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RAE 5214 AIRFOIL (rae5214-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: RAE 5214 AIRFOIL (rae5214-il)
Reynolds number: 500,000
Max Cl/Cd: 68.4 at α=8°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-rae5214-il-500000-n5.txt
Download as CSV file: xf-rae5214-il-500000-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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.250  -0.8651   0.04842   0.04518  -0.0534   1.0000   0.0089
 -12.000  -0.9047   0.04072   0.03712  -0.0573   1.0000   0.0089
 -11.750  -0.9292   0.03632   0.03245  -0.0576   1.0000   0.0089
 -11.500  -0.9398   0.03324   0.02909  -0.0562   1.0000   0.0090
 -11.250  -0.9419   0.03015   0.02567  -0.0550   1.0000   0.0091
 -11.000  -0.9355   0.02783   0.02305  -0.0538   1.0000   0.0092
 -10.750  -0.9245   0.02602   0.02103  -0.0527   1.0000   0.0094
 -10.500  -0.9091   0.02484   0.01974  -0.0517   1.0000   0.0095
 -10.250  -0.8918   0.02391   0.01872  -0.0507   1.0000   0.0097
 -10.000  -0.8736   0.02306   0.01780  -0.0497   1.0000   0.0099
  -9.750  -0.8549   0.02225   0.01690  -0.0487   1.0000   0.0100
  -9.500  -0.8363   0.02139   0.01593  -0.0476   1.0000   0.0102
  -9.250  -0.8174   0.02055   0.01499  -0.0465   1.0000   0.0105
  -9.000  -0.7987   0.01966   0.01398  -0.0454   1.0000   0.0108
  -8.750  -0.7800   0.01876   0.01295  -0.0441   1.0000   0.0112
  -8.500  -0.7611   0.01792   0.01198  -0.0428   1.0000   0.0115
  -8.250  -0.7313   0.01723   0.01123  -0.0438   0.9981   0.0119
  -8.000  -0.6996   0.01672   0.01068  -0.0450   0.9957   0.0122
  -7.750  -0.6682   0.01619   0.01010  -0.0460   0.9933   0.0127
  -7.500  -0.6376   0.01557   0.00941  -0.0469   0.9904   0.0133
  -7.250  -0.6062   0.01496   0.00869  -0.0480   0.9878   0.0140
  -7.000  -0.5739   0.01441   0.00811  -0.0492   0.9858   0.0145
  -6.750  -0.5424   0.01403   0.00772  -0.0502   0.9830   0.0152
  -6.500  -0.5114   0.01360   0.00725  -0.0510   0.9796   0.0161
  -6.250  -0.4791   0.01320   0.00679  -0.0521   0.9769   0.0171
  -6.000  -0.4463   0.01280   0.00641  -0.0533   0.9746   0.0181
  -5.750  -0.4171   0.01246   0.00604  -0.0537   0.9693   0.0193
  -5.500  -0.3862   0.01205   0.00559  -0.0544   0.9648   0.0203
  -5.250  -0.3555   0.01161   0.00516  -0.0552   0.9604   0.0213
  -5.000  -0.3260   0.01125   0.00479  -0.0555   0.9547   0.0223
  -4.750  -0.2944   0.01095   0.00445  -0.0563   0.9502   0.0234
  -4.500  -0.2653   0.01056   0.00407  -0.0566   0.9441   0.0247
  -4.250  -0.2356   0.01027   0.00377  -0.0570   0.9381   0.0260
  -4.000  -0.2058   0.01000   0.00348  -0.0573   0.9323   0.0273
  -3.750  -0.1778   0.00973   0.00322  -0.0572   0.9243   0.0291
  -3.500  -0.1487   0.00951   0.00298  -0.0574   0.9177   0.0311
  -3.250  -0.1211   0.00929   0.00278  -0.0572   0.9093   0.0341
  -3.000  -0.0927   0.00909   0.00257  -0.0571   0.9021   0.0392
  -2.750  -0.0652   0.00888   0.00241  -0.0570   0.8942   0.0504
  -2.500  -0.0374   0.00865   0.00224  -0.0568   0.8867   0.0712
  -2.250  -0.0102   0.00831   0.00207  -0.0567   0.8781   0.1192
  -2.000   0.0161   0.00781   0.00186  -0.0565   0.8657   0.2136
  -1.750   0.0412   0.00709   0.00162  -0.0563   0.8492   0.3680
  -1.500   0.0665   0.00664   0.00153  -0.0558   0.8306   0.4897
  -1.250   0.0927   0.00653   0.00156  -0.0551   0.8104   0.5580
  -1.000   0.1193   0.00655   0.00161  -0.0545   0.7895   0.5949
  -0.750   0.1463   0.00663   0.00164  -0.0540   0.7677   0.6180
  -0.500   0.1729   0.00672   0.00165  -0.0534   0.7410   0.6297
  -0.250   0.1993   0.00685   0.00161  -0.0528   0.7036   0.6352
   0.000   0.2256   0.00701   0.00159  -0.0522   0.6616   0.6394
   0.250   0.2515   0.00719   0.00160  -0.0516   0.6143   0.6433
   0.500   0.2760   0.00754   0.00165  -0.0508   0.5391   0.6475
   0.750   0.2995   0.00807   0.00176  -0.0499   0.4409   0.6519
   1.000   0.3240   0.00858   0.00190  -0.0493   0.3511   0.6561
   1.250   0.3483   0.00910   0.00206  -0.0488   0.2604   0.6598
   1.500   0.3739   0.00948   0.00222  -0.0484   0.2046   0.6638
   1.750   0.4004   0.00975   0.00235  -0.0480   0.1750   0.6680
   2.000   0.4274   0.00997   0.00246  -0.0478   0.1553   0.6721
   2.250   0.4544   0.01016   0.00259  -0.0476   0.1399   0.6758
   2.500   0.4813   0.01034   0.00272  -0.0473   0.1266   0.6794
   2.750   0.5082   0.01052   0.00286  -0.0470   0.1161   0.6834
   3.000   0.5353   0.01070   0.00301  -0.0468   0.1088   0.6877
   3.250   0.5623   0.01090   0.00317  -0.0465   0.1023   0.6917
   3.500   0.5892   0.01107   0.00334  -0.0462   0.0974   0.6953
   3.750   0.6159   0.01125   0.00352  -0.0459   0.0923   0.6995
   4.000   0.6425   0.01146   0.00373  -0.0456   0.0874   0.7042
   4.250   0.6693   0.01166   0.00391  -0.0453   0.0821   0.7088
   4.500   0.6957   0.01187   0.00411  -0.0450   0.0774   0.7130
   4.750   0.7223   0.01205   0.00432  -0.0447   0.0732   0.7177
   5.000   0.7485   0.01229   0.00454  -0.0443   0.0690   0.7232
   5.250   0.7750   0.01248   0.00477  -0.0440   0.0655   0.7287
   5.500   0.8009   0.01272   0.00501  -0.0436   0.0617   0.7346
   5.750   0.8271   0.01294   0.00527  -0.0433   0.0582   0.7409
   6.000   0.8528   0.01320   0.00553  -0.0429   0.0544   0.7473
   6.250   0.8785   0.01345   0.00582  -0.0424   0.0511   0.7549
   6.500   0.9038   0.01375   0.00612  -0.0420   0.0477   0.7636
   6.750   0.9290   0.01400   0.00645  -0.0415   0.0449   0.7740
   7.000   0.9537   0.01433   0.00680  -0.0409   0.0421   0.7859
   7.250   0.9784   0.01460   0.00716  -0.0403   0.0396   0.8005
   7.500   1.0021   0.01492   0.00755  -0.0395   0.0374   0.8205
   7.750   1.0245   0.01515   0.00794  -0.0384   0.0355   0.8570
   8.000   1.0513   0.01537   0.00833  -0.0383   0.0335   1.0000
   8.250   1.0756   0.01582   0.00879  -0.0378   0.0320   1.0000
   8.500   1.1000   0.01625   0.00925  -0.0372   0.0305   1.0000
   8.750   1.1239   0.01673   0.00974  -0.0367   0.0294   1.0000
   9.000   1.1471   0.01727   0.01030  -0.0360   0.0285   1.0000
   9.250   1.1704   0.01777   0.01085  -0.0354   0.0277   1.0000
   9.500   1.1934   0.01830   0.01143  -0.0347   0.0270   1.0000
   9.750   1.2159   0.01886   0.01204  -0.0340   0.0264   1.0000
  10.000   1.2379   0.01945   0.01267  -0.0332   0.0258   1.0000
  10.250   1.2590   0.02011   0.01337  -0.0323   0.0253   1.0000
  10.500   1.2790   0.02087   0.01416  -0.0313   0.0248   1.0000
  10.750   1.2998   0.02151   0.01489  -0.0304   0.0244   1.0000
  11.000   1.3199   0.02219   0.01565  -0.0294   0.0240   1.0000
  11.250   1.3392   0.02291   0.01645  -0.0283   0.0236   1.0000
  11.500   1.3577   0.02366   0.01728  -0.0271   0.0232   1.0000
  11.750   1.3752   0.02445   0.01815  -0.0259   0.0229   1.0000
  12.000   1.3917   0.02529   0.01906  -0.0245   0.0226   1.0000
  12.250   1.4067   0.02617   0.02003  -0.0230   0.0223   1.0000
  12.500   1.4189   0.02709   0.02102  -0.0211   0.0221   1.0000
  12.750   1.4281   0.02810   0.02210  -0.0188   0.0219   1.0000
  13.000   1.4347   0.02925   0.02333  -0.0163   0.0217   1.0000
  13.250   1.4394   0.03058   0.02474  -0.0139   0.0215   1.0000
  13.500   1.4463   0.03181   0.02609  -0.0119   0.0214   1.0000
  13.750   1.4516   0.03321   0.02762  -0.0100   0.0212   1.0000
  14.000   1.4556   0.03478   0.02932  -0.0082   0.0211   1.0000
  14.250   1.4585   0.03652   0.03119  -0.0067   0.0210   1.0000
  14.500   1.4594   0.03852   0.03333  -0.0054   0.0208   1.0000
  14.750   1.4590   0.04077   0.03573  -0.0044   0.0207   1.0000
  15.000   1.4568   0.04336   0.03846  -0.0038   0.0206   1.0000
  15.250   1.4529   0.04630   0.04154  -0.0036   0.0205   1.0000
  15.500   1.4469   0.04972   0.04512  -0.0040   0.0204   1.0000
  15.750   1.4388   0.05368   0.04923  -0.0050   0.0203   1.0000
  16.000   1.4281   0.05837   0.05408  -0.0068   0.0202   1.0000
  16.250   1.4141   0.06400   0.05989  -0.0096   0.0202   1.0000
  16.500   1.3960   0.07092   0.06700  -0.0136   0.0201   1.0000
  16.750   1.3727   0.07950   0.07578  -0.0191   0.0201   1.0000
  17.000   1.3431   0.09003   0.08652  -0.0260   0.0201   1.0000
  17.250   1.3029   0.10337   0.10008  -0.0347   0.0202   1.0000
  17.500   1.2541   0.11897   0.11592  -0.0446   0.0202   1.0000
  17.750   1.1770   0.14205   0.13928  -0.0596   0.0203   1.0000
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