250   1.6703   0.02057   0.01508  -0.0723   0.1935   1.0000
  12.500   1.6840   0.02147   0.01601  -0.0712   0.1883   1.0000
  12.750   1.6936   0.02267   0.01720  -0.0698   0.1820   1.0000
  13.000   1.7042   0.02383   0.01838  -0.0686   0.1765   1.0000
  13.250   1.7150   0.02501   0.01957  -0.0674   0.1712   1.0000
  13.500   1.7218   0.02651   0.02107  -0.0660   0.1658   1.0000
  13.750   1.7325   0.02774   0.02235  -0.0650   0.1615   1.0000
  14.000   1.7396   0.02926   0.02389  -0.0639   0.1561   1.0000
  14.250   1.7445   0.03102   0.02565  -0.0626   0.1507   1.0000
  14.500   1.7524   0.03255   0.02722  -0.0617   0.1452   1.0000
  14.750   1.7528   0.03477   0.02943  -0.0604   0.1381   1.0000
  15.000   1.7576   0.03669   0.03137  -0.0594   0.1314   1.0000
  15.250   1.7570   0.03916   0.03384  -0.0584   0.1241   1.0000
  15.500   1.7538   0.04192   0.03659  -0.0573   0.1152   1.0000
  15.750   1.7490   0.04494   0.03960  -0.0564   0.1061   1.0000
  16.000   1.7423   0.04824   0.04290  -0.0555   0.0986   1.0000
  16.250   1.7340   0.05175   0.04642  -0.0547   0.0925   1.0000
  16.500   1.7292   0.05500   0.04971  -0.0542   0.0883   1.0000
  16.750   1.7213   0.05864   0.05339  -0.0537   0.0844   1.0000
  17.000   1.7173   0.06192   0.05673  -0.0534   0.0814   1.0000
  17.250   1.7117   0.06541   0.06027  -0.0531   0.0786   1.0000
  17.500   1.7035   0.06926   0.06417  -0.0530   0.0758   1.0000
  17.750   1.6981   0.07284   0.06782  -0.0530   0.0732   1.0000
  18.000   1.6944   0.07627   0.07131  -0.0530   0.0706   1.0000
  18.250   1.6858   0.08031   0.07540  -0.0532   0.0679   1.0000
  18.500   1.6767   0.08449   0.07964  -0.0535   0.0652   1.0000
  18.750   1.6716   0.08820   0.08341  -0.0538   0.0622   1.0000
  19.000   1.6605   0.09273   0.08797  -0.0543   0.0585   1.0000
  19.250   1.6526   0.09683   0.09212  -0.0549   0.0544   1.0000
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