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RAE(NPL) 5213 AIRFOIL (rae5213-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: RAE(NPL) 5213 AIRFOIL (rae5213-il)
Reynolds number: 1,000,000
Max Cl/Cd: 83.18 at α=7.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-rae5213-il-1000000.txt
Download as CSV file: xf-rae5213-il-1000000.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 =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.000  -0.5560   0.13461   0.13271  -0.0058   1.0000   0.0141
 -12.750  -0.5538   0.13014   0.12824  -0.0076   1.0000   0.0141
 -12.500  -0.7841   0.06579   0.06376  -0.0387   1.0000   0.0096
 -12.250  -0.7743   0.06312   0.06110  -0.0409   1.0000   0.0097
 -12.000  -0.7707   0.05929   0.05724  -0.0443   1.0000   0.0098
 -11.750  -0.7720   0.05513   0.05303  -0.0480   1.0000   0.0099
 -11.500  -0.7644   0.05313   0.05102  -0.0497   1.0000   0.0099
 -11.250  -0.9348   0.02977   0.02624  -0.0558   1.0000   0.0093
 -11.000  -0.9306   0.02732   0.02355  -0.0545   1.0000   0.0093
 -10.750  -0.9320   0.02363   0.01945  -0.0526   1.0000   0.0094
 -10.500  -0.9201   0.02174   0.01734  -0.0513   1.0000   0.0095
 -10.250  -0.9045   0.02039   0.01585  -0.0501   1.0000   0.0097
 -10.000  -0.8863   0.01947   0.01484  -0.0489   1.0000   0.0098
  -9.750  -0.8669   0.01877   0.01409  -0.0479   1.0000   0.0100
  -9.500  -0.8471   0.01814   0.01339  -0.0468   1.0000   0.0102
  -9.250  -0.8274   0.01748   0.01267  -0.0456   1.0000   0.0104
  -9.000  -0.8077   0.01684   0.01195  -0.0444   1.0000   0.0108
  -8.750  -0.7883   0.01615   0.01117  -0.0431   1.0000   0.0110
  -8.500  -0.7687   0.01552   0.01046  -0.0418   1.0000   0.0113
  -8.250  -0.7455   0.01487   0.00972  -0.0412   0.9997   0.0117
  -8.000  -0.7129   0.01416   0.00899  -0.0427   0.9982   0.0122
  -7.750  -0.6790   0.01388   0.00871  -0.0441   0.9967   0.0128
  -7.500  -0.6451   0.01344   0.00821  -0.0456   0.9952   0.0134
  -7.250  -0.6114   0.01307   0.00778  -0.0469   0.9935   0.0140
  -7.000  -0.5797   0.01238   0.00706  -0.0480   0.9912   0.0147
  -6.750  -0.5460   0.01208   0.00677  -0.0494   0.9891   0.0154
  -6.500  -0.5116   0.01173   0.00639  -0.0509   0.9874   0.0162
  -6.250  -0.4765   0.01150   0.00611  -0.0524   0.9860   0.0170
  -6.000  -0.4418   0.01085   0.00549  -0.0541   0.9848   0.0180
  -5.750  -0.4104   0.01053   0.00516  -0.0549   0.9811   0.0190
  -5.500  -0.3765   0.01026   0.00487  -0.0562   0.9784   0.0199
  -5.250  -0.3431   0.00972   0.00432  -0.0575   0.9757   0.0211
  -5.000  -0.3120   0.00945   0.00406  -0.0582   0.9709   0.0223
  -4.750  -0.2817   0.00923   0.00382  -0.0586   0.9648   0.0233
  -4.500  -0.2529   0.00881   0.00340  -0.0588   0.9579   0.0250
  -4.250  -0.2235   0.00856   0.00315  -0.0590   0.9506   0.0263
  -4.000  -0.1958   0.00831   0.00288  -0.0588   0.9416   0.0277
  -3.750  -0.1678   0.00807   0.00263  -0.0587   0.9330   0.0295
  -3.500  -0.1407   0.00789   0.00243  -0.0583   0.9216   0.0308
  -3.250  -0.1136   0.00769   0.00220  -0.0580   0.9099   0.0328
  -3.000  -0.0863   0.00755   0.00203  -0.0576   0.8981   0.0357
  -2.750  -0.0592   0.00737   0.00185  -0.0573   0.8859   0.0425
  -2.500  -0.0324   0.00705   0.00166  -0.0570   0.8726   0.0787
  -2.250  -0.0064   0.00650   0.00145  -0.0568   0.8582   0.1863
  -2.000   0.0187   0.00567   0.00120  -0.0567   0.8446   0.3701
  -1.750   0.0449   0.00521   0.00110  -0.0564   0.8317   0.4929
  -1.500   0.0723   0.00511   0.00109  -0.0562   0.8178   0.5408
  -1.250   0.0998   0.00512   0.00108  -0.0558   0.8005   0.5661
  -1.000   0.1267   0.00516   0.00107  -0.0553   0.7776   0.5864
  -0.750   0.1540   0.00523   0.00109  -0.0549   0.7558   0.6046
  -0.500   0.1815   0.00531   0.00112  -0.0546   0.7364   0.6211
  -0.250   0.2090   0.00540   0.00118  -0.0542   0.7173   0.6355
   0.000   0.2366   0.00547   0.00121  -0.0539   0.6992   0.6457
   0.250   0.2644   0.00555   0.00123  -0.0537   0.6808   0.6506
   0.500   0.2921   0.00565   0.00124  -0.0534   0.6561   0.6544
   0.750   0.3194   0.00577   0.00125  -0.0531   0.6255   0.6581
   1.000   0.3456   0.00596   0.00128  -0.0526   0.5775   0.6622
   1.250   0.3709   0.00631   0.00136  -0.0521   0.5029   0.6661
   1.500   0.3952   0.00683   0.00150  -0.0514   0.4080   0.6700
   1.750   0.4190   0.00749   0.00170  -0.0508   0.2967   0.6736
   2.000   0.4432   0.00806   0.00189  -0.0502   0.2033   0.6776
   2.250   0.4685   0.00849   0.00208  -0.0498   0.1450   0.6817
   2.500   0.4953   0.00874   0.00223  -0.0495   0.1219   0.6857
   2.750   0.5226   0.00893   0.00236  -0.0493   0.1107   0.6896
   3.000   0.5497   0.00913   0.00251  -0.0490   0.1025   0.6933
   3.250   0.5771   0.00925   0.00265  -0.0488   0.0980   0.6976
   3.500   0.6039   0.00946   0.00282  -0.0486   0.0909   0.7018
   3.750   0.6315   0.00958   0.00295  -0.0484   0.0876   0.7061
   4.000   0.6587   0.00975   0.00310  -0.0482   0.0835   0.7101
   4.250   0.6853   0.00995   0.00330  -0.0479   0.0790   0.7148
   4.500   0.7127   0.01005   0.00343  -0.0477   0.0763   0.7195
   4.750   0.7396   0.01023   0.00359  -0.0475   0.0724   0.7246
   5.000   0.7664   0.01042   0.00378  -0.0472   0.0687   0.7298
   5.250   0.7933   0.01055   0.00393  -0.0469   0.0653   0.7354
   5.500   0.8196   0.01079   0.00415  -0.0466   0.0614   0.7414
   5.750   0.8465   0.01093   0.00432  -0.0464   0.0585   0.7476
   6.000   0.8725   0.01117   0.00455  -0.0460   0.0548   0.7552
   6.250   0.8990   0.01135   0.00476  -0.0457   0.0518   0.7634
   6.500   0.9245   0.01161   0.00503  -0.0453   0.0480   0.7733
   6.750   0.9505   0.01180   0.00526  -0.0449   0.0449   0.7845
   7.000   0.9755   0.01207   0.00557  -0.0444   0.0414   0.7994
   7.250   1.0003   0.01231   0.00587  -0.0438   0.0384   0.8216
   7.500   1.0228   0.01247   0.00621  -0.0427   0.0361   0.8729
   7.750   1.0497   0.01262   0.00652  -0.0425   0.0340   1.0000
   8.000   1.0744   0.01306   0.00695  -0.0420   0.0323   1.0000
   8.250   1.0995   0.01340   0.00731  -0.0416   0.0311   1.0000
   8.500   1.1242   0.01379   0.00770  -0.0411   0.0300   1.0000
   8.750   1.1476   0.01431   0.00823  -0.0404   0.0289   1.0000
   9.000   1.1715   0.01477   0.00872  -0.0398   0.0282   1.0000
   9.250   1.1956   0.01517   0.00916  -0.0392   0.0276   1.0000
   9.500   1.2194   0.01560   0.00961  -0.0386   0.0269   1.0000
   9.750   1.2425   0.01607   0.01011  -0.0379   0.0263   1.0000
  10.000   1.2649   0.01661   0.01068  -0.0371   0.0258   1.0000
  10.250   1.2853   0.01735   0.01145  -0.0361   0.0252   1.0000
  10.500   1.3053   0.01811   0.01226  -0.0350   0.0248   1.0000
  10.750   1.3271   0.01863   0.01284  -0.0342   0.0246   1.0000
  11.000   1.3481   0.01921   0.01348  -0.0332   0.0243   1.0000
  11.250   1.3684   0.01983   0.01417  -0.0322   0.0240   1.0000
  11.500   1.3879   0.02049   0.01488  -0.0311   0.0237   1.0000
  11.750   1.4067   0.02118   0.01563  -0.0299   0.0234   1.0000
  12.000   1.4246   0.02189   0.01640  -0.0286   0.0231   1.0000
  12.250   1.4414   0.02265   0.01722  -0.0272   0.0229   1.0000
  12.500   1.4569   0.02344   0.01807  -0.0257   0.0227   1.0000
  12.750   1.4693   0.02427   0.01895  -0.0236   0.0224   1.0000
  13.000   1.4783   0.02519   0.01993  -0.0211   0.0222   1.0000
  13.250   1.4854   0.02624   0.02106  -0.0186   0.0221   1.0000
  13.500   1.4890   0.02761   0.02251  -0.0158   0.0219   1.0000
  13.750   1.4900   0.02928   0.02428  -0.0132   0.0217   1.0000
  14.000   1.4916   0.03099   0.02611  -0.0109   0.0215   1.0000
  14.250   1.4968   0.03241   0.02763  -0.0091   0.0215   1.0000
  14.500   1.5018   0.03388   0.02922  -0.0076   0.0214   1.0000
  14.750   1.5051   0.03561   0.03105  -0.0062   0.0213   1.0000
  15.000   1.5061   0.03765   0.03322  -0.0051   0.0212   1.0000
  15.250   1.5066   0.03985   0.03553  -0.0042   0.0211   1.0000
  15.500   1.5060   0.04230   0.03810  -0.0037   0.0210   1.0000
  15.750   1.5031   0.04514   0.04106  -0.0035   0.0210   1.0000
  16.000   1.4985   0.04836   0.04442  -0.0037   0.0209   1.0000
  16.250   1.4926   0.05192   0.04812  -0.0044   0.0208   1.0000
  16.500   1.4849   0.05596   0.05228  -0.0056   0.0207   1.0000
  16.750   1.4758   0.06045   0.05692  -0.0073   0.0206   1.0000
  17.000   1.4631   0.06579   0.06240  -0.0098   0.0206   1.0000
  17.250   1.4491   0.07177   0.06853  -0.0130   0.0205   1.0000
  17.500   1.4314   0.07880   0.07572  -0.0171   0.0205   1.0000
  17.750   1.4107   0.08689   0.08397  -0.0221   0.0204   1.0000
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