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GOE 648 AIRFOIL (goe648-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 648 AIRFOIL (goe648-il)
Reynolds number: 1,000,000
Max Cl/Cd: 101.91 at α=6.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe648-il-1000000-n5.txt
Download as CSV file: xf-goe648-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 648 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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -18.250  -0.8354   0.09913   0.09631  -0.0609   1.0000   0.0149
 -18.000  -0.9304   0.08061   0.07753  -0.0721   1.0000   0.0146
 -17.750  -1.0244   0.06337   0.05998  -0.0828   1.0000   0.0143
 -17.500  -1.0788   0.05212   0.04849  -0.0900   1.0000   0.0142
 -17.250  -1.1111   0.04444   0.04063  -0.0950   1.0000   0.0142
 -17.000  -1.1307   0.03908   0.03513  -0.0980   1.0000   0.0143
 -16.750  -1.1435   0.03508   0.03102  -0.0998   1.0000   0.0144
 -16.500  -1.1530   0.03197   0.02780  -0.1004   1.0000   0.0146
 -16.250  -1.1610   0.02958   0.02533  -0.0999   1.0000   0.0147
 -16.000  -1.1698   0.02770   0.02337  -0.0981   1.0000   0.0149
 -15.750  -1.1713   0.02624   0.02182  -0.0966   0.9996   0.0151
 -15.500  -1.1543   0.02495   0.02046  -0.0974   0.9979   0.0154
 -15.250  -1.1356   0.02390   0.01934  -0.0978   0.9956   0.0157
 -15.000  -1.1149   0.02302   0.01838  -0.0981   0.9932   0.0161
 -14.750  -1.0993   0.02218   0.01747  -0.0972   0.9899   0.0164
 -14.500  -1.0778   0.02131   0.01657  -0.0972   0.9871   0.0169
 -14.250  -1.0532   0.02053   0.01575  -0.0975   0.9849   0.0173
 -14.000  -1.0265   0.01983   0.01500  -0.0981   0.9832   0.0180
 -13.750  -0.9986   0.01918   0.01431  -0.0989   0.9818   0.0184
 -13.500  -0.9781   0.01864   0.01372  -0.0980   0.9779   0.0190
 -13.250  -0.9540   0.01806   0.01309  -0.0977   0.9748   0.0195
 -13.000  -0.9272   0.01747   0.01249  -0.0980   0.9724   0.0201
 -12.750  -0.8986   0.01693   0.01191  -0.0986   0.9706   0.0207
 -12.500  -0.8684   0.01643   0.01138  -0.0994   0.9691   0.0214
 -12.250  -0.8463   0.01601   0.01091  -0.0984   0.9631   0.0219
 -12.000  -0.8154   0.01555   0.01041  -0.0993   0.9588   0.0224
 -11.500  -0.7504   0.01456   0.00938  -0.1016   0.9484   0.0238
 -11.250  -0.7172   0.01416   0.00894  -0.1028   0.9431   0.0247
 -11.000  -0.6845   0.01378   0.00851  -0.1039   0.9373   0.0254
 -10.750  -0.6546   0.01344   0.00811  -0.1044   0.9288   0.0259
 -10.500  -0.6248   0.01303   0.00767  -0.1049   0.9206   0.0267
 -10.250  -0.5969   0.01270   0.00730  -0.1049   0.9100   0.0274
 -10.000  -0.5701   0.01241   0.00696  -0.1047   0.8997   0.0282
  -9.750  -0.5434   0.01217   0.00665  -0.1044   0.8887   0.0290
  -9.500  -0.5183   0.01195   0.00636  -0.1037   0.8773   0.0296
  -9.250  -0.4940   0.01168   0.00604  -0.1029   0.8666   0.0304
  -9.000  -0.4700   0.01145   0.00575  -0.1020   0.8533   0.0313
  -8.750  -0.4460   0.01125   0.00549  -0.1011   0.8398   0.0322
  -8.500  -0.4218   0.01108   0.00524  -0.1002   0.8275   0.0331
  -8.250  -0.3973   0.01092   0.00502  -0.0993   0.8177   0.0338
  -8.000  -0.3730   0.01069   0.00476  -0.0985   0.8076   0.0350
  -7.750  -0.3487   0.01052   0.00454  -0.0976   0.7972   0.0362
  -7.500  -0.3239   0.01036   0.00433  -0.0968   0.7862   0.0374
  -7.250  -0.2990   0.01020   0.00413  -0.0959   0.7757   0.0388
  -7.000  -0.2745   0.01004   0.00393  -0.0951   0.7643   0.0406
  -6.750  -0.2494   0.00989   0.00376  -0.0943   0.7530   0.0425
  -6.500  -0.2247   0.00976   0.00358  -0.0934   0.7400   0.0448
  -6.250  -0.2003   0.00965   0.00342  -0.0925   0.7240   0.0475
  -6.000  -0.1758   0.00956   0.00327  -0.0916   0.7073   0.0502
  -5.750  -0.1512   0.00947   0.00314  -0.0907   0.6908   0.0535
  -5.500  -0.1270   0.00943   0.00302  -0.0897   0.6698   0.0565
  -5.250  -0.1032   0.00940   0.00292  -0.0887   0.6459   0.0601
  -5.000  -0.0788   0.00939   0.00282  -0.0878   0.6252   0.0630
  -4.750  -0.0541   0.00935   0.00273  -0.0869   0.6075   0.0661
  -4.500  -0.0287   0.00933   0.00265  -0.0862   0.5925   0.0687
  -4.250  -0.0033   0.00930   0.00256  -0.0855   0.5798   0.0710
  -4.000   0.0223   0.00925   0.00247  -0.0848   0.5667   0.0739
  -3.750   0.0480   0.00922   0.00240  -0.0841   0.5532   0.0766
  -3.500   0.0736   0.00922   0.00234  -0.0834   0.5395   0.0787
  -3.250   0.0987   0.00919   0.00226  -0.0827   0.5246   0.0823
  -3.000   0.1243   0.00917   0.00220  -0.0820   0.5107   0.0854
  -2.750   0.1500   0.00916   0.00215  -0.0813   0.4971   0.0886
  -2.500   0.1751   0.00914   0.00210  -0.0806   0.4821   0.0950
  -2.250   0.1997   0.00911   0.00205  -0.0798   0.4650   0.1077
  -2.000   0.2237   0.00908   0.00202  -0.0789   0.4450   0.1287
  -1.750   0.2469   0.00911   0.00201  -0.0778   0.4190   0.1495
  -1.500   0.2697   0.00919   0.00202  -0.0767   0.3870   0.1694
  -1.250   0.2929   0.00926   0.00204  -0.0757   0.3637   0.1908
  -1.000   0.3168   0.00928   0.00207  -0.0748   0.3475   0.2143
  -0.750   0.3415   0.00928   0.00209  -0.0740   0.3364   0.2378
  -0.500   0.3664   0.00928   0.00211  -0.0732   0.3282   0.2616
  -0.250   0.3913   0.00927   0.00214  -0.0725   0.3207   0.2860
   0.000   0.4159   0.00928   0.00218  -0.0717   0.3134   0.3105
   0.250   0.4409   0.00923   0.00221  -0.0710   0.3087   0.3439
   0.500   0.4657   0.00919   0.00224  -0.0703   0.3045   0.3773
   0.750   0.4897   0.00914   0.00230  -0.0694   0.2996   0.4221
   1.000   0.5133   0.00910   0.00237  -0.0685   0.2945   0.4735
   1.250   0.5380   0.00906   0.00244  -0.0677   0.2912   0.5137
   1.500   0.5630   0.00908   0.00250  -0.0670   0.2872   0.5382
   1.750   0.5875   0.00912   0.00258  -0.0661   0.2829   0.5632
   2.000   0.6116   0.00917   0.00266  -0.0653   0.2786   0.5872
   2.250   0.6351   0.00914   0.00274  -0.0642   0.2760   0.6268
   2.500   0.6579   0.00909   0.00284  -0.0631   0.2735   0.6759
   2.750   0.6805   0.00907   0.00294  -0.0619   0.2706   0.7193
   3.000   0.7034   0.00910   0.00303  -0.0607   0.2671   0.7526
   3.250   0.7260   0.00915   0.00314  -0.0595   0.2640   0.7790
   3.500   0.7481   0.00921   0.00324  -0.0582   0.2607   0.8053
   3.750   0.7696   0.00920   0.00335  -0.0567   0.2585   0.8402
   4.000   0.8050   0.00914   0.00352  -0.0582   0.2553   0.9181
   4.250   0.9089   0.00949   0.00384  -0.0749   0.2490   0.9795
   4.500   0.9408   0.00971   0.00402  -0.0758   0.2448   0.9994
   4.750   0.9657   0.00985   0.00414  -0.0752   0.2420   1.0000
   5.000   0.9877   0.00997   0.00426  -0.0739   0.2392   1.0000
   5.250   1.0094   0.01010   0.00438  -0.0726   0.2363   1.0000
   5.500   1.0307   0.01026   0.00451  -0.0713   0.2331   1.0000
   5.750   1.0516   0.01043   0.00466  -0.0699   0.2295   1.0000
   6.000   1.0720   0.01059   0.00481  -0.0684   0.2262   1.0000
   6.250   1.0918   0.01073   0.00495  -0.0667   0.2226   1.0000
   6.500   1.1108   0.01090   0.00509  -0.0650   0.2184   1.0000
   6.750   1.1289   0.01112   0.00527  -0.0631   0.2129   1.0000
   7.000   1.1486   0.01130   0.00544  -0.0615   0.2083   1.0000
   7.250   1.1681   0.01150   0.00563  -0.0599   0.2037   1.0000
   7.500   1.1871   0.01174   0.00584  -0.0583   0.1989   1.0000
   7.750   1.2068   0.01196   0.00606  -0.0569   0.1946   1.0000
   8.000   1.2266   0.01220   0.00628  -0.0554   0.1900   1.0000
   8.250   1.2454   0.01248   0.00654  -0.0539   0.1850   1.0000
   8.500   1.2651   0.01275   0.00680  -0.0526   0.1811   1.0000
   8.750   1.2847   0.01302   0.00707  -0.0512   0.1770   1.0000
   9.000   1.3030   0.01336   0.00738  -0.0497   0.1717   1.0000
   9.250   1.3218   0.01369   0.00770  -0.0484   0.1672   1.0000
   9.500   1.3407   0.01402   0.00803  -0.0470   0.1629   1.0000
   9.750   1.3587   0.01440   0.00840  -0.0456   0.1585   1.0000
  10.000   1.3767   0.01479   0.00879  -0.0442   0.1548   1.0000
  10.250   1.3958   0.01514   0.00915  -0.0431   0.1522   1.0000
  10.500   1.4141   0.01553   0.00955  -0.0418   0.1489   1.0000
  10.750   1.4316   0.01597   0.00999  -0.0405   0.1459   1.0000
  11.000   1.4482   0.01647   0.01049  -0.0391   0.1423   1.0000
  11.250   1.4663   0.01689   0.01094  -0.0380   0.1397   1.0000
  11.500   1.4833   0.01738   0.01144  -0.0367   0.1363   1.0000
  11.750   1.4987   0.01798   0.01204  -0.0354   0.1323   1.0000
  12.000   1.5140   0.01860   0.01266  -0.0340   0.1285   1.0000
  12.250   1.5303   0.01916   0.01325  -0.0329   0.1258   1.0000
  12.500   1.5445   0.01987   0.01396  -0.0316   0.1212   1.0000
  12.750   1.5573   0.02068   0.01477  -0.0302   0.1170   1.0000
  13.000   1.5697   0.02153   0.01561  -0.0288   0.1107   1.0000
  13.250   1.5801   0.02254   0.01661  -0.0273   0.1051   1.0000
  13.500   1.5885   0.02371   0.01776  -0.0258   0.0973   1.0000
  13.750   1.5976   0.02486   0.01891  -0.0245   0.0915   1.0000
  14.000   1.5997   0.02655   0.02056  -0.0227   0.0806   1.0000
  14.250   1.5998   0.02847   0.02243  -0.0210   0.0708   1.0000
  14.500   1.6001   0.03045   0.02440  -0.0195   0.0638   1.0000
  14.750   1.6005   0.03251   0.02648  -0.0183   0.0590   1.0000
  15.000   1.6031   0.03448   0.02848  -0.0173   0.0560   1.0000
  15.250   1.6048   0.03660   0.03065  -0.0165   0.0537   1.0000
  15.500   1.6085   0.03862   0.03272  -0.0159   0.0520   1.0000
  15.750   1.6121   0.04073   0.03489  -0.0154   0.0509   1.0000
  16.000   1.6117   0.04330   0.03752  -0.0150   0.0492   1.0000
  16.250   1.6129   0.04578   0.04006  -0.0148   0.0486   1.0000
  16.500   1.6115   0.04860   0.04295  -0.0147   0.0475   1.0000
  16.750   1.6107   0.05145   0.04588  -0.0148   0.0467   1.0000
  17.000   1.6097   0.05437   0.04888  -0.0149   0.0459   1.0000
  17.250   1.6075   0.05748   0.05207  -0.0152   0.0455   1.0000
  17.500   1.6027   0.06098   0.05565  -0.0156   0.0448   1.0000
  17.750   1.5956   0.06482   0.05959  -0.0162   0.0441   1.0000
  18.000   1.5861   0.06903   0.06389  -0.0170   0.0434   1.0000
  18.250   1.5759   0.07339   0.06835  -0.0179   0.0430   1.0000
  18.500   1.5620   0.07836   0.07341  -0.0191   0.0424   1.0000
  18.750   1.5474   0.08351   0.07868  -0.0205   0.0421   1.0000
  19.000   1.5294   0.08921   0.08448  -0.0221   0.0415   1.0000
  19.250   1.5116   0.09499   0.09037  -0.0238   0.0408   1.0000
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