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N-11 (n11-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: N-11 (n11-il)
Reynolds number: 1,000,000
Max Cl/Cd: 111.61 at α=4°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-n11-il-1000000-n5.txt
Download as CSV file: xf-n11-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: N-11                                            
  
 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  -1.0256   0.03176   0.02915  -0.0990   0.9974   0.0108
 -15.250  -1.0076   0.02913   0.02634  -0.1011   0.9956   0.0113
 -15.000  -0.9854   0.02713   0.02419  -0.1028   0.9943   0.0118
 -14.750  -0.9652   0.02547   0.02237  -0.1034   0.9922   0.0122
 -14.500  -0.9429   0.02401   0.02076  -0.1040   0.9902   0.0127
 -14.250  -0.9149   0.02343   0.02016  -0.1046   0.9889   0.0133
 -14.000  -0.8855   0.02298   0.01969  -0.1053   0.9877   0.0138
 -13.750  -0.8561   0.02244   0.01910  -0.1061   0.9866   0.0143
 -13.500  -0.8274   0.02168   0.01825  -0.1069   0.9857   0.0148
 -13.250  -0.7994   0.02077   0.01722  -0.1078   0.9846   0.0153
 -13.000  -0.7762   0.01991   0.01623  -0.1075   0.9814   0.0157
 -12.750  -0.7501   0.01911   0.01531  -0.1077   0.9788   0.0160
 -12.500  -0.7211   0.01872   0.01489  -0.1081   0.9766   0.0164
 -12.250  -0.6909   0.01856   0.01473  -0.1086   0.9748   0.0168
 -12.000  -0.6619   0.01844   0.01460  -0.1088   0.9724   0.0171
 -11.750  -0.6357   0.01823   0.01437  -0.1085   0.9680   0.0175
 -11.500  -0.6078   0.01787   0.01396  -0.1086   0.9634   0.0178
 -11.250  -0.5819   0.01742   0.01343  -0.1083   0.9568   0.0182
 -11.000  -0.5557   0.01696   0.01287  -0.1081   0.9489   0.0187
 -10.750  -0.5301   0.01653   0.01236  -0.1077   0.9405   0.0191
 -10.500  -0.5040   0.01608   0.01180  -0.1074   0.9320   0.0195
 -10.250  -0.4783   0.01565   0.01127  -0.1070   0.9205   0.0198
 -10.000  -0.4520   0.01533   0.01084  -0.1066   0.9065   0.0200
  -9.750  -0.4272   0.01471   0.01006  -0.1061   0.8889   0.0203
  -9.500  -0.4027   0.01407   0.00927  -0.1056   0.8715   0.0208
  -9.250  -0.3768   0.01376   0.00885  -0.1052   0.8568   0.0211
  -8.750  -0.3238   0.01321   0.00813  -0.1046   0.8353   0.0217
  -8.500  -0.2973   0.01286   0.00769  -0.1043   0.8275   0.0220
  -8.250  -0.2702   0.01257   0.00733  -0.1041   0.8203   0.0224
  -7.750  -0.2163   0.01189   0.00648  -0.1036   0.8076   0.0231
  -7.500  -0.1892   0.01153   0.00604  -0.1034   0.8018   0.0235
  -7.250  -0.1621   0.01121   0.00564  -0.1032   0.7958   0.0238
  -7.000  -0.1348   0.01090   0.00526  -0.1030   0.7884   0.0241
  -6.750  -0.1075   0.01067   0.00496  -0.1028   0.7804   0.0245
  -6.500  -0.0798   0.01045   0.00468  -0.1026   0.7724   0.0248
  -6.250  -0.0524   0.01023   0.00439  -0.1024   0.7653   0.0250
  -6.000  -0.0247   0.00999   0.00411  -0.1023   0.7574   0.0251
  -5.750   0.0028   0.00980   0.00385  -0.1021   0.7483   0.0253
  -5.500   0.0303   0.00960   0.00359  -0.1019   0.7376   0.0254
  -5.250   0.0574   0.00924   0.00315  -0.1018   0.7281   0.0258
  -5.000   0.0847   0.00899   0.00283  -0.1015   0.7167   0.0262
  -4.750   0.1119   0.00881   0.00258  -0.1013   0.7015   0.0266
  -4.500   0.1391   0.00868   0.00236  -0.1011   0.6845   0.0271
  -4.250   0.1661   0.00859   0.00219  -0.1008   0.6651   0.0275
  -4.000   0.1930   0.00855   0.00204  -0.1005   0.6451   0.0280
  -3.750   0.2201   0.00851   0.00193  -0.1003   0.6278   0.0286
  -3.500   0.2476   0.00847   0.00182  -0.1002   0.6138   0.0293
  -3.250   0.2753   0.00842   0.00173  -0.1000   0.6021   0.0300
  -3.000   0.3029   0.00839   0.00164  -0.0999   0.5905   0.0306
  -2.750   0.3305   0.00838   0.00157  -0.0998   0.5786   0.0312
  -2.500   0.3581   0.00838   0.00152  -0.0997   0.5666   0.0317
  -2.250   0.3860   0.00837   0.00147  -0.0997   0.5563   0.0322
  -2.000   0.4137   0.00836   0.00142  -0.0996   0.5465   0.0338
  -1.750   0.4412   0.00837   0.00140  -0.0995   0.5341   0.0366
  -1.500   0.4686   0.00837   0.00138  -0.0994   0.5206   0.0443
  -1.250   0.4957   0.00829   0.00138  -0.0993   0.5065   0.0870
  -1.000   0.5230   0.00827   0.00140  -0.0992   0.4926   0.1135
  -0.750   0.5498   0.00827   0.00144  -0.0991   0.4755   0.1532
  -0.500   0.5765   0.00831   0.00149  -0.0990   0.4560   0.1868
  -0.250   0.6032   0.00838   0.00155  -0.0988   0.4355   0.2136
   0.000   0.6293   0.00844   0.00163  -0.0986   0.4110   0.2637
   0.250   0.6550   0.00848   0.00173  -0.0984   0.3852   0.3351
   0.500   0.6806   0.00847   0.00186  -0.0982   0.3646   0.4291
   0.750   0.7059   0.00833   0.00200  -0.0980   0.3479   0.5728
   1.000   0.7324   0.00759   0.00222  -0.0977   0.3319   0.9895
   1.250   0.7624   0.00779   0.00233  -0.0983   0.3184   1.0000
   1.500   0.7888   0.00793   0.00242  -0.0981   0.3104   1.0000
   1.750   0.8151   0.00808   0.00252  -0.0979   0.3041   1.0000
   2.000   0.8419   0.00820   0.00262  -0.0977   0.2995   1.0000
   2.250   0.8685   0.00832   0.00272  -0.0976   0.2944   1.0000
   2.500   0.8949   0.00848   0.00284  -0.0974   0.2890   1.0000
   2.750   0.9216   0.00860   0.00295  -0.0973   0.2848   1.0000
   3.000   0.9481   0.00874   0.00306  -0.0972   0.2792   1.0000
   3.250   0.9741   0.00893   0.00321  -0.0970   0.2721   1.0000
   3.500   1.0006   0.00906   0.00334  -0.0969   0.2661   1.0000
   3.750   1.0265   0.00925   0.00348  -0.0967   0.2590   1.0000
   4.000   1.0525   0.00943   0.00364  -0.0965   0.2504   1.0000
   4.250   1.0775   0.00968   0.00382  -0.0962   0.2364   1.0000
   4.500   1.1014   0.01001   0.00404  -0.0957   0.2165   1.0000
   4.750   1.1241   0.01043   0.00433  -0.0950   0.1914   1.0000
   5.000   1.1473   0.01080   0.00461  -0.0944   0.1754   1.0000
   5.250   1.1709   0.01114   0.00488  -0.0939   0.1633   1.0000
   5.500   1.1946   0.01147   0.00516  -0.0934   0.1529   1.0000
   5.750   1.2178   0.01181   0.00546  -0.0929   0.1428   1.0000
   6.000   1.2399   0.01224   0.00580  -0.0921   0.1257   1.0000
   6.500   1.2762   0.01365   0.00688  -0.0895   0.0729   1.0000
   6.750   1.2979   0.01405   0.00727  -0.0887   0.0647   1.0000
   7.000   1.3157   0.01472   0.00782  -0.0873   0.0471   1.0000
   7.250   1.3269   0.01586   0.00877  -0.0849   0.0155   1.0000
   7.500   1.3462   0.01633   0.00925  -0.0837   0.0130   1.0000
   7.750   1.3650   0.01673   0.00968  -0.0825   0.0121   1.0000
   8.000   1.3830   0.01717   0.01016  -0.0811   0.0113   1.0000
   8.250   1.4000   0.01767   0.01068  -0.0796   0.0105   1.0000
   8.500   1.4160   0.01823   0.01128  -0.0780   0.0096   1.0000
   8.750   1.4326   0.01876   0.01184  -0.0765   0.0092   1.0000
   9.000   1.4490   0.01930   0.01242  -0.0751   0.0088   1.0000
   9.250   1.4647   0.01989   0.01306  -0.0736   0.0083   1.0000
   9.500   1.4794   0.02055   0.01375  -0.0721   0.0079   1.0000
   9.750   1.4932   0.02127   0.01451  -0.0705   0.0075   1.0000
  10.000   1.5054   0.02212   0.01541  -0.0687   0.0071   1.0000
  10.250   1.5176   0.02299   0.01633  -0.0671   0.0069   1.0000
  10.500   1.5303   0.02384   0.01725  -0.0656   0.0067   1.0000
  10.750   1.5421   0.02478   0.01824  -0.0642   0.0065   1.0000
  11.000   1.5532   0.02581   0.01933  -0.0628   0.0063   1.0000
  11.250   1.5635   0.02693   0.02050  -0.0614   0.0061   1.0000
  11.500   1.5733   0.02812   0.02176  -0.0601   0.0059   1.0000
  11.750   1.5822   0.02944   0.02313  -0.0588   0.0057   1.0000
  12.000   1.5900   0.03088   0.02463  -0.0576   0.0055   1.0000
  12.250   1.5961   0.03253   0.02635  -0.0564   0.0053   1.0000
  12.500   1.5999   0.03445   0.02835  -0.0552   0.0051   1.0000
  12.750   1.6030   0.03648   0.03046  -0.0541   0.0050   1.0000
  13.000   1.6074   0.03846   0.03252  -0.0532   0.0049   1.0000
  13.250   1.6102   0.04065   0.03480  -0.0524   0.0048   1.0000
  13.500   1.6120   0.04304   0.03728  -0.0518   0.0047   1.0000
  13.750   1.6126   0.04563   0.03996  -0.0513   0.0047   1.0000
  14.000   1.6119   0.04848   0.04291  -0.0510   0.0046   1.0000
  14.250   1.6102   0.05157   0.04610  -0.0508   0.0045   1.0000
  14.500   1.6076   0.05488   0.04950  -0.0509   0.0044   1.0000
  14.750   1.6032   0.05849   0.05322  -0.0511   0.0044   1.0000
  15.000   1.5977   0.06237   0.05721  -0.0515   0.0043   1.0000
  15.250   1.5911   0.06652   0.06146  -0.0521   0.0042   1.0000
  15.500   1.5828   0.07099   0.06604  -0.0529   0.0042   1.0000
  15.750   1.5735   0.07565   0.07081  -0.0539   0.0041   1.0000
  16.000   1.5624   0.08072   0.07600  -0.0550   0.0041   1.0000
  16.250   1.5505   0.08600   0.08139  -0.0564   0.0041   1.0000
  16.500   1.5368   0.09165   0.08715  -0.0579   0.0040   1.0000
  16.750   1.5231   0.09736   0.09298  -0.0596   0.0040   1.0000
  17.000   1.5082   0.10343   0.09916  -0.0615   0.0040   1.0000
  17.250   1.4940   0.10944   0.10528  -0.0635   0.0039   1.0000
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