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RAE 5214 AIRFOIL (rae5214-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: RAE 5214 AIRFOIL (rae5214-il)
Reynolds number: 1,000,000
Max Cl/Cd: 83.26 at α=7.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-rae5214-il-1000000.txt
Download as CSV file: xf-rae5214-il-1000000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.500  -0.7964   0.06381   0.06174  -0.0404   1.0000   0.0097
 -12.250  -0.7916   0.06021   0.05813  -0.0435   1.0000   0.0097
 -12.000  -0.7898   0.05645   0.05434  -0.0468   1.0000   0.0098
 -11.750  -0.7824   0.05420   0.05206  -0.0487   1.0000   0.0099
 -11.500  -0.7764   0.05198   0.04983  -0.0505   1.0000   0.0099
 -11.250  -0.9329   0.03067   0.02722  -0.0559   1.0000   0.0093
 -11.000  -0.9317   0.02792   0.02419  -0.0545   1.0000   0.0093
 -10.750  -0.9343   0.02409   0.01995  -0.0526   1.0000   0.0094
 -10.500  -0.9246   0.02188   0.01749  -0.0511   1.0000   0.0095
 -10.250  -0.9098   0.02044   0.01590  -0.0498   1.0000   0.0097
 -10.000  -0.8920   0.01950   0.01488  -0.0486   1.0000   0.0098
  -9.750  -0.8731   0.01876   0.01407  -0.0474   1.0000   0.0100
  -9.500  -0.8542   0.01804   0.01327  -0.0462   1.0000   0.0102
  -9.250  -0.8347   0.01744   0.01262  -0.0450   1.0000   0.0104
  -9.000  -0.8157   0.01678   0.01188  -0.0436   1.0000   0.0107
  -8.750  -0.7969   0.01611   0.01113  -0.0423   1.0000   0.0109
  -8.500  -0.7768   0.01556   0.01050  -0.0410   0.9999   0.0113
  -8.250  -0.7446   0.01480   0.00964  -0.0423   0.9986   0.0117
  -8.000  -0.7120   0.01412   0.00893  -0.0438   0.9970   0.0123
  -7.750  -0.6782   0.01382   0.00863  -0.0452   0.9956   0.0128
  -7.500  -0.6444   0.01337   0.00813  -0.0467   0.9943   0.0134
  -7.250  -0.6123   0.01306   0.00775  -0.0476   0.9921   0.0141
  -7.000  -0.5804   0.01235   0.00703  -0.0488   0.9900   0.0148
  -6.750  -0.5466   0.01208   0.00677  -0.0502   0.9882   0.0155
  -6.500  -0.5124   0.01173   0.00638  -0.0516   0.9868   0.0163
  -6.250  -0.4777   0.01139   0.00599  -0.0531   0.9856   0.0171
  -6.000  -0.4448   0.01085   0.00547  -0.0544   0.9838   0.0181
  -5.750  -0.4126   0.01053   0.00515  -0.0554   0.9807   0.0190
  -5.500  -0.3788   0.01029   0.00488  -0.0566   0.9784   0.0200
  -5.250  -0.3457   0.00973   0.00433  -0.0579   0.9759   0.0212
  -5.000  -0.3137   0.00944   0.00404  -0.0588   0.9726   0.0224
  -4.750  -0.2844   0.00922   0.00381  -0.0589   0.9664   0.0234
  -4.500  -0.2539   0.00879   0.00338  -0.0595   0.9619   0.0249
  -4.250  -0.2269   0.00857   0.00316  -0.0592   0.9541   0.0263
  -4.000  -0.1977   0.00831   0.00288  -0.0594   0.9483   0.0278
  -3.750  -0.1709   0.00808   0.00265  -0.0590   0.9398   0.0296
  -3.500  -0.1427   0.00790   0.00245  -0.0588   0.9329   0.0310
  -3.250  -0.1157   0.00768   0.00223  -0.0585   0.9242   0.0331
  -3.000  -0.0881   0.00753   0.00206  -0.0582   0.9161   0.0361
  -2.750  -0.0614   0.00733   0.00188  -0.0578   0.9042   0.0439
  -2.500  -0.0351   0.00698   0.00168  -0.0574   0.8915   0.0865
  -2.250  -0.0095   0.00639   0.00146  -0.0571   0.8781   0.2004
  -2.000   0.0153   0.00558   0.00120  -0.0568   0.8636   0.3821
  -1.750   0.0414   0.00516   0.00111  -0.0565   0.8502   0.4971
  -1.500   0.0688   0.00505   0.00110  -0.0562   0.8380   0.5431
  -1.250   0.0964   0.00504   0.00108  -0.0558   0.8234   0.5672
  -1.000   0.1237   0.00505   0.00108  -0.0554   0.8046   0.5875
  -0.750   0.1510   0.00510   0.00109  -0.0550   0.7852   0.6055
  -0.500   0.1787   0.00516   0.00113  -0.0547   0.7690   0.6223
  -0.250   0.2063   0.00524   0.00117  -0.0543   0.7518   0.6361
   0.000   0.2336   0.00531   0.00120  -0.0539   0.7291   0.6460
   0.250   0.2608   0.00543   0.00121  -0.0535   0.7027   0.6507
   0.500   0.2878   0.00557   0.00122  -0.0531   0.6683   0.6545
   0.750   0.3136   0.00581   0.00125  -0.0525   0.6073   0.6581
   1.000   0.3370   0.00630   0.00134  -0.0516   0.5008   0.6622
   1.250   0.3603   0.00694   0.00151  -0.0508   0.3809   0.6661
   1.750   0.4096   0.00802   0.00185  -0.0497   0.2001   0.6736
   2.000   0.4363   0.00824   0.00196  -0.0495   0.1708   0.6777
   2.250   0.4633   0.00843   0.00208  -0.0492   0.1506   0.6818
   2.500   0.4905   0.00862   0.00219  -0.0490   0.1336   0.6858
   2.750   0.5177   0.00881   0.00231  -0.0487   0.1207   0.6897
   3.000   0.5450   0.00899   0.00244  -0.0485   0.1112   0.6934
   3.250   0.5720   0.00914   0.00257  -0.0483   0.1039   0.6977
   3.500   0.5992   0.00929   0.00272  -0.0480   0.0979   0.7019
   3.750   0.6263   0.00948   0.00286  -0.0478   0.0920   0.7062
   4.000   0.6535   0.00965   0.00303  -0.0476   0.0875   0.7102
   4.250   0.6806   0.00977   0.00317  -0.0473   0.0838   0.7149
   4.500   0.7073   0.00998   0.00336  -0.0470   0.0790   0.7196
   4.750   0.7345   0.01012   0.00352  -0.0468   0.0757   0.7247
   5.000   0.7614   0.01029   0.00367  -0.0465   0.0715   0.7299
   5.250   0.7880   0.01047   0.00386  -0.0462   0.0676   0.7355
   5.500   0.8147   0.01064   0.00404  -0.0459   0.0638   0.7415
   5.750   0.8411   0.01085   0.00425  -0.0456   0.0601   0.7477
   6.000   0.8675   0.01103   0.00445  -0.0453   0.0566   0.7553
   6.250   0.8936   0.01127   0.00470  -0.0449   0.0530   0.7635
   6.500   0.9196   0.01149   0.00493  -0.0445   0.0494   0.7734
   6.750   0.9453   0.01172   0.00521  -0.0441   0.0459   0.7847
   7.000   0.9702   0.01203   0.00553  -0.0436   0.0420   0.7995
   7.250   0.9953   0.01222   0.00581  -0.0430   0.0391   0.8218
   7.500   1.0176   0.01241   0.00617  -0.0418   0.0365   0.8743
   7.750   1.0449   0.01255   0.00647  -0.0417   0.0343   1.0000
   8.000   1.0695   0.01301   0.00691  -0.0412   0.0325   1.0000
   8.250   1.0949   0.01334   0.00727  -0.0408   0.0313   1.0000
   8.500   1.1198   0.01372   0.00765  -0.0403   0.0302   1.0000
   8.750   1.1439   0.01419   0.00812  -0.0397   0.0291   1.0000
   9.000   1.1675   0.01471   0.00867  -0.0390   0.0283   1.0000
   9.250   1.1919   0.01510   0.00910  -0.0385   0.0276   1.0000
   9.500   1.2158   0.01553   0.00956  -0.0379   0.0270   1.0000
   9.750   1.2393   0.01600   0.01006  -0.0372   0.0264   1.0000
  10.000   1.2622   0.01652   0.01061  -0.0365   0.0259   1.0000
  10.250   1.2837   0.01717   0.01129  -0.0356   0.0254   1.0000
  10.500   1.3030   0.01805   0.01222  -0.0345   0.0248   1.0000
  10.750   1.3252   0.01857   0.01280  -0.0337   0.0246   1.0000
  11.000   1.3468   0.01914   0.01343  -0.0328   0.0243   1.0000
  11.250   1.3676   0.01975   0.01411  -0.0318   0.0240   1.0000
  11.500   1.3877   0.02040   0.01483  -0.0308   0.0237   1.0000
  11.750   1.4071   0.02108   0.01557  -0.0297   0.0235   1.0000
  12.000   1.4257   0.02180   0.01635  -0.0285   0.0232   1.0000
  12.250   1.4433   0.02255   0.01717  -0.0272   0.0229   1.0000
  12.500   1.4600   0.02332   0.01799  -0.0258   0.0227   1.0000
  12.750   1.4751   0.02416   0.01890  -0.0242   0.0225   1.0000
  13.000   1.4870   0.02509   0.01988  -0.0221   0.0222   1.0000
  13.250   1.4947   0.02610   0.02096  -0.0195   0.0220   1.0000
  13.500   1.4988   0.02735   0.02230  -0.0165   0.0218   1.0000
  13.750   1.4996   0.02893   0.02398  -0.0136   0.0216   1.0000
  14.000   1.4987   0.03075   0.02592  -0.0108   0.0215   1.0000
  14.250   1.5047   0.03200   0.02728  -0.0089   0.0214   1.0000
  14.500   1.5084   0.03353   0.02891  -0.0071   0.0213   1.0000
  14.750   1.5114   0.03519   0.03069  -0.0055   0.0213   1.0000
  15.000   1.5128   0.03708   0.03270  -0.0041   0.0212   1.0000
  15.250   1.5124   0.03927   0.03500  -0.0030   0.0211   1.0000
  15.500   1.5106   0.04172   0.03758  -0.0023   0.0210   1.0000
  15.750   1.5070   0.04455   0.04054  -0.0019   0.0209   1.0000
  16.000   1.5016   0.04777   0.04389  -0.0020   0.0209   1.0000
  16.250   1.4943   0.05147   0.04773  -0.0027   0.0208   1.0000
  16.500   1.4845   0.05580   0.05220  -0.0041   0.0207   1.0000
  16.750   1.4718   0.06091   0.05747  -0.0063   0.0207   1.0000
  17.000   1.4572   0.06680   0.06350  -0.0094   0.0206   1.0000
  17.250   1.4384   0.07394   0.07081  -0.0136   0.0206   1.0000
  17.500   1.4166   0.08221   0.07925  -0.0189   0.0206   1.0000
  17.750   1.3898   0.09208   0.08930  -0.0254   0.0205   1.0000
  18.000   1.3549   0.10402   0.10143  -0.0333   0.0206   1.0000
  18.250   1.3127   0.11815   0.11576  -0.0427   0.0207   1.0000
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