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RAE 5215 AIRFOIL (rae5215-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: RAE 5215 AIRFOIL (rae5215-il)
Reynolds number: 500,000
Max Cl/Cd: 68.64 at α=8°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-rae5215-il-500000-n5.txt
Download as CSV file: xf-rae5215-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: RAE 5215 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
  ------ -------- --------- --------- -------- -------- --------
 -11.250  -0.9188   0.04121   0.03777  -0.0489   1.0000   0.0090
 -11.000  -0.9403   0.03378   0.02969  -0.0508   1.0000   0.0091
 -10.750  -0.9354   0.02995   0.02544  -0.0510   1.0000   0.0092
 -10.500  -0.9226   0.02722   0.02237  -0.0510   1.0000   0.0094
 -10.250  -0.9058   0.02509   0.01994  -0.0508   1.0000   0.0096
 -10.000  -0.8866   0.02335   0.01794  -0.0505   1.0000   0.0097
  -9.750  -0.8654   0.02207   0.01652  -0.0503   1.0000   0.0099
  -9.500  -0.8425   0.02121   0.01559  -0.0502   1.0000   0.0101
  -9.250  -0.8190   0.02048   0.01479  -0.0499   1.0000   0.0103
  -9.000  -0.7954   0.01977   0.01401  -0.0496   1.0000   0.0106
  -8.750  -0.7719   0.01905   0.01321  -0.0493   1.0000   0.0109
  -8.500  -0.7486   0.01830   0.01237  -0.0489   1.0000   0.0112
  -8.250  -0.7255   0.01752   0.01148  -0.0483   1.0000   0.0117
  -8.000  -0.7026   0.01676   0.01059  -0.0477   1.0000   0.0121
  -7.750  -0.6796   0.01620   0.01000  -0.0471   1.0000   0.0124
  -7.500  -0.6515   0.01576   0.00954  -0.0475   0.9986   0.0129
  -7.250  -0.6194   0.01525   0.00899  -0.0487   0.9961   0.0134
  -7.000  -0.5870   0.01469   0.00835  -0.0500   0.9939   0.0141
  -6.750  -0.5553   0.01413   0.00771  -0.0510   0.9905   0.0148
  -6.500  -0.5231   0.01366   0.00724  -0.0522   0.9872   0.0154
  -6.250  -0.4902   0.01325   0.00680  -0.0535   0.9843   0.0162
  -6.000  -0.4595   0.01284   0.00635  -0.0542   0.9795   0.0171
  -5.750  -0.4275   0.01244   0.00593  -0.0553   0.9755   0.0181
  -5.500  -0.3957   0.01211   0.00560  -0.0563   0.9715   0.0193
  -5.250  -0.3651   0.01180   0.00525  -0.0569   0.9658   0.0205
  -5.000  -0.3338   0.01140   0.00485  -0.0578   0.9609   0.0217
  -4.750  -0.3042   0.01108   0.00453  -0.0582   0.9547   0.0230
  -4.500  -0.2745   0.01079   0.00421  -0.0585   0.9484   0.0240
  -4.250  -0.2453   0.01046   0.00388  -0.0588   0.9426   0.0252
  -4.000  -0.2167   0.01022   0.00363  -0.0589   0.9355   0.0269
  -3.750  -0.1881   0.00997   0.00337  -0.0590   0.9292   0.0288
  -3.500  -0.1597   0.00975   0.00315  -0.0591   0.9222   0.0307
  -3.250  -0.1313   0.00955   0.00294  -0.0590   0.9156   0.0329
  -3.000  -0.1029   0.00936   0.00276  -0.0591   0.9095   0.0372
  -2.750  -0.0744   0.00914   0.00259  -0.0591   0.9025   0.0473
  -2.500  -0.0466   0.00892   0.00241  -0.0590   0.8939   0.0663
  -2.250  -0.0186   0.00862   0.00225  -0.0590   0.8825   0.1080
  -2.000   0.0096   0.00819   0.00206  -0.0592   0.8719   0.1852
  -1.750   0.0382   0.00748   0.00184  -0.0597   0.8619   0.3348
  -1.500   0.0669   0.00689   0.00175  -0.0602   0.8534   0.4838
  -1.250   0.0947   0.00675   0.00180  -0.0600   0.8408   0.5561
  -1.000   0.1220   0.00676   0.00184  -0.0595   0.8189   0.5948
  -0.750   0.1491   0.00685   0.00185  -0.0589   0.7893   0.6176
  -0.500   0.1766   0.00694   0.00184  -0.0585   0.7577   0.6299
  -0.250   0.2043   0.00705   0.00180  -0.0582   0.7215   0.6356
   0.000   0.2317   0.00722   0.00177  -0.0579   0.6710   0.6398
   0.250   0.2569   0.00771   0.00180  -0.0572   0.5587   0.6437
   0.500   0.2813   0.00852   0.00198  -0.0568   0.4039   0.6479
   0.750   0.3074   0.00911   0.00214  -0.0566   0.2963   0.6523
   1.000   0.3344   0.00954   0.00226  -0.0566   0.2271   0.6565
   1.250   0.3617   0.00986   0.00239  -0.0565   0.1791   0.6602
   1.500   0.3893   0.01011   0.00251  -0.0564   0.1516   0.6642
   1.750   0.4173   0.01031   0.00263  -0.0564   0.1363   0.6683
   2.000   0.4453   0.01049   0.00275  -0.0563   0.1263   0.6725
   2.250   0.4734   0.01065   0.00288  -0.0563   0.1193   0.6762
   2.500   0.5013   0.01079   0.00301  -0.0562   0.1141   0.6798
   2.750   0.5291   0.01098   0.00317  -0.0561   0.1086   0.6837
   3.000   0.5571   0.01113   0.00332  -0.0561   0.1051   0.6880
   3.250   0.5850   0.01129   0.00348  -0.0560   0.1014   0.6921
   3.500   0.6126   0.01147   0.00366  -0.0559   0.0974   0.6957
   3.750   0.6402   0.01165   0.00384  -0.0558   0.0935   0.6999
   4.000   0.6679   0.01181   0.00401  -0.0557   0.0888   0.7046
   4.250   0.6953   0.01203   0.00419  -0.0556   0.0836   0.7091
   4.500   0.7228   0.01218   0.00437  -0.0555   0.0794   0.7133
   4.750   0.7500   0.01239   0.00457  -0.0553   0.0748   0.7180
   5.000   0.7773   0.01258   0.00478  -0.0552   0.0706   0.7234
   5.250   0.8043   0.01281   0.00499  -0.0550   0.0660   0.7289
   5.500   0.8313   0.01301   0.00524  -0.0548   0.0618   0.7348
   5.750   0.8580   0.01327   0.00549  -0.0546   0.0578   0.7412
   6.000   0.8846   0.01352   0.00577  -0.0543   0.0539   0.7475
   6.250   0.9110   0.01380   0.00607  -0.0541   0.0503   0.7550
   6.750   0.9631   0.01440   0.00674  -0.0534   0.0436   0.7736
   7.000   0.9886   0.01474   0.00712  -0.0530   0.0408   0.7852
   7.250   1.0142   0.01504   0.00750  -0.0526   0.0384   0.7993
   7.500   1.0390   0.01538   0.00790  -0.0521   0.0362   0.8180
   7.750   1.0628   0.01566   0.00832  -0.0513   0.0344   0.8491
   8.000   1.0832   0.01578   0.00865  -0.0496   0.0328   1.0000
   8.250   1.1082   0.01627   0.00913  -0.0492   0.0314   1.0000
   8.500   1.1334   0.01671   0.00963  -0.0489   0.0303   1.0000
   8.750   1.1582   0.01719   0.01013  -0.0485   0.0291   1.0000
   9.000   1.1826   0.01771   0.01067  -0.0480   0.0281   1.0000
   9.250   1.2065   0.01829   0.01127  -0.0475   0.0273   1.0000
   9.500   1.2304   0.01883   0.01187  -0.0469   0.0267   1.0000
   9.750   1.2538   0.01940   0.01251  -0.0463   0.0261   1.0000
  10.000   1.2769   0.02000   0.01317  -0.0457   0.0255   1.0000
  10.250   1.2995   0.02063   0.01385  -0.0450   0.0250   1.0000
  10.500   1.3213   0.02132   0.01459  -0.0443   0.0246   1.0000
  10.750   1.3421   0.02211   0.01542  -0.0434   0.0242   1.0000
  11.000   1.3623   0.02292   0.01630  -0.0425   0.0238   1.0000
  11.250   1.3827   0.02367   0.01715  -0.0415   0.0235   1.0000
  11.500   1.4023   0.02447   0.01804  -0.0405   0.0232   1.0000
  11.750   1.4211   0.02530   0.01897  -0.0394   0.0229   1.0000
  12.000   1.4391   0.02616   0.01992  -0.0382   0.0225   1.0000
  12.250   1.4562   0.02705   0.02091  -0.0369   0.0222   1.0000
  12.500   1.4720   0.02799   0.02194  -0.0355   0.0219   1.0000
  12.750   1.4863   0.02900   0.02304  -0.0340   0.0217   1.0000
  13.000   1.4985   0.03006   0.02420  -0.0321   0.0215   1.0000
  13.250   1.5064   0.03118   0.02541  -0.0297   0.0213   1.0000
  13.500   1.5125   0.03245   0.02678  -0.0272   0.0211   1.0000
  13.750   1.5167   0.03392   0.02834  -0.0249   0.0210   1.0000
  14.000   1.5188   0.03562   0.03015  -0.0226   0.0208   1.0000
  14.250   1.5196   0.03755   0.03218  -0.0206   0.0207   1.0000
  14.500   1.5216   0.03950   0.03430  -0.0191   0.0206   1.0000
  14.750   1.5218   0.04173   0.03668  -0.0178   0.0205   1.0000
  15.000   1.5201   0.04428   0.03939  -0.0168   0.0204   1.0000
  15.250   1.5164   0.04722   0.04250  -0.0163   0.0203   1.0000
  15.500   1.5101   0.05066   0.04611  -0.0163   0.0202   1.0000
  15.750   1.5013   0.05470   0.05032  -0.0169   0.0201   1.0000
  16.000   1.4893   0.05957   0.05536  -0.0185   0.0201   1.0000
  16.250   1.4732   0.06557   0.06156  -0.0213   0.0200   1.0000
  16.500   1.4522   0.07323   0.06942  -0.0257   0.0200   1.0000
  16.750   1.4236   0.08322   0.07964  -0.0321   0.0200   1.0000
  17.000   1.3855   0.09577   0.09242  -0.0401   0.0201   1.0000
  17.250   1.3374   0.11029   0.10715  -0.0487   0.0201   1.0000
  17.500   1.2840   0.12594   0.12300  -0.0579   0.0202   1.0000
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