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RAE 5214 AIRFOIL (rae5214-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: RAE 5214 AIRFOIL (rae5214-il)
Reynolds number: 1,000,000
Max Cl/Cd: 80.71 at α=9.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-rae5214-il-1000000-n5.txt
Download as CSV file: xf-rae5214-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: RAE 5214 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
  ------ -------- --------- --------- -------- -------- --------
 -15.500  -1.0587   0.06257   0.05984  -0.0454   1.0000   0.0062
 -15.250  -1.0970   0.05213   0.04916  -0.0531   1.0000   0.0062
 -15.000  -1.1158   0.04614   0.04300  -0.0569   1.0000   0.0062
 -14.750  -1.1290   0.04146   0.03816  -0.0594   1.0000   0.0062
 -14.500  -1.1397   0.03746   0.03400  -0.0612   1.0000   0.0061
 -14.250  -1.1420   0.03467   0.03109  -0.0619   1.0000   0.0062
 -14.000  -1.1442   0.03213   0.02842  -0.0623   1.0000   0.0062
 -13.750  -1.1466   0.02991   0.02607  -0.0620   1.0000   0.0063
 -13.500  -1.1488   0.02826   0.02431  -0.0604   1.0000   0.0063
 -13.250  -1.1421   0.02685   0.02277  -0.0591   1.0000   0.0063
 -13.000  -1.1314   0.02555   0.02137  -0.0581   1.0000   0.0064
 -12.750  -1.1181   0.02439   0.02009  -0.0571   1.0000   0.0065
 -12.500  -1.1032   0.02331   0.01890  -0.0562   1.0000   0.0065
 -12.250  -1.0869   0.02231   0.01780  -0.0552   1.0000   0.0066
 -12.000  -1.0697   0.02136   0.01676  -0.0543   1.0000   0.0067
 -11.750  -1.0516   0.02049   0.01579  -0.0534   1.0000   0.0068
 -11.500  -1.0329   0.01968   0.01490  -0.0524   1.0000   0.0068
 -11.250  -1.0136   0.01892   0.01406  -0.0515   1.0000   0.0069
 -11.000  -0.9938   0.01822   0.01327  -0.0506   1.0000   0.0070
 -10.750  -0.9736   0.01758   0.01256  -0.0496   1.0000   0.0071
 -10.500  -0.9531   0.01697   0.01188  -0.0486   1.0000   0.0072
 -10.250  -0.9334   0.01625   0.01110  -0.0476   1.0000   0.0075
 -10.000  -0.9128   0.01569   0.01050  -0.0465   1.0000   0.0077
  -9.750  -0.8840   0.01514   0.00991  -0.0472   0.9988   0.0079
  -9.500  -0.8536   0.01462   0.00935  -0.0481   0.9971   0.0081
  -9.250  -0.8230   0.01413   0.00882  -0.0490   0.9952   0.0085
  -9.000  -0.7929   0.01365   0.00830  -0.0498   0.9932   0.0088
  -8.750  -0.7629   0.01320   0.00779  -0.0505   0.9909   0.0091
  -8.500  -0.7322   0.01277   0.00733  -0.0514   0.9888   0.0094
  -8.250  -0.7009   0.01235   0.00690  -0.0523   0.9871   0.0099
  -8.000  -0.6688   0.01200   0.00654  -0.0534   0.9857   0.0103
  -7.750  -0.6378   0.01167   0.00619  -0.0542   0.9833   0.0108
  -7.500  -0.6080   0.01134   0.00583  -0.0547   0.9795   0.0113
  -7.250  -0.5769   0.01101   0.00549  -0.0555   0.9766   0.0118
  -6.750  -0.5172   0.01049   0.00496  -0.0565   0.9677   0.0130
  -6.500  -0.4867   0.01022   0.00467  -0.0570   0.9627   0.0137
  -6.250  -0.4579   0.00998   0.00440  -0.0572   0.9563   0.0142
  -6.000  -0.4284   0.00971   0.00414  -0.0576   0.9503   0.0149
  -5.750  -0.4000   0.00950   0.00391  -0.0576   0.9432   0.0156
  -5.500  -0.3716   0.00930   0.00369  -0.0576   0.9357   0.0164
  -5.250  -0.3439   0.00912   0.00348  -0.0575   0.9277   0.0170
  -5.000  -0.3165   0.00889   0.00323  -0.0573   0.9192   0.0177
  -4.750  -0.2891   0.00871   0.00304  -0.0571   0.9106   0.0186
  -4.250  -0.2341   0.00840   0.00267  -0.0567   0.8938   0.0205
  -4.000  -0.2067   0.00823   0.00249  -0.0565   0.8854   0.0217
  -3.750  -0.1790   0.00809   0.00232  -0.0564   0.8777   0.0228
  -3.500  -0.1513   0.00795   0.00216  -0.0562   0.8697   0.0236
  -3.250  -0.1236   0.00780   0.00200  -0.0560   0.8627   0.0251
  -3.000  -0.0957   0.00767   0.00186  -0.0559   0.8541   0.0268
  -2.750  -0.0684   0.00756   0.00173  -0.0556   0.8407   0.0296
  -2.500  -0.0412   0.00746   0.00160  -0.0553   0.8238   0.0358
  -2.250  -0.0142   0.00734   0.00148  -0.0549   0.8043   0.0514
  -2.000   0.0126   0.00724   0.00137  -0.0545   0.7807   0.0696
  -1.750   0.0395   0.00707   0.00126  -0.0543   0.7602   0.1086
  -1.500   0.0664   0.00682   0.00115  -0.0541   0.7412   0.1692
  -1.250   0.0927   0.00646   0.00102  -0.0539   0.7149   0.2703
  -1.000   0.1177   0.00601   0.00088  -0.0536   0.6743   0.4140
  -0.750   0.1424   0.00590   0.00087  -0.0531   0.6122   0.5164
  -0.500   0.1677   0.00609   0.00094  -0.0525   0.5446   0.5627
  -0.250   0.1934   0.00637   0.00104  -0.0520   0.4766   0.5876
   0.250   0.2448   0.00709   0.00124  -0.0511   0.3261   0.6114
   0.500   0.2708   0.00745   0.00134  -0.0508   0.2567   0.6156
   0.750   0.2974   0.00776   0.00144  -0.0505   0.2057   0.6193
   1.000   0.3245   0.00797   0.00152  -0.0502   0.1755   0.6230
   1.250   0.3519   0.00813   0.00160  -0.0500   0.1556   0.6271
   1.500   0.3794   0.00828   0.00169  -0.0498   0.1396   0.6312
   1.750   0.4070   0.00844   0.00177  -0.0497   0.1251   0.6352
   2.250   0.4620   0.00872   0.00196  -0.0493   0.1053   0.6426
   2.500   0.4896   0.00885   0.00207  -0.0491   0.0991   0.6463
   2.750   0.5172   0.00898   0.00218  -0.0489   0.0945   0.6502
   3.000   0.5445   0.00914   0.00231  -0.0487   0.0891   0.6538
   3.500   0.5993   0.00943   0.00255  -0.0483   0.0802   0.6605
   3.750   0.6266   0.00957   0.00269  -0.0481   0.0756   0.6643
   4.000   0.6538   0.00972   0.00283  -0.0479   0.0712   0.6680
   4.250   0.6810   0.00989   0.00298  -0.0476   0.0678   0.6715
   4.750   0.7350   0.01023   0.00330  -0.0471   0.0602   0.6788
   5.000   0.7618   0.01041   0.00347  -0.0469   0.0561   0.6829
   5.250   0.7886   0.01061   0.00366  -0.0466   0.0526   0.6869
   5.500   0.8152   0.01082   0.00386  -0.0463   0.0492   0.6906
   5.750   0.8417   0.01102   0.00407  -0.0460   0.0464   0.6946
   6.000   0.8680   0.01124   0.00429  -0.0457   0.0435   0.6994
   6.250   0.8943   0.01147   0.00453  -0.0453   0.0409   0.7045
   6.500   0.9204   0.01172   0.00478  -0.0450   0.0381   0.7091
   6.750   0.9464   0.01196   0.00504  -0.0446   0.0357   0.7141
   7.000   0.9721   0.01223   0.00532  -0.0442   0.0329   0.7198
   7.250   0.9979   0.01250   0.00561  -0.0438   0.0307   0.7257
   7.500   1.0232   0.01281   0.00593  -0.0433   0.0285   0.7327
   7.750   1.0486   0.01308   0.00624  -0.0429   0.0272   0.7411
   8.000   1.0737   0.01339   0.00658  -0.0424   0.0260   0.7498
   8.250   1.0984   0.01373   0.00696  -0.0419   0.0249   0.7602
   8.500   1.1233   0.01402   0.00732  -0.0414   0.0243   0.7720
   8.750   1.1479   0.01433   0.00769  -0.0408   0.0236   0.7867
   9.000   1.1720   0.01464   0.00809  -0.0402   0.0230   0.8077
   9.250   1.1948   0.01491   0.00851  -0.0393   0.0225   0.8485
   9.500   1.2187   0.01510   0.00894  -0.0386   0.0219   1.0000
   9.750   1.2424   0.01556   0.00943  -0.0380   0.0214   1.0000
  10.000   1.2663   0.01596   0.00986  -0.0374   0.0210   1.0000
  10.250   1.2899   0.01639   0.01033  -0.0368   0.0207   1.0000
  10.500   1.3131   0.01684   0.01082  -0.0361   0.0204   1.0000
  10.750   1.3359   0.01731   0.01134  -0.0354   0.0201   1.0000
  11.000   1.3583   0.01780   0.01187  -0.0347   0.0198   1.0000
  11.250   1.3802   0.01833   0.01244  -0.0339   0.0195   1.0000
  11.500   1.4016   0.01888   0.01303  -0.0330   0.0192   1.0000
  11.750   1.4223   0.01948   0.01367  -0.0321   0.0190   1.0000
  12.000   1.4421   0.02013   0.01438  -0.0310   0.0187   1.0000
  12.250   1.4605   0.02089   0.01519  -0.0298   0.0185   1.0000
  12.500   1.4795   0.02153   0.01589  -0.0287   0.0183   1.0000
  12.750   1.4979   0.02217   0.01661  -0.0275   0.0182   1.0000
  13.000   1.5155   0.02284   0.01735  -0.0262   0.0181   1.0000
  13.250   1.5317   0.02356   0.01815  -0.0247   0.0180   1.0000
  13.500   1.5461   0.02428   0.01895  -0.0230   0.0178   1.0000
  13.750   1.5573   0.02505   0.01979  -0.0207   0.0177   1.0000
  14.000   1.5671   0.02587   0.02070  -0.0184   0.0176   1.0000
  14.250   1.5763   0.02676   0.02166  -0.0161   0.0174   1.0000
  14.500   1.5842   0.02775   0.02273  -0.0139   0.0173   1.0000
  14.750   1.5911   0.02884   0.02392  -0.0118   0.0172   1.0000
  15.000   1.5972   0.03005   0.02522  -0.0098   0.0171   1.0000
  15.250   1.6020   0.03141   0.02667  -0.0080   0.0170   1.0000
  15.500   1.6058   0.03293   0.02829  -0.0063   0.0169   1.0000
  15.750   1.6085   0.03462   0.03008  -0.0049   0.0168   1.0000
  16.000   1.6096   0.03656   0.03212  -0.0036   0.0167   1.0000
  16.250   1.6091   0.03876   0.03442  -0.0027   0.0166   1.0000
  16.500   1.6071   0.04127   0.03704  -0.0021   0.0165   1.0000
  16.750   1.6025   0.04425   0.04013  -0.0019   0.0165   1.0000
  17.000   1.5963   0.04764   0.04365  -0.0023   0.0164   1.0000
  17.250   1.5885   0.05151   0.04763  -0.0033   0.0162   1.0000
  17.500   1.5728   0.05681   0.05310  -0.0053   0.0163   1.0000
  17.750   1.5552   0.06305   0.05948  -0.0085   0.0163   1.0000
  18.000   1.5298   0.07134   0.06797  -0.0134   0.0163   1.0000
  18.250   1.4905   0.08332   0.08018  -0.0212   0.0163   1.0000
  18.500   1.4242   0.10181   0.09897  -0.0330   0.0164   1.0000
  18.750   1.3466   0.12280   0.12023  -0.0463   0.0165   1.0000
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