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RAE(NPL) 5213 AIRFOIL (rae5213-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: RAE(NPL) 5213 AIRFOIL (rae5213-il)
Reynolds number: 500,000
Max Cl/Cd: 68.27 at α=8°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-rae5213-il-500000-n5.txt
Download as CSV file: xf-rae5213-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: RAE(NPL) 5213 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  -0.8598   0.04849   0.04525  -0.0534   1.0000   0.0088
 -12.000  -0.8975   0.04100   0.03743  -0.0573   1.0000   0.0089
 -11.750  -0.9238   0.03635   0.03249  -0.0577   1.0000   0.0089
 -11.500  -0.9375   0.03290   0.02872  -0.0563   1.0000   0.0090
 -11.250  -0.9387   0.02988   0.02536  -0.0551   1.0000   0.0092
 -11.000  -0.9310   0.02773   0.02295  -0.0539   1.0000   0.0092
 -10.750  -0.9192   0.02607   0.02111  -0.0529   1.0000   0.0094
 -10.500  -0.9034   0.02494   0.01987  -0.0519   1.0000   0.0096
 -10.250  -0.8861   0.02397   0.01881  -0.0509   1.0000   0.0097
 -10.000  -0.8679   0.02308   0.01783  -0.0500   1.0000   0.0098
  -9.750  -0.8489   0.02230   0.01697  -0.0491   1.0000   0.0101
  -9.500  -0.8299   0.02146   0.01603  -0.0481   1.0000   0.0103
  -9.250  -0.8109   0.02057   0.01503  -0.0470   1.0000   0.0105
  -9.000  -0.7919   0.01966   0.01399  -0.0459   1.0000   0.0109
  -8.750  -0.7728   0.01875   0.01294  -0.0447   1.0000   0.0112
  -8.500  -0.7536   0.01787   0.01192  -0.0435   1.0000   0.0116
  -8.250  -0.7308   0.01727   0.01128  -0.0430   0.9995   0.0118
  -8.000  -0.6989   0.01675   0.01073  -0.0442   0.9972   0.0122
  -7.750  -0.6667   0.01624   0.01017  -0.0455   0.9947   0.0127
  -7.500  -0.6359   0.01561   0.00947  -0.0464   0.9918   0.0133
  -7.250  -0.6044   0.01498   0.00873  -0.0475   0.9889   0.0140
  -7.000  -0.5720   0.01442   0.00814  -0.0487   0.9864   0.0145
  -6.750  -0.5393   0.01402   0.00773  -0.0500   0.9840   0.0152
  -6.500  -0.5085   0.01361   0.00728  -0.0507   0.9800   0.0160
  -6.250  -0.4758   0.01320   0.00680  -0.0519   0.9769   0.0171
  -6.000  -0.4425   0.01281   0.00643  -0.0532   0.9742   0.0181
  -5.750  -0.4137   0.01246   0.00605  -0.0535   0.9677   0.0192
  -5.500  -0.3818   0.01204   0.00559  -0.0544   0.9630   0.0203
  -5.250  -0.3523   0.01160   0.00516  -0.0549   0.9566   0.0212
  -5.000  -0.3208   0.01123   0.00478  -0.0557   0.9511   0.0222
  -4.750  -0.2904   0.01093   0.00443  -0.0562   0.9444   0.0234
  -4.500  -0.2603   0.01054   0.00405  -0.0567   0.9371   0.0247
  -4.250  -0.2310   0.01025   0.00374  -0.0570   0.9291   0.0259
  -4.000  -0.2019   0.00999   0.00346  -0.0571   0.9200   0.0271
  -3.750  -0.1738   0.00972   0.00318  -0.0571   0.9105   0.0289
  -3.250  -0.1177   0.00930   0.00273  -0.0569   0.8908   0.0338
  -3.000  -0.0899   0.00911   0.00253  -0.0567   0.8812   0.0386
  -2.750  -0.0624   0.00891   0.00236  -0.0565   0.8701   0.0490
  -2.500  -0.0351   0.00869   0.00219  -0.0563   0.8585   0.0686
  -2.250  -0.0081   0.00839   0.00201  -0.0561   0.8463   0.1132
  -2.000   0.0184   0.00792   0.00182  -0.0560   0.8336   0.2009
  -1.750   0.0439   0.00721   0.00159  -0.0559   0.8185   0.3551
  -1.500   0.0695   0.00674   0.00150  -0.0556   0.8007   0.4828
  -1.250   0.0961   0.00661   0.00155  -0.0551   0.7860   0.5554
  -1.000   0.1234   0.00662   0.00161  -0.0547   0.7732   0.5933
  -0.750   0.1505   0.00670   0.00165  -0.0542   0.7556   0.6170
  -0.500   0.1773   0.00679   0.00167  -0.0537   0.7296   0.6293
  -0.250   0.2038   0.00692   0.00164  -0.0531   0.6968   0.6351
   0.000   0.2306   0.00706   0.00162  -0.0526   0.6633   0.6394
   0.250   0.2572   0.00718   0.00162  -0.0522   0.6303   0.6433
   0.500   0.2836   0.00734   0.00164  -0.0517   0.5886   0.6475
   0.750   0.3097   0.00757   0.00167  -0.0512   0.5413   0.6519
   1.000   0.3347   0.00795   0.00175  -0.0506   0.4703   0.6561
   1.250   0.3591   0.00841   0.00188  -0.0499   0.3883   0.6598
   1.500   0.3832   0.00897   0.00206  -0.0493   0.2958   0.6638
   1.750   0.4078   0.00950   0.00226  -0.0488   0.2149   0.6679
   2.000   0.4333   0.00993   0.00243  -0.0485   0.1599   0.6720
   2.250   0.4598   0.01021   0.00259  -0.0482   0.1332   0.6758
   2.500   0.4864   0.01043   0.00274  -0.0479   0.1173   0.6793
   2.750   0.5134   0.01062   0.00289  -0.0476   0.1081   0.6833
   3.000   0.5404   0.01081   0.00306  -0.0474   0.1016   0.6876
   3.250   0.5675   0.01099   0.00323  -0.0471   0.0967   0.6916
   3.500   0.5941   0.01120   0.00342  -0.0468   0.0915   0.6952
   3.750   0.6210   0.01137   0.00360  -0.0466   0.0879   0.6994
   4.000   0.6478   0.01156   0.00380  -0.0463   0.0832   0.7041
   4.250   0.6743   0.01179   0.00400  -0.0460   0.0784   0.7087
   4.500   0.7010   0.01196   0.00419  -0.0457   0.0743   0.7129
   4.750   0.7273   0.01218   0.00441  -0.0454   0.0703   0.7176
   5.000   0.7539   0.01237   0.00462  -0.0451   0.0668   0.7231
   5.250   0.7801   0.01259   0.00484  -0.0447   0.0632   0.7285
   5.500   0.8062   0.01281   0.00510  -0.0444   0.0601   0.7345
   5.750   0.8322   0.01304   0.00534  -0.0440   0.0566   0.7408
   6.000   0.8579   0.01330   0.00561  -0.0436   0.0533   0.7472
   6.250   0.8835   0.01354   0.00589  -0.0432   0.0499   0.7547
   6.500   0.9089   0.01382   0.00620  -0.0427   0.0469   0.7634
   6.750   0.9339   0.01409   0.00652  -0.0422   0.0441   0.7738
   7.000   0.9585   0.01440   0.00687  -0.0417   0.0416   0.7857
   7.250   0.9830   0.01468   0.00723  -0.0411   0.0391   0.8004
   7.500   1.0066   0.01500   0.00761  -0.0403   0.0370   0.8205
   7.750   1.0288   0.01522   0.00800  -0.0392   0.0351   0.8573
   8.000   1.0554   0.01546   0.00839  -0.0390   0.0332   1.0000
   8.250   1.0796   0.01589   0.00885  -0.0385   0.0317   1.0000
   8.500   1.1036   0.01633   0.00931  -0.0379   0.0303   1.0000
   8.750   1.1272   0.01682   0.00980  -0.0373   0.0292   1.0000
   9.000   1.1502   0.01735   0.01036  -0.0366   0.0284   1.0000
   9.250   1.1732   0.01786   0.01092  -0.0360   0.0277   1.0000
   9.500   1.1958   0.01839   0.01150  -0.0352   0.0269   1.0000
   9.750   1.2179   0.01895   0.01210  -0.0345   0.0263   1.0000
  10.000   1.2395   0.01955   0.01274  -0.0336   0.0258   1.0000
  10.250   1.2600   0.02023   0.01345  -0.0327   0.0252   1.0000
  10.500   1.2798   0.02095   0.01422  -0.0317   0.0248   1.0000
  10.750   1.3000   0.02161   0.01496  -0.0307   0.0244   1.0000
  11.000   1.3195   0.02229   0.01572  -0.0296   0.0240   1.0000
  11.250   1.3382   0.02301   0.01651  -0.0285   0.0236   1.0000
  11.500   1.3560   0.02375   0.01733  -0.0273   0.0232   1.0000
  11.750   1.3727   0.02455   0.01820  -0.0259   0.0229   1.0000
  12.000   1.3881   0.02538   0.01910  -0.0244   0.0226   1.0000
  12.250   1.4005   0.02624   0.02004  -0.0224   0.0223   1.0000
  12.500   1.4106   0.02718   0.02104  -0.0202   0.0221   1.0000
  12.750   1.4190   0.02823   0.02217  -0.0180   0.0219   1.0000
  13.000   1.4253   0.02945   0.02346  -0.0157   0.0217   1.0000
  13.250   1.4310   0.03078   0.02487  -0.0136   0.0215   1.0000
  13.500   1.4379   0.03208   0.02630  -0.0118   0.0214   1.0000
  13.750   1.4434   0.03353   0.02788  -0.0102   0.0213   1.0000
  14.000   1.4477   0.03517   0.02965  -0.0087   0.0211   1.0000
  14.250   1.4504   0.03701   0.03162  -0.0074   0.0210   1.0000
  14.500   1.4524   0.03903   0.03377  -0.0064   0.0208   1.0000
  14.750   1.4528   0.04133   0.03621  -0.0056   0.0207   1.0000
  15.000   1.4513   0.04395   0.03897  -0.0052   0.0206   1.0000
  15.250   1.4487   0.04686   0.04202  -0.0052   0.0205   1.0000
  15.500   1.4444   0.05015   0.04546  -0.0056   0.0204   1.0000
  15.750   1.4379   0.05392   0.04938  -0.0065   0.0203   1.0000
  16.000   1.4292   0.05827   0.05389  -0.0080   0.0202   1.0000
  16.250   1.4184   0.06323   0.05901  -0.0102   0.0201   1.0000
  16.500   1.4045   0.06905   0.06499  -0.0131   0.0201   1.0000
  16.750   1.3876   0.07587   0.07199  -0.0170   0.0200   1.0000
  17.000   1.3661   0.08404   0.08035  -0.0220   0.0200   1.0000
  17.250   1.3398   0.09378   0.09029  -0.0283   0.0200   1.0000
  17.500   1.3052   0.10582   0.10255  -0.0360   0.0200   1.0000
  17.750   1.2577   0.12143   0.11841  -0.0461   0.0201   1.0000
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