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GOE 515 AIRFOIL (goe515-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 515 AIRFOIL (goe515-il)
Reynolds number: 1,000,000
Max Cl/Cd: 119.03 at α=2.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe515-il-1000000.txt
Download as CSV file: xf-goe515-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 515 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
  ------ -------- --------- --------- -------- -------- --------
 -13.750  -0.6516   0.10962   0.10785  -0.0233   1.0000   0.0113
 -13.500  -0.7848   0.07999   0.07802  -0.0402   1.0000   0.0106
 -13.250  -0.8572   0.06496   0.06292  -0.0508   1.0000   0.0103
 -13.000  -1.0298   0.03236   0.02965  -0.0707   1.0000   0.0091
 -12.750  -1.0260   0.02984   0.02697  -0.0695   1.0000   0.0093
 -12.500  -1.0206   0.02773   0.02469  -0.0677   1.0000   0.0095
 -12.250  -1.0096   0.02636   0.02320  -0.0661   1.0000   0.0097
 -12.000  -1.0004   0.02486   0.02155  -0.0640   1.0000   0.0100
 -11.750  -0.9901   0.02356   0.02011  -0.0618   1.0000   0.0102
 -11.500  -0.9782   0.02249   0.01891  -0.0597   1.0000   0.0105
 -11.250  -0.9659   0.02151   0.01779  -0.0575   1.0000   0.0107
 -11.000  -0.9524   0.02068   0.01683  -0.0553   1.0000   0.0109
 -10.750  -0.9357   0.01898   0.01493  -0.0544   0.9992   0.0115
 -10.500  -0.9060   0.01804   0.01391  -0.0556   0.9976   0.0122
 -10.250  -0.8745   0.01746   0.01327  -0.0569   0.9961   0.0129
 -10.000  -0.8427   0.01677   0.01248  -0.0582   0.9946   0.0135
  -9.750  -0.8120   0.01622   0.01181  -0.0592   0.9928   0.0141
  -9.500  -0.7840   0.01513   0.01059  -0.0599   0.9901   0.0151
  -9.250  -0.7524   0.01459   0.01001  -0.0610   0.9880   0.0160
  -9.000  -0.7189   0.01423   0.00961  -0.0624   0.9862   0.0171
  -8.750  -0.6847   0.01383   0.00914  -0.0639   0.9847   0.0180
  -8.500  -0.6512   0.01316   0.00838  -0.0655   0.9834   0.0194
  -8.250  -0.6218   0.01281   0.00803  -0.0660   0.9799   0.0207
  -8.000  -0.5901   0.01251   0.00770  -0.0669   0.9772   0.0220
  -7.750  -0.5565   0.01225   0.00738  -0.0682   0.9751   0.0231
  -7.500  -0.5244   0.01166   0.00669  -0.0693   0.9727   0.0243
  -7.250  -0.4916   0.01112   0.00614  -0.0706   0.9705   0.0262
  -7.000  -0.4635   0.01087   0.00585  -0.0707   0.9649   0.0276
  -6.750  -0.4336   0.01058   0.00552  -0.0711   0.9599   0.0289
  -6.500  -0.4016   0.01034   0.00522  -0.0720   0.9559   0.0298
  -6.250  -0.3772   0.00983   0.00463  -0.0712   0.9475   0.0314
  -6.000  -0.3492   0.00941   0.00416  -0.0712   0.9414   0.0333
  -5.750  -0.3236   0.00915   0.00386  -0.0707   0.9328   0.0348
  -5.250  -0.2700   0.00874   0.00334  -0.0700   0.9172   0.0376
  -5.000  -0.2437   0.00845   0.00298  -0.0696   0.9098   0.0397
  -4.750  -0.2180   0.00817   0.00267  -0.0690   0.9012   0.0429
  -4.500  -0.1914   0.00798   0.00245  -0.0687   0.8938   0.0460
  -4.250  -0.1654   0.00775   0.00222  -0.0682   0.8859   0.0535
  -4.000  -0.1391   0.00755   0.00206  -0.0678   0.8788   0.0688
  -3.750  -0.1123   0.00745   0.00200  -0.0674   0.8713   0.0811
  -3.500  -0.0853   0.00737   0.00192  -0.0671   0.8647   0.0885
  -3.250  -0.0581   0.00733   0.00186  -0.0669   0.8576   0.0935
  -3.000  -0.0309   0.00732   0.00178  -0.0666   0.8503   0.0963
  -2.750  -0.0047   0.00720   0.00166  -0.0661   0.8405   0.1021
  -2.500   0.0217   0.00715   0.00158  -0.0657   0.8293   0.1060
  -2.250   0.0485   0.00713   0.00149  -0.0652   0.8196   0.1086
  -2.000   0.0754   0.00706   0.00140  -0.0649   0.8117   0.1111
  -1.750   0.1020   0.00697   0.00131  -0.0646   0.8049   0.1170
  -1.500   0.1291   0.00690   0.00124  -0.0643   0.7976   0.1216
  -1.250   0.1561   0.00688   0.00118  -0.0640   0.7908   0.1252
  -1.000   0.1829   0.00676   0.00112  -0.0637   0.7831   0.1341
  -0.750   0.2096   0.00672   0.00106  -0.0633   0.7757   0.1418
  -0.500   0.2364   0.00661   0.00102  -0.0630   0.7679   0.1573
  -0.250   0.2626   0.00649   0.00100  -0.0626   0.7601   0.1928
   0.000   0.2887   0.00638   0.00098  -0.0621   0.7499   0.2313
   0.250   0.3146   0.00626   0.00097  -0.0616   0.7379   0.2723
   0.500   0.3397   0.00609   0.00096  -0.0610   0.7260   0.3379
   0.750   0.3621   0.00569   0.00097  -0.0600   0.7138   0.4977
   1.000   0.3765   0.00454   0.00107  -0.0569   0.7011   0.9160
   1.250   0.4424   0.00467   0.00119  -0.0653   0.6821   0.9712
   1.500   0.4772   0.00483   0.00127  -0.0666   0.6626   0.9831
   1.750   0.5212   0.00498   0.00133  -0.0702   0.6441   0.9893
   2.000   0.5619   0.00512   0.00140  -0.0730   0.6253   0.9948
   2.250   0.6126   0.00526   0.00144  -0.0781   0.6009   0.9999
   2.500   0.6367   0.00538   0.00149  -0.0772   0.5790   1.0000
   2.750   0.6594   0.00554   0.00154  -0.0761   0.5495   1.0000
   3.000   0.6804   0.00582   0.00163  -0.0747   0.4995   1.0000
   3.250   0.7005   0.00618   0.00176  -0.0731   0.4462   1.0000
   3.500   0.7215   0.00650   0.00190  -0.0717   0.4058   1.0000
   3.750   0.7437   0.00676   0.00204  -0.0706   0.3768   1.0000
   4.000   0.7655   0.00704   0.00220  -0.0693   0.3460   1.0000
   4.250   0.7870   0.00734   0.00237  -0.0681   0.3126   1.0000
   4.500   0.8074   0.00773   0.00256  -0.0667   0.2692   1.0000
   4.750   0.8249   0.00835   0.00285  -0.0648   0.1994   1.0000
   5.000   0.8436   0.00887   0.00316  -0.0631   0.1561   1.0000
   5.250   0.8647   0.00922   0.00341  -0.0618   0.1349   1.0000
   5.500   0.8867   0.00950   0.00364  -0.0606   0.1211   1.0000
   5.750   0.9087   0.00978   0.00387  -0.0594   0.1079   1.0000
   6.000   0.9302   0.01010   0.00412  -0.0582   0.0913   1.0000
   6.250   0.9498   0.01057   0.00443  -0.0567   0.0647   1.0000
   6.500   0.9701   0.01098   0.00476  -0.0553   0.0498   1.0000
   6.750   0.9905   0.01138   0.00511  -0.0539   0.0387   1.0000
   7.000   1.0103   0.01184   0.00551  -0.0524   0.0284   1.0000
   7.250   1.0304   0.01227   0.00591  -0.0509   0.0226   1.0000
   7.500   1.0502   0.01274   0.00638  -0.0494   0.0193   1.0000
   7.750   1.0711   0.01309   0.00675  -0.0481   0.0177   1.0000
   8.000   1.0905   0.01358   0.00724  -0.0466   0.0160   1.0000
   8.250   1.1088   0.01415   0.00788  -0.0448   0.0149   1.0000
   8.500   1.1289   0.01454   0.00831  -0.0434   0.0142   1.0000
   8.750   1.1482   0.01499   0.00880  -0.0419   0.0135   1.0000
   9.000   1.1668   0.01548   0.00932  -0.0404   0.0128   1.0000
   9.250   1.1830   0.01614   0.01002  -0.0384   0.0121   1.0000
   9.500   1.1953   0.01705   0.01103  -0.0358   0.0114   1.0000
   9.750   1.2142   0.01746   0.01147  -0.0343   0.0110   1.0000
  10.000   1.2302   0.01804   0.01212  -0.0324   0.0107   1.0000
  10.250   1.2452   0.01864   0.01277  -0.0303   0.0102   1.0000
  10.500   1.2579   0.01922   0.01340  -0.0278   0.0099   1.0000
  10.750   1.2693   0.01987   0.01410  -0.0252   0.0096   1.0000
  11.000   1.2803   0.02059   0.01488  -0.0226   0.0093   1.0000
  11.250   1.2890   0.02149   0.01585  -0.0199   0.0090   1.0000
  11.500   1.2912   0.02292   0.01737  -0.0165   0.0088   1.0000
  11.750   1.2925   0.02453   0.01912  -0.0132   0.0085   1.0000
  12.000   1.3016   0.02559   0.02027  -0.0111   0.0084   1.0000
  12.250   1.3122   0.02653   0.02130  -0.0093   0.0083   1.0000
  12.500   1.3214   0.02762   0.02247  -0.0075   0.0081   1.0000
  12.750   1.3283   0.02895   0.02391  -0.0056   0.0079   1.0000
  13.000   1.3344   0.03038   0.02545  -0.0038   0.0077   1.0000
  13.250   1.3388   0.03202   0.02719  -0.0021   0.0076   1.0000
  13.500   1.3487   0.03315   0.02839  -0.0011   0.0074   1.0000
  13.750   1.3519   0.03500   0.03034   0.0003   0.0072   1.0000
  14.000   1.3547   0.03696   0.03240   0.0014   0.0071   1.0000
  14.250   1.3571   0.03900   0.03454   0.0023   0.0070   1.0000
  14.500   1.3587   0.04123   0.03685   0.0030   0.0068   1.0000
  14.750   1.3569   0.04391   0.03966   0.0035   0.0068   1.0000
  15.000   1.3533   0.04694   0.04280   0.0037   0.0067   1.0000
  15.250   1.3513   0.04991   0.04585   0.0036   0.0066   1.0000
  15.500   1.3391   0.05429   0.05036   0.0031   0.0064   1.0000
  15.750   1.3277   0.05883   0.05504   0.0021   0.0063   1.0000
  16.000   1.3207   0.06305   0.05940   0.0009   0.0064   1.0000
  16.250   1.3034   0.06897   0.06547  -0.0011   0.0063   1.0000
  16.500   1.2927   0.07427   0.07091  -0.0033   0.0063   1.0000
  16.750   1.2639   0.08270   0.07954  -0.0070   0.0062   1.0000
  17.000   1.2444   0.09006   0.08705  -0.0105   0.0062   1.0000
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