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GOE 404 AIRFOIL (goe404-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 404 AIRFOIL (goe404-il)
Reynolds number: 1,000,000
Max Cl/Cd: 121.56 at α=6.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe404-il-1000000.txt
Download as CSV file: xf-goe404-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 404 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
  ------ -------- --------- --------- -------- -------- --------
 -13.500  -0.3548   0.14871   0.14688  -0.0130   1.0000   0.0250
 -13.250  -0.3664   0.14075   0.13891  -0.0184   1.0000   0.0263
 -12.000  -0.7735   0.03241   0.02955  -0.0918   0.9938   0.0273
 -11.750  -0.7511   0.02975   0.02671  -0.0944   0.9901   0.0275
 -11.500  -0.7266   0.02778   0.02459  -0.0962   0.9857   0.0277
 -11.250  -0.7004   0.02603   0.02269  -0.0979   0.9820   0.0280
 -11.000  -0.6781   0.02444   0.02094  -0.0984   0.9755   0.0281
 -10.750  -0.6548   0.02300   0.01934  -0.0987   0.9693   0.0283
 -10.500  -0.6336   0.02178   0.01797  -0.0983   0.9614   0.0285
 -10.250  -0.6122   0.02069   0.01674  -0.0976   0.9527   0.0286
 -10.000  -0.5913   0.01973   0.01564  -0.0966   0.9426   0.0288
  -9.750  -0.5694   0.01885   0.01462  -0.0957   0.9329   0.0290
  -9.500  -0.5467   0.01805   0.01368  -0.0949   0.9227   0.0292
  -9.250  -0.5231   0.01732   0.01282  -0.0942   0.9124   0.0293
  -9.000  -0.4992   0.01667   0.01204  -0.0934   0.9007   0.0295
  -8.750  -0.4743   0.01608   0.01133  -0.0928   0.8883   0.0297
  -8.500  -0.4490   0.01556   0.01069  -0.0922   0.8758   0.0298
  -8.250  -0.4234   0.01512   0.01012  -0.0916   0.8616   0.0300
  -8.000  -0.3997   0.01412   0.00896  -0.0909   0.8446   0.0303
  -7.750  -0.3749   0.01346   0.00818  -0.0902   0.8243   0.0306
  -7.500  -0.3492   0.01302   0.00763  -0.0897   0.7995   0.0310
  -7.250  -0.3233   0.01269   0.00717  -0.0891   0.7740   0.0313
  -7.000  -0.2970   0.01241   0.00675  -0.0886   0.7517   0.0316
  -6.750  -0.2702   0.01215   0.00639  -0.0882   0.7338   0.0321
  -6.500  -0.2430   0.01189   0.00605  -0.0878   0.7197   0.0325
  -6.250  -0.2157   0.01164   0.00570  -0.0875   0.7078   0.0329
  -6.000  -0.1882   0.01139   0.00536  -0.0871   0.6965   0.0333
  -5.750  -0.1605   0.01116   0.00506  -0.0869   0.6865   0.0336
  -5.500  -0.1327   0.01096   0.00479  -0.0866   0.6763   0.0339
  -5.250  -0.1055   0.01055   0.00432  -0.0862   0.6678   0.0346
  -5.000  -0.0778   0.01028   0.00402  -0.0860   0.6591   0.0352
  -4.750  -0.0499   0.01009   0.00378  -0.0857   0.6510   0.0359
  -4.500  -0.0217   0.00990   0.00356  -0.0855   0.6426   0.0367
  -4.250   0.0063   0.00977   0.00336  -0.0852   0.6335   0.0375
  -4.000   0.0347   0.00960   0.00316  -0.0851   0.6252   0.0383
  -3.750   0.0624   0.00940   0.00293  -0.0848   0.6159   0.0399
  -3.500   0.0909   0.00925   0.00277  -0.0846   0.6078   0.0415
  -3.250   0.1189   0.00911   0.00260  -0.0844   0.5982   0.0440
  -3.000   0.1472   0.00897   0.00246  -0.0842   0.5891   0.0483
  -2.750   0.1752   0.00888   0.00239  -0.0840   0.5783   0.0572
  -2.500   0.2038   0.00887   0.00238  -0.0838   0.5671   0.0654
  -2.250   0.2322   0.00891   0.00240  -0.0837   0.5541   0.0706
  -2.000   0.2604   0.00895   0.00238  -0.0835   0.5389   0.0740
  -1.750   0.2886   0.00900   0.00240  -0.0833   0.5222   0.0770
  -1.500   0.3168   0.00908   0.00241  -0.0831   0.5047   0.0795
  -1.250   0.3447   0.00914   0.00239  -0.0829   0.4871   0.0816
  -1.000   0.3724   0.00917   0.00237  -0.0826   0.4709   0.0843
  -0.750   0.4003   0.00925   0.00241  -0.0824   0.4568   0.0867
  -0.500   0.4282   0.00933   0.00242  -0.0822   0.4434   0.0886
   0.000   0.4837   0.00938   0.00238  -0.0818   0.4211   0.0932
   0.250   0.5113   0.00945   0.00242  -0.0816   0.4119   0.0957
   0.500   0.5397   0.00947   0.00243  -0.0815   0.4050   0.0983
   0.750   0.5676   0.00956   0.00248  -0.0813   0.3973   0.1002
   1.000   0.5954   0.00953   0.00243  -0.0812   0.3915   0.1033
   1.250   0.6236   0.00952   0.00243  -0.0810   0.3861   0.1060
   1.500   0.6513   0.00957   0.00246  -0.0808   0.3795   0.1087
   1.750   0.6793   0.00962   0.00249  -0.0807   0.3740   0.1113
   2.000   0.7075   0.00963   0.00250  -0.0806   0.3694   0.1144
   2.250   0.7354   0.00965   0.00253  -0.0804   0.3647   0.1202
   2.500   0.7629   0.00973   0.00259  -0.0802   0.3595   0.1256
   2.750   0.7909   0.00973   0.00265  -0.0801   0.3560   0.1397
   3.000   0.8187   0.00965   0.00273  -0.0800   0.3523   0.2017
   3.250   0.8379   0.00835   0.00295  -0.0788   0.3484   0.8011
   3.500   0.8851   0.00822   0.00312  -0.0827   0.3415   1.0000
   3.750   0.9118   0.00831   0.00319  -0.0823   0.3378   1.0000
   4.000   0.9385   0.00841   0.00327  -0.0819   0.3342   1.0000
   4.250   0.9649   0.00854   0.00336  -0.0815   0.3298   1.0000
   4.500   0.9907   0.00872   0.00348  -0.0810   0.3240   1.0000
   4.750   1.0177   0.00882   0.00357  -0.0807   0.3202   1.0000
   5.000   1.0445   0.00894   0.00366  -0.0804   0.3154   1.0000
   5.250   1.0706   0.00911   0.00379  -0.0800   0.3099   1.0000
   5.500   1.0969   0.00926   0.00392  -0.0797   0.3052   1.0000
   5.750   1.1238   0.00938   0.00403  -0.0794   0.3005   1.0000
   6.000   1.1499   0.00956   0.00417  -0.0790   0.2943   1.0000
   6.250   1.1759   0.00974   0.00432  -0.0787   0.2884   1.0000
   6.500   1.2022   0.00989   0.00446  -0.0784   0.2813   1.0000
   6.750   1.2275   0.01013   0.00463  -0.0779   0.2726   1.0000
   7.000   1.2529   0.01035   0.00481  -0.0775   0.2621   1.0000
   7.250   1.2775   0.01062   0.00502  -0.0770   0.2485   1.0000
   7.500   1.3000   0.01106   0.00532  -0.0762   0.2275   1.0000
   7.750   1.3193   0.01173   0.00578  -0.0749   0.1951   1.0000
   8.000   1.3397   0.01229   0.00622  -0.0738   0.1773   1.0000
   8.250   1.3615   0.01274   0.00661  -0.0729   0.1678   1.0000
   8.500   1.3839   0.01313   0.00696  -0.0721   0.1621   1.0000
   8.750   1.4056   0.01354   0.00735  -0.0713   0.1567   1.0000
   9.000   1.4291   0.01381   0.00763  -0.0706   0.1543   1.0000
   9.250   1.4517   0.01413   0.00796  -0.0699   0.1515   1.0000
   9.500   1.4732   0.01450   0.00832  -0.0690   0.1485   1.0000
   9.750   1.4936   0.01492   0.00874  -0.0679   0.1451   1.0000
  10.000   1.5140   0.01529   0.00912  -0.0669   0.1426   1.0000
  10.250   1.5347   0.01557   0.00944  -0.0658   0.1410   1.0000
  10.500   1.5541   0.01591   0.00980  -0.0646   0.1390   1.0000
  10.750   1.5725   0.01632   0.01021  -0.0632   0.1364   1.0000
  11.000   1.5893   0.01681   0.01071  -0.0618   0.1335   1.0000
  11.250   1.6046   0.01740   0.01130  -0.0601   0.1303   1.0000
  11.500   1.6240   0.01776   0.01171  -0.0591   0.1290   1.0000
  11.750   1.6423   0.01820   0.01219  -0.0580   0.1270   1.0000
  12.000   1.6593   0.01873   0.01274  -0.0568   0.1244   1.0000
  12.250   1.6742   0.01940   0.01341  -0.0554   0.1212   1.0000
  12.500   1.6880   0.02016   0.01418  -0.0540   0.1180   1.0000
  12.750   1.7049   0.02073   0.01480  -0.0530   0.1154   1.0000
  13.000   1.7186   0.02154   0.01561  -0.0517   0.1109   1.0000
  13.250   1.7298   0.02254   0.01660  -0.0503   0.1057   1.0000
  13.500   1.7390   0.02372   0.01776  -0.0489   0.0982   1.0000
  13.750   1.7445   0.02524   0.01924  -0.0473   0.0886   1.0000
  14.000   1.7435   0.02734   0.02128  -0.0455   0.0771   1.0000
  14.250   1.7417   0.02969   0.02361  -0.0441   0.0698   1.0000
  14.500   1.7424   0.03193   0.02588  -0.0430   0.0663   1.0000
  14.750   1.7423   0.03439   0.02837  -0.0422   0.0636   1.0000
  15.000   1.7453   0.03662   0.03066  -0.0416   0.0623   1.0000
  15.250   1.7463   0.03910   0.03321  -0.0411   0.0613   1.0000
  15.500   1.7451   0.04186   0.03605  -0.0407   0.0603   1.0000
  15.750   1.7424   0.04486   0.03911  -0.0404   0.0594   1.0000
  16.000   1.7378   0.04812   0.04244  -0.0402   0.0585   1.0000
  16.250   1.7323   0.05156   0.04596  -0.0401   0.0577   1.0000
  16.500   1.7242   0.05541   0.04990  -0.0402   0.0569   1.0000
  16.750   1.7195   0.05890   0.05348  -0.0404   0.0566   1.0000
  17.000   1.7150   0.06245   0.05713  -0.0406   0.0563   1.0000
  17.250   1.7092   0.06622   0.06100  -0.0411   0.0559   1.0000
  17.500   1.7022   0.07019   0.06506  -0.0416   0.0555   1.0000
  17.750   1.6943   0.07434   0.06930  -0.0422   0.0551   1.0000
  18.000   1.6855   0.07866   0.07371  -0.0429   0.0547   1.0000
  18.250   1.6760   0.08311   0.07825  -0.0438   0.0543   1.0000
  18.500   1.6656   0.08769   0.08292  -0.0447   0.0539   1.0000
  18.750   1.6547   0.09240   0.08771  -0.0457   0.0534   1.0000
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