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SD7062 (14%) (sd7062-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: SD7062 (14%) (sd7062-il)
Reynolds number: 1,000,000
Max Cl/Cd: 113.49 at α=6.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-sd7062-il-1000000-n5.txt
Download as CSV file: xf-sd7062-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: SD7062 (14%)                                    
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -14.000  -0.7847   0.05436   0.05160  -0.0715   1.0000   0.0107
 -13.750  -0.8129   0.04574   0.04280  -0.0784   1.0000   0.0107
 -13.500  -0.8281   0.03960   0.03650  -0.0837   1.0000   0.0107
 -13.250  -0.8415   0.03454   0.03129  -0.0879   1.0000   0.0107
 -13.000  -0.8541   0.03103   0.02764  -0.0897   1.0000   0.0107
 -12.750  -0.8594   0.02866   0.02515  -0.0900   0.9900   0.0108
 -12.500  -0.8350   0.02662   0.02294  -0.0934   0.9779   0.0109
 -12.250  -0.8089   0.02488   0.02105  -0.0961   0.9628   0.0109
 -12.000  -0.7857   0.02357   0.01957  -0.0973   0.9416   0.0110
 -11.750  -0.7702   0.02249   0.01832  -0.0965   0.9161   0.0111
 -11.500  -0.7544   0.02162   0.01727  -0.0953   0.8935   0.0112
 -11.250  -0.7372   0.02078   0.01628  -0.0943   0.8753   0.0112
 -11.000  -0.7182   0.02003   0.01538  -0.0934   0.8597   0.0113
 -10.750  -0.6977   0.01935   0.01456  -0.0926   0.8460   0.0114
 -10.500  -0.6761   0.01874   0.01382  -0.0919   0.8340   0.0115
 -10.250  -0.6534   0.01817   0.01314  -0.0914   0.8222   0.0115
 -10.000  -0.6330   0.01722   0.01207  -0.0907   0.8117   0.0117
  -9.750  -0.6105   0.01655   0.01130  -0.0901   0.8008   0.0119
  -9.500  -0.5864   0.01600   0.01067  -0.0897   0.7910   0.0120
  -9.250  -0.5621   0.01550   0.01007  -0.0893   0.7812   0.0122
  -9.000  -0.5368   0.01504   0.00955  -0.0889   0.7719   0.0123
  -8.750  -0.5115   0.01462   0.00905  -0.0886   0.7628   0.0124
  -8.500  -0.4858   0.01419   0.00855  -0.0883   0.7537   0.0126
  -8.250  -0.4599   0.01381   0.00808  -0.0880   0.7447   0.0127
  -8.000  -0.4336   0.01342   0.00763  -0.0877   0.7356   0.0129
  -7.750  -0.4073   0.01306   0.00719  -0.0874   0.7268   0.0131
  -7.500  -0.3806   0.01271   0.00678  -0.0872   0.7177   0.0133
  -7.250  -0.3539   0.01239   0.00638  -0.0870   0.7092   0.0134
  -7.000  -0.3268   0.01207   0.00600  -0.0868   0.7002   0.0136
  -6.750  -0.2997   0.01179   0.00565  -0.0866   0.6916   0.0138
  -6.500  -0.2723   0.01151   0.00532  -0.0864   0.6825   0.0140
  -6.250  -0.2449   0.01128   0.00501  -0.0862   0.6737   0.0142
  -6.000  -0.2172   0.01103   0.00472  -0.0861   0.6648   0.0143
  -5.750  -0.1901   0.01070   0.00433  -0.0859   0.6562   0.0147
  -5.500  -0.1623   0.01045   0.00403  -0.0858   0.6471   0.0150
  -5.250  -0.1346   0.01025   0.00379  -0.0856   0.6381   0.0154
  -5.000  -0.1065   0.01007   0.00356  -0.0855   0.6290   0.0157
  -4.750  -0.0785   0.00991   0.00336  -0.0854   0.6201   0.0162
  -4.500  -0.0503   0.00977   0.00317  -0.0853   0.6104   0.0167
  -4.250  -0.0221   0.00965   0.00300  -0.0852   0.6016   0.0172
  -4.000   0.0060   0.00949   0.00280  -0.0851   0.5919   0.0177
  -3.750   0.0343   0.00935   0.00262  -0.0851   0.5830   0.0184
  -3.500   0.0625   0.00925   0.00248  -0.0850   0.5730   0.0193
  -3.250   0.0909   0.00915   0.00235  -0.0849   0.5640   0.0202
  -3.000   0.1191   0.00907   0.00222  -0.0848   0.5540   0.0217
  -2.750   0.1476   0.00898   0.00211  -0.0848   0.5449   0.0242
  -2.500   0.1757   0.00887   0.00200  -0.0847   0.5354   0.0314
  -2.250   0.2039   0.00872   0.00190  -0.0847   0.5260   0.0501
  -2.000   0.2321   0.00860   0.00182  -0.0846   0.5169   0.0691
  -1.750   0.2603   0.00849   0.00175  -0.0846   0.5071   0.0906
  -1.500   0.2885   0.00839   0.00170  -0.0846   0.4982   0.1157
  -1.250   0.3165   0.00825   0.00165  -0.0846   0.4884   0.1553
  -1.000   0.3446   0.00811   0.00161  -0.0846   0.4795   0.1988
  -0.750   0.3725   0.00801   0.00160  -0.0846   0.4698   0.2443
  -0.500   0.4006   0.00788   0.00159  -0.0846   0.4606   0.2929
  -0.250   0.4285   0.00781   0.00160  -0.0846   0.4511   0.3392
   0.000   0.4565   0.00769   0.00162  -0.0846   0.4419   0.3972
   0.250   0.4845   0.00767   0.00166  -0.0845   0.4326   0.4362
   0.500   0.5126   0.00767   0.00169  -0.0845   0.4232   0.4649
   0.750   0.5406   0.00769   0.00174  -0.0844   0.4141   0.4949
   1.000   0.5686   0.00771   0.00180  -0.0844   0.4051   0.5261
   1.250   0.5966   0.00774   0.00186  -0.0843   0.3964   0.5526
   1.500   0.6244   0.00779   0.00193  -0.0842   0.3870   0.5772
   1.750   0.6523   0.00784   0.00199  -0.0841   0.3789   0.6021
   2.000   0.6799   0.00791   0.00208  -0.0840   0.3697   0.6266
   2.250   0.7077   0.00795   0.00216  -0.0839   0.3615   0.6528
   2.500   0.7350   0.00804   0.00226  -0.0837   0.3529   0.6792
   2.750   0.7625   0.00809   0.00236  -0.0836   0.3446   0.7072
   3.000   0.7894   0.00818   0.00247  -0.0833   0.3357   0.7353
   3.250   0.8165   0.00823   0.00258  -0.0831   0.3281   0.7651
   3.500   0.8428   0.00833   0.00271  -0.0827   0.3194   0.7964
   3.750   0.8690   0.00838   0.00283  -0.0823   0.3118   0.8307
   4.000   0.8935   0.00846   0.00297  -0.0815   0.3035   0.8703
   4.250   0.9164   0.00847   0.00308  -0.0803   0.2964   0.9214
   4.500   0.9494   0.00859   0.00321  -0.0813   0.2877   1.0000
   4.750   0.9765   0.00875   0.00333  -0.0812   0.2804   1.0000
   5.250   1.0296   0.00914   0.00364  -0.0808   0.2651   1.0000
   5.500   1.0556   0.00937   0.00381  -0.0805   0.2566   1.0000
   5.750   1.0821   0.00955   0.00396  -0.0802   0.2504   1.0000
   6.000   1.1078   0.00979   0.00415  -0.0799   0.2425   1.0000
   6.250   1.1338   0.00999   0.00433  -0.0796   0.2358   1.0000
   6.500   1.1594   0.01022   0.00453  -0.0793   0.2291   1.0000
   6.750   1.1848   0.01045   0.00473  -0.0789   0.2228   1.0000
   7.000   1.2099   0.01070   0.00495  -0.0785   0.2153   1.0000
   7.250   1.2346   0.01096   0.00518  -0.0781   0.2091   1.0000
   7.500   1.2596   0.01119   0.00540  -0.0777   0.2032   1.0000
   7.750   1.2831   0.01151   0.00567  -0.0770   0.1956   1.0000
   8.000   1.3077   0.01174   0.00589  -0.0766   0.1909   1.0000
   8.250   1.3311   0.01204   0.00617  -0.0759   0.1845   1.0000
   8.500   1.3542   0.01234   0.00645  -0.0753   0.1786   1.0000
   8.750   1.3772   0.01263   0.00673  -0.0746   0.1729   1.0000
   9.000   1.3987   0.01299   0.00706  -0.0737   0.1668   1.0000
   9.250   1.4210   0.01328   0.00735  -0.0729   0.1616   1.0000
   9.500   1.4414   0.01365   0.00770  -0.0718   0.1558   1.0000
   9.750   1.4619   0.01400   0.00804  -0.0708   0.1510   1.0000
  10.000   1.4805   0.01435   0.00839  -0.0694   0.1457   1.0000
  10.250   1.4957   0.01479   0.00880  -0.0674   0.1401   1.0000
  10.500   1.5125   0.01515   0.00918  -0.0658   0.1361   1.0000
  10.750   1.5274   0.01560   0.00963  -0.0639   0.1312   1.0000
  11.000   1.5415   0.01612   0.01013  -0.0620   0.1264   1.0000
  11.250   1.5564   0.01661   0.01064  -0.0603   0.1219   1.0000
  11.500   1.5692   0.01723   0.01125  -0.0584   0.1172   1.0000
  11.750   1.5828   0.01782   0.01186  -0.0567   0.1134   1.0000
  12.000   1.5959   0.01847   0.01252  -0.0550   0.1094   1.0000
  12.250   1.6069   0.01926   0.01332  -0.0532   0.1052   1.0000
  12.500   1.6189   0.02004   0.01412  -0.0516   0.1018   1.0000
  12.750   1.6305   0.02088   0.01498  -0.0501   0.0983   1.0000
  13.000   1.6399   0.02189   0.01600  -0.0485   0.0945   1.0000
  13.250   1.6496   0.02294   0.01707  -0.0471   0.0910   1.0000
  13.500   1.6597   0.02400   0.01816  -0.0458   0.0880   1.0000
  13.750   1.6672   0.02529   0.01947  -0.0445   0.0845   1.0000
  14.000   1.6747   0.02664   0.02085  -0.0432   0.0816   1.0000
  14.250   1.6837   0.02793   0.02219  -0.0422   0.0793   1.0000
  14.500   1.6904   0.02945   0.02374  -0.0412   0.0765   1.0000
  14.750   1.6950   0.03119   0.02551  -0.0402   0.0738   1.0000
  15.000   1.7006   0.03291   0.02728  -0.0393   0.0713   1.0000
  15.250   1.7056   0.03475   0.02916  -0.0386   0.0688   1.0000
  15.500   1.7082   0.03685   0.03130  -0.0380   0.0664   1.0000
  15.750   1.7089   0.03922   0.03371  -0.0374   0.0638   1.0000
  16.000   1.7130   0.04134   0.03590  -0.0370   0.0623   1.0000
  16.250   1.7141   0.04384   0.03846  -0.0368   0.0598   1.0000
  16.500   1.7116   0.04680   0.04146  -0.0367   0.0572   1.0000
  16.750   1.7103   0.04974   0.04446  -0.0367   0.0551   1.0000
  17.000   1.7097   0.05270   0.04748  -0.0369   0.0533   1.0000
  17.250   1.7065   0.05603   0.05088  -0.0373   0.0513   1.0000
  17.500   1.7002   0.05986   0.05476  -0.0379   0.0491   1.0000
  17.750   1.6969   0.06343   0.05840  -0.0386   0.0474   1.0000
  18.000   1.6928   0.06715   0.06221  -0.0394   0.0460   1.0000
  18.250   1.6865   0.07129   0.06642  -0.0404   0.0446   1.0000
  18.500   1.6775   0.07589   0.07109  -0.0417   0.0430   1.0000
  18.750   1.6705   0.08030   0.07559  -0.0431   0.0420   1.0000
  19.000   1.6634   0.08482   0.08019  -0.0446   0.0406   1.0000
  19.250   1.6547   0.08966   0.08512  -0.0463   0.0393   1.0000
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