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S8037 (16%) (s8037-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: S8037 (16%) (s8037-il)
Reynolds number: 1,000,000
Max Cl/Cd: 98.48 at α=5.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-s8037-il-1000000-n5.txt
Download as CSV file: xf-s8037-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: S8037 (16%)                                     
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -19.000  -0.6881   0.14556   0.14331  -0.0269   1.0000   0.0058
 -18.750  -0.7316   0.13211   0.12971  -0.0336   1.0000   0.0058
 -18.500  -0.7663   0.12113   0.11862  -0.0391   1.0000   0.0058
 -18.250  -0.8291   0.10537   0.10267  -0.0473   1.0000   0.0058
 -18.000  -0.8807   0.09223   0.08936  -0.0542   1.0000   0.0057
 -17.750  -0.9264   0.08042   0.07736  -0.0606   1.0000   0.0056
 -17.500  -0.9525   0.07225   0.06904  -0.0652   1.0000   0.0057
 -17.250  -0.9827   0.06384   0.06045  -0.0700   1.0000   0.0056
 -17.000  -1.0069   0.05692   0.05337  -0.0737   1.0000   0.0057
 -16.750  -1.0171   0.05243   0.04876  -0.0758   1.0000   0.0057
 -16.500  -1.0267   0.04828   0.04450  -0.0774   1.0000   0.0057
 -16.250  -1.0381   0.04420   0.04029  -0.0787   1.0000   0.0057
 -16.000  -1.0419   0.04124   0.03723  -0.0793   1.0000   0.0057
 -15.750  -1.0421   0.03879   0.03469  -0.0795   1.0000   0.0058
 -15.500  -1.0517   0.03561   0.03139  -0.0794   1.0000   0.0058
 -15.250  -1.0511   0.03358   0.02926  -0.0788   1.0000   0.0058
 -15.000  -1.0507   0.03166   0.02727  -0.0780   1.0000   0.0060
 -14.750  -1.0537   0.02964   0.02515  -0.0766   1.0000   0.0060
 -14.500  -1.0511   0.02819   0.02362  -0.0751   1.0000   0.0060
 -14.250  -1.0478   0.02691   0.02228  -0.0733   1.0000   0.0061
 -14.000  -1.0445   0.02574   0.02105  -0.0711   1.0000   0.0062
 -13.750  -1.0336   0.02465   0.01990  -0.0701   0.9995   0.0064
 -13.500  -1.0104   0.02343   0.01861  -0.0715   0.9967   0.0064
 -13.250  -0.9911   0.02255   0.01767  -0.0714   0.9913   0.0065
 -13.000  -0.9841   0.02184   0.01692  -0.0687   0.9694   0.0067
 -12.750  -0.9348   0.02087   0.01588  -0.0744   0.9491   0.0069
 -12.500  -0.8714   0.01966   0.01456  -0.0833   0.9364   0.0072
 -12.250  -0.8069   0.01856   0.01328  -0.0924   0.9083   0.0075
 -12.000  -0.7801   0.01829   0.01278  -0.0929   0.8619   0.0078
 -11.750  -0.7715   0.01781   0.01212  -0.0899   0.8328   0.0078
 -11.500  -0.7598   0.01740   0.01160  -0.0874   0.8143   0.0078
 -11.250  -0.7496   0.01687   0.01096  -0.0846   0.7997   0.0081
 -11.000  -0.7369   0.01642   0.01044  -0.0822   0.7875   0.0083
 -10.750  -0.7230   0.01605   0.00999  -0.0799   0.7764   0.0086
 -10.500  -0.7080   0.01568   0.00955  -0.0777   0.7667   0.0087
 -10.250  -0.6926   0.01536   0.00916  -0.0755   0.7584   0.0089
 -10.000  -0.6770   0.01503   0.00878  -0.0734   0.7508   0.0091
  -9.750  -0.6613   0.01476   0.00844  -0.0712   0.7436   0.0094
  -9.500  -0.6433   0.01448   0.00811  -0.0694   0.7372   0.0097
  -9.250  -0.6242   0.01419   0.00775  -0.0679   0.7304   0.0099
  -9.000  -0.6047   0.01389   0.00740  -0.0664   0.7249   0.0101
  -8.750  -0.5853   0.01355   0.00701  -0.0649   0.7194   0.0104
  -8.500  -0.5656   0.01323   0.00667  -0.0634   0.7135   0.0110
  -8.250  -0.5447   0.01297   0.00635  -0.0621   0.7086   0.0112
  -8.000  -0.5226   0.01273   0.00609  -0.0611   0.7037   0.0117
  -7.750  -0.5009   0.01248   0.00580  -0.0600   0.6987   0.0122
  -7.250  -0.4568   0.01200   0.00523  -0.0578   0.6891   0.0131
  -7.000  -0.4343   0.01175   0.00496  -0.0568   0.6843   0.0137
  -6.750  -0.4117   0.01153   0.00471  -0.0557   0.6796   0.0143
  -6.500  -0.3886   0.01134   0.00448  -0.0548   0.6753   0.0150
  -6.250  -0.3649   0.01114   0.00425  -0.0540   0.6710   0.0156
  -6.000  -0.3417   0.01091   0.00402  -0.0531   0.6665   0.0169
  -5.750  -0.3181   0.01074   0.00382  -0.0522   0.6623   0.0180
  -5.500  -0.2941   0.01057   0.00363  -0.0514   0.6584   0.0193
  -5.250  -0.2701   0.01037   0.00343  -0.0507   0.6541   0.0217
  -5.000  -0.2463   0.01018   0.00325  -0.0499   0.6496   0.0260
  -4.750  -0.2229   0.00999   0.00307  -0.0490   0.6452   0.0335
  -4.500  -0.1990   0.00980   0.00291  -0.0482   0.6414   0.0428
  -4.000  -0.1507   0.00943   0.00262  -0.0467   0.6322   0.0647
  -3.750  -0.1270   0.00926   0.00248  -0.0458   0.6276   0.0797
  -3.500  -0.1029   0.00907   0.00236  -0.0451   0.6234   0.0992
  -3.250  -0.0791   0.00887   0.00223  -0.0443   0.6182   0.1223
  -3.000  -0.0560   0.00866   0.00211  -0.0434   0.6130   0.1517
  -2.750  -0.0341   0.00837   0.00198  -0.0422   0.6084   0.1995
  -2.500  -0.0131   0.00801   0.00185  -0.0409   0.6035   0.2651
  -2.250   0.0074   0.00766   0.00173  -0.0396   0.5981   0.3349
  -2.000   0.0290   0.00739   0.00164  -0.0383   0.5932   0.3929
  -1.750   0.0524   0.00719   0.00158  -0.0375   0.5884   0.4386
  -1.500   0.0759   0.00704   0.00153  -0.0365   0.5829   0.4780
  -1.250   0.0991   0.00691   0.00149  -0.0356   0.5779   0.5185
  -1.000   0.1235   0.00680   0.00148  -0.0348   0.5731   0.5531
  -0.750   0.1488   0.00675   0.00147  -0.0342   0.5678   0.5728
  -0.250   0.1985   0.00667   0.00146  -0.0329   0.5566   0.6181
   0.000   0.2234   0.00665   0.00147  -0.0322   0.5499   0.6367
   0.250   0.2487   0.00665   0.00148  -0.0317   0.5438   0.6497
   0.500   0.2745   0.00665   0.00149  -0.0312   0.5377   0.6619
   0.750   0.2997   0.00668   0.00150  -0.0306   0.5306   0.6738
   1.000   0.3255   0.00668   0.00152  -0.0302   0.5242   0.6853
   1.250   0.3506   0.00671   0.00155  -0.0296   0.5162   0.6953
   1.500   0.3762   0.00674   0.00158  -0.0291   0.5085   0.7056
   1.750   0.4010   0.00677   0.00161  -0.0284   0.5002   0.7160
   2.000   0.4261   0.00681   0.00165  -0.0279   0.4926   0.7270
   2.250   0.4503   0.00686   0.00170  -0.0271   0.4834   0.7399
   2.500   0.4747   0.00688   0.00175  -0.0264   0.4755   0.7531
   3.000   0.5226   0.00699   0.00187  -0.0248   0.4573   0.7787
   3.250   0.5457   0.00706   0.00195  -0.0238   0.4470   0.7931
   3.500   0.5681   0.00714   0.00203  -0.0227   0.4351   0.8090
   3.750   0.5910   0.00719   0.00212  -0.0217   0.4244   0.8264
   4.000   0.6133   0.00727   0.00222  -0.0206   0.4123   0.8460
   4.250   0.6367   0.00735   0.00234  -0.0198   0.4000   0.8693
   4.500   0.6653   0.00748   0.00249  -0.0201   0.3859   0.8958
   4.750   0.7089   0.00770   0.00272  -0.0239   0.3708   0.9169
   5.000   0.7608   0.00801   0.00297  -0.0296   0.3514   0.9296
   5.250   0.8111   0.00832   0.00322  -0.0349   0.3350   0.9362
   5.500   0.8509   0.00864   0.00348  -0.0378   0.3183   0.9447
   5.750   0.8847   0.00903   0.00378  -0.0395   0.2972   0.9518
   6.250   0.9291   0.00972   0.00431  -0.0377   0.2647   0.9729
   6.500   0.9522   0.01006   0.00460  -0.0370   0.2498   0.9803
   6.750   0.9768   0.01038   0.00486  -0.0367   0.2379   0.9847
   7.000   1.0064   0.01070   0.00514  -0.0376   0.2264   0.9876
   7.250   1.0340   0.01105   0.00543  -0.0380   0.2147   0.9908
   7.500   1.0597   0.01139   0.00573  -0.0380   0.2038   0.9936
   7.750   1.0899   0.01172   0.00602  -0.0391   0.1924   0.9953
   8.000   1.1187   0.01208   0.00633  -0.0399   0.1812   0.9973
   8.250   1.1462   0.01247   0.00666  -0.0405   0.1692   0.9992
   8.500   1.1640   0.01278   0.00694  -0.0390   0.1602   1.0000
   8.750   1.1687   0.01308   0.00722  -0.0347   0.1528   1.0000
   9.000   1.1757   0.01342   0.00754  -0.0309   0.1458   1.0000
   9.250   1.1843   0.01378   0.00789  -0.0276   0.1392   1.0000
   9.500   1.1929   0.01420   0.00829  -0.0245   0.1322   1.0000
   9.750   1.2030   0.01462   0.00871  -0.0217   0.1271   1.0000
  10.000   1.2138   0.01507   0.00916  -0.0191   0.1218   1.0000
  10.250   1.2218   0.01566   0.00973  -0.0162   0.1151   1.0000
  10.500   1.2332   0.01618   0.01026  -0.0140   0.1104   1.0000
  10.750   1.2423   0.01684   0.01091  -0.0116   0.1049   1.0000
  11.000   1.2532   0.01748   0.01157  -0.0096   0.1008   1.0000
  11.250   1.2641   0.01817   0.01227  -0.0077   0.0963   1.0000
  11.500   1.2729   0.01903   0.01312  -0.0056   0.0913   1.0000
  11.750   1.2838   0.01982   0.01393  -0.0040   0.0872   1.0000
  12.000   1.2928   0.02078   0.01489  -0.0023   0.0824   1.0000
  12.250   1.3022   0.02175   0.01587  -0.0007   0.0784   1.0000
  12.500   1.3129   0.02269   0.01684   0.0007   0.0754   1.0000
  12.750   1.3215   0.02379   0.01795   0.0021   0.0719   1.0000
  13.000   1.3296   0.02497   0.01914   0.0035   0.0680   1.0000
  13.250   1.3398   0.02603   0.02025   0.0046   0.0661   1.0000
  13.500   1.3481   0.02726   0.02150   0.0058   0.0630   1.0000
  13.750   1.3547   0.02864   0.02289   0.0070   0.0600   1.0000
  14.000   1.3634   0.02989   0.02418   0.0080   0.0580   1.0000
  14.250   1.3702   0.03131   0.02562   0.0091   0.0549   1.0000
  14.500   1.3750   0.03293   0.02725   0.0101   0.0518   1.0000
  14.750   1.3811   0.03447   0.02883   0.0110   0.0493   1.0000
  15.000   1.3871   0.03607   0.03047   0.0119   0.0471   1.0000
  15.250   1.3884   0.03810   0.03250   0.0128   0.0432   1.0000
  15.500   1.3947   0.03976   0.03421   0.0134   0.0424   1.0000
  15.750   1.3955   0.04195   0.03640   0.0142   0.0380   1.0000
  16.000   1.4001   0.04385   0.03836   0.0147   0.0372   1.0000
  16.250   1.4024   0.04601   0.04054   0.0152   0.0348   1.0000
  16.500   1.4059   0.04809   0.04268   0.0155   0.0333   1.0000
  16.750   1.4099   0.05018   0.04483   0.0158   0.0328   1.0000
  17.000   1.4095   0.05275   0.04743   0.0160   0.0310   1.0000
  17.250   1.4111   0.05515   0.04989   0.0162   0.0300   1.0000
  17.500   1.4123   0.05763   0.05242   0.0163   0.0284   1.0000
  17.750   1.4132   0.06020   0.05506   0.0162   0.0277   1.0000
  18.000   1.4110   0.06318   0.05808   0.0161   0.0262   1.0000
  18.250   1.4089   0.06616   0.06112   0.0159   0.0252   1.0000
  18.500   1.4082   0.06901   0.06404   0.0156   0.0240   1.0000
  18.750   1.4085   0.07184   0.06695   0.0153   0.0244   1.0000
  19.000   1.4053   0.07511   0.07028   0.0148   0.0233   1.0000
  19.250   1.3987   0.07885   0.07407   0.0141   0.0216   1.0000
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