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GOE 14K AIRFOIL (goe14k-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 14K AIRFOIL (goe14k-il)
Reynolds number: 1,000,000
Max Cl/Cd: 98.09 at α=3°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe14k-il-1000000.txt
Download as CSV file: xf-goe14k-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 14K 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
  ------ -------- --------- --------- -------- -------- --------
 -15.750  -0.8322   0.08139   0.07921  -0.0786   0.9917   0.0095
 -15.500  -0.8791   0.06806   0.06574  -0.0873   0.9902   0.0095
 -15.250  -0.9112   0.05588   0.05336  -0.0976   0.9887   0.0095
 -15.000  -0.9486   0.04296   0.04004  -0.1109   0.9870   0.0094
 -14.750  -0.9460   0.03978   0.03676  -0.1138   0.9861   0.0097
 -14.500  -0.9605   0.03652   0.03331  -0.1123   0.9819   0.0096
 -14.250  -0.9514   0.03516   0.03192  -0.1120   0.9797   0.0100
 -14.000  -0.9648   0.03175   0.02820  -0.1100   0.9774   0.0097
 -13.750  -0.9502   0.03060   0.02697  -0.1098   0.9765   0.0100
 -13.500  -0.9284   0.02997   0.02628  -0.1103   0.9759   0.0104
 -13.250  -0.9335   0.02836   0.02451  -0.1060   0.9712   0.0104
 -13.000  -0.9260   0.02710   0.02312  -0.1037   0.9682   0.0106
 -12.750  -0.9135   0.02586   0.02173  -0.1022   0.9665   0.0107
 -12.500  -0.8929   0.02512   0.02088  -0.1019   0.9655   0.0113
 -12.250  -0.8765   0.02396   0.01958  -0.1010   0.9645   0.0113
 -12.000  -0.8726   0.02320   0.01871  -0.0968   0.9598   0.0115
 -11.750  -0.8651   0.02206   0.01740  -0.0936   0.9561   0.0119
 -11.500  -0.8490   0.02106   0.01629  -0.0922   0.9544   0.0121
 -11.250  -0.8285   0.02028   0.01546  -0.0915   0.9534   0.0128
 -11.000  -0.8033   0.01977   0.01491  -0.0916   0.9526   0.0134
 -10.750  -0.8033   0.01898   0.01399  -0.0861   0.9467   0.0134
 -10.500  -0.7831   0.01847   0.01342  -0.0850   0.9441   0.0139
 -10.250  -0.7582   0.01797   0.01284  -0.0848   0.9428   0.0145
 -10.000  -0.7328   0.01740   0.01218  -0.0847   0.9418   0.0148
  -9.750  -0.7129   0.01623   0.01089  -0.0837   0.9407   0.0159
  -9.500  -0.6867   0.01565   0.01028  -0.0838   0.9401   0.0166
  -9.250  -0.6589   0.01519   0.00977  -0.0843   0.9395   0.0172
  -9.000  -0.6540   0.01482   0.00933  -0.0794   0.9328   0.0177
  -8.750  -0.6291   0.01444   0.00890  -0.0790   0.9311   0.0183
  -8.500  -0.6040   0.01379   0.00816  -0.0788   0.9299   0.0195
  -8.250  -0.5766   0.01325   0.00761  -0.0790   0.9289   0.0209
  -8.000  -0.5470   0.01288   0.00720  -0.0798   0.9280   0.0225
  -7.750  -0.5164   0.01251   0.00678  -0.0807   0.9272   0.0234
  -7.500  -0.4854   0.01194   0.00620  -0.0817   0.9265   0.0261
  -7.250  -0.4702   0.01180   0.00605  -0.0791   0.9216   0.0275
  -7.000  -0.4436   0.01158   0.00579  -0.0790   0.9191   0.0292
  -6.750  -0.4141   0.01120   0.00543  -0.0797   0.9174   0.0329
  -6.500  -0.3814   0.01100   0.00522  -0.0810   0.9160   0.0354
  -6.250  -0.3476   0.01066   0.00486  -0.0826   0.9149   0.0385
  -6.000  -0.3116   0.01047   0.00470  -0.0848   0.9140   0.0420
  -5.750  -0.2744   0.01032   0.00453  -0.0872   0.9131   0.0442
  -5.500  -0.2363   0.00996   0.00414  -0.0899   0.9123   0.0478
  -5.250  -0.2299   0.00989   0.00406  -0.0851   0.9062   0.0496
  -5.000  -0.2005   0.00971   0.00387  -0.0857   0.9040   0.0521
  -4.750  -0.1675   0.00957   0.00372  -0.0871   0.9024   0.0544
  -4.500  -0.1309   0.00940   0.00353  -0.0893   0.9012   0.0555
  -4.250  -0.0920   0.00902   0.00312  -0.0922   0.9003   0.0604
  -4.000  -0.0528   0.00879   0.00289  -0.0951   0.8993   0.0639
  -3.750  -0.0129   0.00861   0.00269  -0.0982   0.8982   0.0669
  -3.500  -0.0083   0.00862   0.00269  -0.0929   0.8933   0.0681
  -3.250   0.0187   0.00845   0.00252  -0.0929   0.8907   0.0744
  -3.000   0.0494   0.00824   0.00238  -0.0938   0.8888   0.0881
  -2.750   0.0831   0.00771   0.00222  -0.0957   0.8873   0.1853
  -2.500   0.1182   0.00734   0.00212  -0.0978   0.8861   0.2623
  -2.250   0.1548   0.00709   0.00206  -0.1003   0.8849   0.3209
  -2.000   0.1934   0.00686   0.00202  -0.1032   0.8838   0.3805
  -1.750   0.1946   0.00681   0.00207  -0.0970   0.8795   0.4105
  -1.500   0.2156   0.00663   0.00205  -0.0957   0.8764   0.4612
  -1.250   0.2388   0.00627   0.00200  -0.0949   0.8733   0.5587
  -1.000   0.2502   0.00557   0.00195  -0.0914   0.8701   0.7546
  -0.750   0.3772   0.00586   0.00275  -0.1144   0.8739   0.9018
  -0.500   0.4149   0.00602   0.00290  -0.1167   0.8717   0.9125
  -0.250   0.4519   0.00617   0.00303  -0.1188   0.8697   0.9208
   0.000   0.4760   0.00642   0.00328  -0.1178   0.8668   0.9284
   0.250   0.4933   0.00669   0.00356  -0.1151   0.8617   0.9389
   0.500   0.5356   0.00680   0.00360  -0.1183   0.8535   0.9404
   0.750   0.5507   0.00698   0.00380  -0.1152   0.8472   0.9467
   1.000   0.5802   0.00713   0.00392  -0.1155   0.8412   0.9511
   1.250   0.6149   0.00730   0.00409  -0.1169   0.8348   0.9534
   1.500   0.6512   0.00747   0.00422  -0.1187   0.8252   0.9567
   1.750   0.6624   0.00765   0.00442  -0.1148   0.8163   0.9632
   2.000   0.6973   0.00771   0.00446  -0.1163   0.8040   0.9650
   2.250   0.7287   0.00777   0.00449  -0.1172   0.7943   0.9670
   2.500   0.7492   0.00791   0.00465  -0.1155   0.7837   0.9716
   2.750   0.7737   0.00801   0.00475  -0.1147   0.7698   0.9753
   3.000   0.7945   0.00810   0.00472  -0.1131   0.7312   0.9783
   3.250   0.7880   0.00883   0.00502  -0.1052   0.6335   0.9860
   3.500   0.7816   0.01003   0.00542  -0.0982   0.4626   0.9921
   3.750   0.7997   0.01079   0.00567  -0.0967   0.3558   0.9964
   4.000   0.8275   0.01132   0.00574  -0.0975   0.2544   1.0000
   4.250   0.8310   0.01190   0.00603  -0.0926   0.1933   1.0000
   4.500   0.8376   0.01238   0.00630  -0.0885   0.1493   1.0000
   4.750   0.8479   0.01276   0.00654  -0.0850   0.1177   1.0000
   5.000   0.8586   0.01317   0.00681  -0.0817   0.0891   1.0000
   5.250   0.8724   0.01346   0.00704  -0.0790   0.0771   1.0000
   5.500   0.8868   0.01372   0.00728  -0.0764   0.0690   1.0000
   5.750   0.9009   0.01400   0.00753  -0.0738   0.0630   1.0000
   6.000   0.9160   0.01426   0.00779  -0.0714   0.0585   1.0000
   6.250   0.9325   0.01447   0.00802  -0.0693   0.0555   1.0000
   6.500   0.9478   0.01476   0.00829  -0.0669   0.0510   1.0000
   6.750   0.9637   0.01502   0.00856  -0.0647   0.0468   1.0000
   7.000   0.9792   0.01531   0.00883  -0.0625   0.0418   1.0000
   7.250   0.9946   0.01562   0.00913  -0.0602   0.0372   1.0000
   7.500   1.0094   0.01598   0.00946  -0.0579   0.0325   1.0000
   7.750   1.0250   0.01633   0.00981  -0.0557   0.0289   1.0000
   8.000   1.0396   0.01674   0.01021  -0.0533   0.0265   1.0000
   8.250   1.0539   0.01718   0.01067  -0.0509   0.0239   1.0000
   8.500   1.0693   0.01754   0.01106  -0.0488   0.0226   1.0000
   8.750   1.0844   0.01794   0.01147  -0.0466   0.0213   1.0000
   9.000   1.0967   0.01857   0.01212  -0.0440   0.0196   1.0000
   9.250   1.1121   0.01895   0.01255  -0.0419   0.0188   1.0000
   9.500   1.1270   0.01939   0.01303  -0.0398   0.0179   1.0000
   9.750   1.1418   0.01985   0.01352  -0.0377   0.0172   1.0000
  10.000   1.1553   0.02042   0.01409  -0.0354   0.0161   1.0000
  10.250   1.1650   0.02125   0.01498  -0.0325   0.0153   1.0000
  10.500   1.1788   0.02179   0.01559  -0.0303   0.0150   1.0000
  10.750   1.1914   0.02244   0.01631  -0.0279   0.0147   1.0000
  11.000   1.2078   0.02278   0.01668  -0.0263   0.0139   1.0000
  11.250   1.2203   0.02342   0.01737  -0.0241   0.0135   1.0000
  11.500   1.2320   0.02413   0.01813  -0.0217   0.0131   1.0000
  11.750   1.2442   0.02478   0.01882  -0.0196   0.0128   1.0000
  12.000   1.2484   0.02608   0.02018  -0.0162   0.0121   1.0000
  12.250   1.2545   0.02723   0.02143  -0.0133   0.0118   1.0000
  12.500   1.2676   0.02785   0.02212  -0.0113   0.0117   1.0000
  12.750   1.2791   0.02860   0.02295  -0.0093   0.0113   1.0000
  13.000   1.2893   0.02946   0.02387  -0.0070   0.0111   1.0000
  13.250   1.3016   0.03014   0.02460  -0.0053   0.0105   1.0000
  13.500   1.3088   0.03123   0.02578  -0.0028   0.0105   1.0000
  13.750   1.3181   0.03217   0.02679  -0.0007   0.0103   1.0000
  14.000   1.3246   0.03334   0.02802   0.0017   0.0100   1.0000
  14.250   1.3274   0.03484   0.02963   0.0044   0.0099   1.0000
  14.500   1.3337   0.03603   0.03089   0.0065   0.0097   1.0000
  14.750   1.3305   0.03808   0.03303   0.0095   0.0093   1.0000
  15.000   1.3277   0.04016   0.03524   0.0123   0.0092   1.0000
  15.250   1.3272   0.04208   0.03729   0.0147   0.0090   1.0000
  15.500   1.3233   0.04440   0.03975   0.0172   0.0089   1.0000
  15.750   1.3320   0.04553   0.04095   0.0185   0.0088   1.0000
  16.000   1.3376   0.04699   0.04251   0.0199   0.0084   1.0000
  16.250   1.3368   0.04911   0.04473   0.0216   0.0085   1.0000
  16.500   1.3279   0.05221   0.04798   0.0236   0.0083   1.0000
  16.750   1.3295   0.05428   0.05015   0.0247   0.0081   1.0000
  17.000   1.3147   0.05829   0.05432   0.0261   0.0082   1.0000
  17.250   1.3048   0.06196   0.05815   0.0269   0.0082   1.0000
  17.500   1.2936   0.06599   0.06232   0.0273   0.0083   1.0000
  17.750   1.2957   0.06854   0.06493   0.0272   0.0077   1.0000
  18.000   1.2743   0.07439   0.07098   0.0265   0.0080   1.0000
  18.250   1.2633   0.07917   0.07588   0.0254   0.0079   1.0000
  18.500   1.2530   0.08405   0.08088   0.0239   0.0078   1.0000
  18.750   1.2425   0.08931   0.08623   0.0218   0.0075   1.0000
  19.000   1.1892   0.10234   0.09960   0.0162   0.0080   1.0000
  19.250   1.1733   0.10921   0.10658   0.0128   0.0079   1.0000
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