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RAE(NPL) 5213 AIRFOIL (rae5213-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: RAE(NPL) 5213 AIRFOIL (rae5213-il)
Reynolds number: 1,000,000
Max Cl/Cd: 80.58 at α=9.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-rae5213-il-1000000-n5.txt
Download as CSV file: xf-rae5213-il-1000000-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 =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.500  -1.0513   0.06321   0.06051  -0.0448   1.0000   0.0062
 -15.250  -1.0889   0.05275   0.04981  -0.0525   1.0000   0.0062
 -15.000  -1.1132   0.04595   0.04281  -0.0569   1.0000   0.0061
 -14.750  -1.1233   0.04166   0.03838  -0.0592   1.0000   0.0062
 -14.500  -1.1326   0.03781   0.03437  -0.0609   1.0000   0.0062
 -14.250  -1.1379   0.03470   0.03112  -0.0618   1.0000   0.0061
 -14.000  -1.1402   0.03212   0.02841  -0.0622   1.0000   0.0062
 -13.750  -1.1412   0.03001   0.02619  -0.0620   1.0000   0.0063
 -13.500  -1.1443   0.02829   0.02435  -0.0604   1.0000   0.0063
 -13.250  -1.1378   0.02688   0.02281  -0.0591   1.0000   0.0063
 -13.000  -1.1271   0.02557   0.02139  -0.0581   1.0000   0.0064
 -12.750  -1.1139   0.02439   0.02009  -0.0571   1.0000   0.0065
 -12.500  -1.0990   0.02330   0.01890  -0.0562   1.0000   0.0065
 -12.250  -1.0826   0.02230   0.01780  -0.0553   1.0000   0.0066
 -12.000  -1.0653   0.02136   0.01676  -0.0544   1.0000   0.0067
 -11.750  -1.0470   0.02050   0.01580  -0.0535   1.0000   0.0068
 -11.500  -1.0282   0.01967   0.01489  -0.0526   1.0000   0.0069
 -11.250  -1.0086   0.01894   0.01407  -0.0517   1.0000   0.0070
 -11.000  -0.9886   0.01822   0.01328  -0.0508   1.0000   0.0070
 -10.750  -0.9682   0.01758   0.01256  -0.0499   1.0000   0.0072
 -10.500  -0.9479   0.01690   0.01181  -0.0489   1.0000   0.0073
 -10.250  -0.9276   0.01623   0.01109  -0.0479   1.0000   0.0075
 -10.000  -0.9066   0.01568   0.01050  -0.0469   1.0000   0.0077
  -9.750  -0.8834   0.01517   0.00995  -0.0464   0.9997   0.0079
  -9.500  -0.8528   0.01466   0.00940  -0.0474   0.9982   0.0082
  -9.250  -0.8221   0.01417   0.00887  -0.0483   0.9963   0.0085
  -9.000  -0.7910   0.01369   0.00834  -0.0493   0.9944   0.0088
  -8.750  -0.7613   0.01323   0.00783  -0.0500   0.9920   0.0091
  -8.500  -0.7307   0.01279   0.00735  -0.0508   0.9897   0.0094
  -8.250  -0.6994   0.01237   0.00692  -0.0517   0.9876   0.0098
  -8.000  -0.6671   0.01202   0.00656  -0.0529   0.9860   0.0103
  -7.750  -0.6351   0.01169   0.00622  -0.0539   0.9840   0.0108
  -7.500  -0.6056   0.01135   0.00586  -0.0544   0.9800   0.0113
  -7.250  -0.5742   0.01102   0.00551  -0.0552   0.9766   0.0118
  -7.000  -0.5424   0.01074   0.00522  -0.0561   0.9734   0.0123
  -6.750  -0.5140   0.01049   0.00497  -0.0563   0.9667   0.0130
  -6.500  -0.4834   0.01022   0.00468  -0.0569   0.9609   0.0136
  -6.250  -0.4540   0.00998   0.00440  -0.0572   0.9536   0.0142
  -6.000  -0.4245   0.00972   0.00414  -0.0575   0.9465   0.0149
  -5.750  -0.3960   0.00951   0.00391  -0.0576   0.9374   0.0156
  -5.500  -0.3680   0.00931   0.00369  -0.0575   0.9279   0.0164
  -5.250  -0.3404   0.00914   0.00347  -0.0574   0.9175   0.0169
  -5.000  -0.3132   0.00892   0.00323  -0.0571   0.9064   0.0178
  -4.750  -0.2859   0.00876   0.00304  -0.0569   0.8961   0.0186
  -4.500  -0.2585   0.00862   0.00287  -0.0567   0.8857   0.0196
  -4.250  -0.2311   0.00845   0.00266  -0.0565   0.8755   0.0205
  -4.000  -0.2039   0.00830   0.00248  -0.0562   0.8651   0.0217
  -3.750  -0.1763   0.00815   0.00232  -0.0561   0.8545   0.0227
  -3.500  -0.1487   0.00803   0.00215  -0.0559   0.8433   0.0235
  -3.000  -0.0939   0.00779   0.00184  -0.0554   0.8157   0.0266
  -2.750  -0.0663   0.00768   0.00171  -0.0552   0.8024   0.0292
  -2.500  -0.0389   0.00759   0.00159  -0.0549   0.7869   0.0347
  -2.250  -0.0117   0.00747   0.00148  -0.0547   0.7692   0.0494
  -2.000   0.0157   0.00736   0.00138  -0.0545   0.7538   0.0676
  -1.750   0.0432   0.00717   0.00128  -0.0543   0.7410   0.1054
  -1.500   0.0706   0.00691   0.00117  -0.0543   0.7269   0.1635
  -1.250   0.0971   0.00654   0.00104  -0.0542   0.7064   0.2642
  -1.000   0.1226   0.00605   0.00091  -0.0540   0.6754   0.4083
  -0.750   0.1484   0.00582   0.00088  -0.0536   0.6384   0.5159
  -0.500   0.1749   0.00587   0.00092  -0.0533   0.5991   0.5624
  -0.250   0.2013   0.00605   0.00098  -0.0528   0.5478   0.5882
   0.000   0.2274   0.00632   0.00105  -0.0524   0.4864   0.6044
   0.250   0.2538   0.00659   0.00113  -0.0520   0.4315   0.6114
   0.500   0.2798   0.00696   0.00122  -0.0517   0.3614   0.6156
   0.750   0.3056   0.00737   0.00134  -0.0513   0.2878   0.6193
   1.000   0.3314   0.00776   0.00146  -0.0509   0.2195   0.6230
   1.250   0.3574   0.00812   0.00160  -0.0506   0.1619   0.6270
   1.500   0.3845   0.00835   0.00171  -0.0503   0.1323   0.6312
   1.750   0.4118   0.00854   0.00181  -0.0502   0.1138   0.6351
   2.250   0.4670   0.00882   0.00201  -0.0498   0.0981   0.6425
   2.500   0.4945   0.00895   0.00212  -0.0496   0.0929   0.6463
   2.750   0.5222   0.00908   0.00224  -0.0495   0.0890   0.6502
   3.000   0.5498   0.00921   0.00235  -0.0493   0.0855   0.6537
   3.500   0.6046   0.00950   0.00261  -0.0489   0.0769   0.6604
   3.750   0.6319   0.00965   0.00274  -0.0487   0.0721   0.6642
   4.000   0.6591   0.00981   0.00289  -0.0485   0.0686   0.6679
   4.250   0.6864   0.00996   0.00303  -0.0483   0.0653   0.6714
   4.750   0.7405   0.01029   0.00335  -0.0479   0.0584   0.6787
   5.000   0.7672   0.01049   0.00352  -0.0476   0.0544   0.6828
   5.250   0.7941   0.01067   0.00371  -0.0473   0.0514   0.6868
   5.500   0.8206   0.01089   0.00391  -0.0471   0.0482   0.6906
   5.750   0.8472   0.01108   0.00411  -0.0468   0.0456   0.6946
   6.000   0.8734   0.01130   0.00434  -0.0464   0.0427   0.6994
   6.250   0.8998   0.01152   0.00457  -0.0461   0.0403   0.7044
   6.500   0.9258   0.01178   0.00482  -0.0458   0.0375   0.7091
   6.750   0.9518   0.01200   0.00507  -0.0454   0.0351   0.7140
   7.000   0.9774   0.01228   0.00536  -0.0450   0.0324   0.7197
   7.250   1.0031   0.01255   0.00564  -0.0446   0.0302   0.7256
   7.500   1.0284   0.01285   0.00595  -0.0442   0.0283   0.7324
   7.750   1.0537   0.01313   0.00627  -0.0437   0.0270   0.7409
   8.000   1.0786   0.01344   0.00661  -0.0432   0.0258   0.7497
   8.250   1.1033   0.01377   0.00699  -0.0427   0.0248   0.7601
   8.500   1.1280   0.01406   0.00735  -0.0422   0.0242   0.7720
   8.750   1.1524   0.01437   0.00772  -0.0416   0.0235   0.7868
   9.000   1.1763   0.01468   0.00812  -0.0410   0.0229   0.8079
   9.250   1.1987   0.01496   0.00854  -0.0400   0.0224   0.8500
   9.500   1.2224   0.01517   0.00899  -0.0393   0.0218   1.0000
   9.750   1.2460   0.01560   0.00945  -0.0387   0.0214   1.0000
  10.000   1.2697   0.01600   0.00989  -0.0381   0.0210   1.0000
  10.250   1.2929   0.01643   0.01036  -0.0374   0.0207   1.0000
  10.500   1.3158   0.01688   0.01085  -0.0367   0.0203   1.0000
  10.750   1.3382   0.01735   0.01136  -0.0360   0.0200   1.0000
  11.000   1.3602   0.01786   0.01190  -0.0352   0.0198   1.0000
  11.250   1.3817   0.01838   0.01247  -0.0343   0.0195   1.0000
  11.500   1.4026   0.01894   0.01306  -0.0334   0.0192   1.0000
  11.750   1.4227   0.01955   0.01371  -0.0324   0.0190   1.0000
  12.000   1.4415   0.02023   0.01444  -0.0312   0.0187   1.0000
  12.250   1.4593   0.02096   0.01524  -0.0300   0.0185   1.0000
  12.500   1.4779   0.02157   0.01590  -0.0288   0.0184   1.0000
  12.750   1.4955   0.02221   0.01662  -0.0275   0.0182   1.0000
  13.000   1.5120   0.02288   0.01735  -0.0260   0.0181   1.0000
  13.250   1.5256   0.02357   0.01812  -0.0241   0.0180   1.0000
  13.500   1.5370   0.02430   0.01892  -0.0219   0.0178   1.0000
  13.750   1.5473   0.02510   0.01980  -0.0196   0.0177   1.0000
  14.000   1.5569   0.02597   0.02075  -0.0174   0.0176   1.0000
  14.250   1.5653   0.02694   0.02180  -0.0153   0.0175   1.0000
  14.500   1.5734   0.02797   0.02291  -0.0133   0.0173   1.0000
  14.750   1.5804   0.02914   0.02416  -0.0115   0.0172   1.0000
  15.000   1.5860   0.03045   0.02557  -0.0097   0.0171   1.0000
  15.250   1.5911   0.03189   0.02709  -0.0081   0.0170   1.0000
  15.500   1.5953   0.03347   0.02877  -0.0068   0.0169   1.0000
  15.750   1.5978   0.03529   0.03069  -0.0056   0.0168   1.0000
  16.000   1.5993   0.03732   0.03281  -0.0047   0.0167   1.0000
  16.250   1.5995   0.03960   0.03520  -0.0040   0.0166   1.0000
  16.500   1.5976   0.04225   0.03795  -0.0037   0.0166   1.0000
  16.750   1.5945   0.04519   0.04100  -0.0038   0.0165   1.0000
  17.000   1.5895   0.04855   0.04448  -0.0042   0.0164   1.0000
  17.250   1.5818   0.05248   0.04853  -0.0053   0.0163   1.0000
  17.500   1.5705   0.05718   0.05337  -0.0070   0.0163   1.0000
  17.750   1.5585   0.06237   0.05867  -0.0093   0.0162   1.0000
  18.000   1.5388   0.06920   0.06567  -0.0129   0.0162   1.0000
  18.250   1.5179   0.07688   0.07351  -0.0174   0.0161   1.0000
  18.500   1.4854   0.08728   0.08412  -0.0238   0.0162   1.0000
  18.750   1.4423   0.10054   0.09761  -0.0322   0.0163   1.0000
  19.000   1.3870   0.11689   0.11420  -0.0425   0.0163   1.0000
  19.250   1.3308   0.13387   0.13139  -0.0534   0.0164   1.0000
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