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S4110 (s4110-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: S4110 (s4110-il)
Reynolds number: 1,000,000
Max Cl/Cd: 99.93 at α=4.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-s4110-il-1000000-n5.txt
Download as CSV file: xf-s4110-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: S4110                                           
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -11.250  -0.4470   0.11277   0.11099  -0.0227   1.0000   0.0058
 -11.000  -0.4464   0.10858   0.10681  -0.0241   1.0000   0.0057
 -10.000  -0.6887   0.02960   0.02713  -0.0799   0.9935   0.0057
  -9.750  -0.6676   0.02587   0.02305  -0.0832   0.9897   0.0057
  -9.500  -0.6419   0.02323   0.02010  -0.0856   0.9868   0.0058
  -9.250  -0.6139   0.02111   0.01772  -0.0878   0.9848   0.0058
  -9.000  -0.5840   0.01948   0.01587  -0.0896   0.9834   0.0059
  -8.750  -0.5595   0.01822   0.01442  -0.0899   0.9785   0.0059
  -8.500  -0.5323   0.01672   0.01270  -0.0909   0.9745   0.0060
  -8.250  -0.5040   0.01490   0.01061  -0.0921   0.9712   0.0063
  -8.000  -0.4776   0.01400   0.00957  -0.0923   0.9656   0.0065
  -7.750  -0.4491   0.01321   0.00866  -0.0928   0.9603   0.0066
  -7.500  -0.4199   0.01255   0.00789  -0.0934   0.9553   0.0068
  -7.250  -0.3923   0.01197   0.00722  -0.0935   0.9479   0.0069
  -7.000  -0.3638   0.01146   0.00663  -0.0938   0.9411   0.0072
  -6.750  -0.3365   0.01099   0.00606  -0.0937   0.9325   0.0074
  -6.500  -0.3091   0.01056   0.00554  -0.0937   0.9241   0.0077
  -6.250  -0.2820   0.01017   0.00505  -0.0935   0.9150   0.0079
  -6.000  -0.2550   0.00982   0.00462  -0.0933   0.9058   0.0082
  -5.750  -0.2280   0.00952   0.00424  -0.0931   0.8970   0.0085
  -5.500  -0.2009   0.00924   0.00387  -0.0929   0.8876   0.0086
  -5.250  -0.1737   0.00899   0.00355  -0.0927   0.8788   0.0088
  -5.000  -0.1466   0.00871   0.00318  -0.0924   0.8700   0.0091
  -4.750  -0.1193   0.00841   0.00282  -0.0922   0.8611   0.0097
  -4.500  -0.0919   0.00820   0.00254  -0.0920   0.8529   0.0103
  -4.250  -0.0645   0.00801   0.00231  -0.0919   0.8440   0.0113
  -4.000  -0.0369   0.00785   0.00209  -0.0917   0.8356   0.0123
  -3.750  -0.0094   0.00766   0.00188  -0.0915   0.8268   0.0155
  -3.500   0.0181   0.00744   0.00169  -0.0914   0.8176   0.0262
  -3.250   0.0456   0.00730   0.00156  -0.0912   0.8085   0.0355
  -3.000   0.0732   0.00721   0.00144  -0.0911   0.7987   0.0413
  -2.750   0.1010   0.00711   0.00134  -0.0910   0.7888   0.0483
  -2.500   0.1286   0.00703   0.00124  -0.0908   0.7786   0.0559
  -2.250   0.1561   0.00695   0.00115  -0.0906   0.7671   0.0658
  -1.750   0.2112   0.00680   0.00100  -0.0903   0.7419   0.0937
  -1.500   0.2388   0.00673   0.00094  -0.0902   0.7292   0.1087
  -1.250   0.2663   0.00668   0.00089  -0.0900   0.7153   0.1278
  -1.000   0.2936   0.00661   0.00085  -0.0898   0.6991   0.1559
  -0.750   0.3207   0.00657   0.00082  -0.0896   0.6819   0.1869
  -0.500   0.3480   0.00651   0.00080  -0.0895   0.6650   0.2224
  -0.250   0.3751   0.00642   0.00080  -0.0893   0.6467   0.2747
   0.000   0.4021   0.00635   0.00081  -0.0892   0.6267   0.3340
   0.250   0.4288   0.00628   0.00083  -0.0890   0.6044   0.3986
   0.500   0.4555   0.00628   0.00087  -0.0888   0.5805   0.4521
   0.750   0.4820   0.00623   0.00093  -0.0885   0.5548   0.5247
   1.000   0.5083   0.00624   0.00101  -0.0882   0.5270   0.5917
   1.250   0.5342   0.00626   0.00110  -0.0879   0.4960   0.6607
   1.500   0.5594   0.00629   0.00121  -0.0873   0.4629   0.7401
   1.750   0.5827   0.00626   0.00134  -0.0863   0.4301   0.8392
   2.000   0.6035   0.00621   0.00143  -0.0844   0.4012   0.9532
   2.250   0.6356   0.00641   0.00151  -0.0854   0.3728   1.0000
   2.500   0.6616   0.00667   0.00163  -0.0851   0.3419   1.0000
   2.750   0.6878   0.00692   0.00175  -0.0847   0.3152   1.0000
   3.000   0.7141   0.00716   0.00188  -0.0844   0.2915   1.0000
   3.250   0.7401   0.00743   0.00202  -0.0841   0.2643   1.0000
   3.500   0.7662   0.00768   0.00217  -0.0838   0.2428   1.0000
   3.750   0.7924   0.00793   0.00233  -0.0835   0.2223   1.0000
   4.000   0.8183   0.00820   0.00250  -0.0831   0.2010   1.0000
   4.250   0.8444   0.00845   0.00267  -0.0828   0.1842   1.0000
   4.500   0.8701   0.00873   0.00286  -0.0825   0.1657   1.0000
   4.750   0.8957   0.00902   0.00306  -0.0821   0.1481   1.0000
   5.000   0.9215   0.00929   0.00327  -0.0817   0.1337   1.0000
   5.250   0.9471   0.00957   0.00348  -0.0814   0.1209   1.0000
   5.750   0.9986   0.01009   0.00393  -0.0807   0.1014   1.0000
   6.000   1.0240   0.01037   0.00417  -0.0803   0.0922   1.0000
   6.250   1.0492   0.01067   0.00443  -0.0798   0.0834   1.0000
   6.500   1.0747   0.01094   0.00469  -0.0794   0.0765   1.0000
   6.750   1.0995   0.01126   0.00497  -0.0790   0.0685   1.0000
   7.000   1.1244   0.01157   0.00526  -0.0785   0.0618   1.0000
   7.250   1.1492   0.01188   0.00556  -0.0780   0.0558   1.0000
   7.500   1.1730   0.01229   0.00592  -0.0774   0.0472   1.0000
   7.750   1.1969   0.01268   0.00628  -0.0768   0.0405   1.0000
   8.000   1.2209   0.01305   0.00664  -0.0763   0.0356   1.0000
   8.250   1.2446   0.01343   0.00702  -0.0756   0.0319   1.0000
   8.500   1.2680   0.01383   0.00742  -0.0750   0.0284   1.0000
   8.750   1.2915   0.01421   0.00782  -0.0743   0.0258   1.0000
   9.000   1.3140   0.01468   0.00828  -0.0736   0.0224   1.0000
   9.250   1.3369   0.01508   0.00871  -0.0729   0.0205   1.0000
   9.500   1.3594   0.01552   0.00916  -0.0721   0.0186   1.0000
   9.750   1.3809   0.01603   0.00968  -0.0712   0.0162   1.0000
  10.000   1.4027   0.01648   0.01018  -0.0703   0.0149   1.0000
  10.250   1.4238   0.01699   0.01071  -0.0694   0.0134   1.0000
  10.500   1.4438   0.01757   0.01130  -0.0683   0.0117   1.0000
  10.750   1.4641   0.01809   0.01187  -0.0672   0.0107   1.0000
  11.000   1.4834   0.01866   0.01248  -0.0661   0.0096   1.0000
  11.250   1.5015   0.01931   0.01315  -0.0647   0.0086   1.0000
  11.500   1.5191   0.01995   0.01385  -0.0633   0.0079   1.0000
  11.750   1.5363   0.02056   0.01453  -0.0619   0.0074   1.0000
  12.000   1.5509   0.02120   0.01522  -0.0600   0.0069   1.0000
  12.250   1.5631   0.02191   0.01598  -0.0577   0.0064   1.0000
  12.500   1.5741   0.02270   0.01683  -0.0553   0.0060   1.0000
  12.750   1.5837   0.02360   0.01780  -0.0529   0.0056   1.0000
  13.000   1.5947   0.02441   0.01868  -0.0508   0.0055   1.0000
  13.250   1.6047   0.02531   0.01967  -0.0487   0.0053   1.0000
  13.500   1.6138   0.02629   0.02074  -0.0466   0.0052   1.0000
  13.750   1.6220   0.02738   0.02193  -0.0446   0.0050   1.0000
  14.000   1.6291   0.02860   0.02324  -0.0426   0.0048   1.0000
  14.250   1.6354   0.02993   0.02465  -0.0408   0.0046   1.0000
  14.500   1.6402   0.03144   0.02625  -0.0390   0.0045   1.0000
  14.750   1.6442   0.03309   0.02799  -0.0374   0.0043   1.0000
  15.000   1.6465   0.03498   0.02998  -0.0360   0.0042   1.0000
  15.250   1.6476   0.03708   0.03218  -0.0347   0.0041   1.0000
  15.500   1.6467   0.03949   0.03470  -0.0337   0.0039   1.0000
  15.750   1.6434   0.04230   0.03764  -0.0329   0.0038   1.0000
  16.000   1.6372   0.04562   0.04109  -0.0325   0.0037   1.0000
  16.250   1.6330   0.04890   0.04449  -0.0325   0.0036   1.0000
  16.500   1.6287   0.05239   0.04810  -0.0329   0.0036   1.0000
  16.750   1.6219   0.05643   0.05227  -0.0337   0.0036   1.0000
  17.000   1.6138   0.06090   0.05688  -0.0350   0.0035   1.0000
  17.250   1.6025   0.06617   0.06229  -0.0369   0.0035   1.0000
  17.500   1.5869   0.07249   0.06878  -0.0397   0.0035   1.0000
  17.750   1.5702   0.07940   0.07585  -0.0430   0.0035   1.0000
  18.000   1.5503   0.08730   0.08390  -0.0471   0.0035   1.0000
  18.250   1.5240   0.09687   0.09364  -0.0524   0.0035   1.0000
  18.500   1.4949   0.10737   0.10433  -0.0584   0.0035   1.0000
  18.750   1.4599   0.11956   0.11670  -0.0655   0.0035   1.0000
  19.000   1.4224   0.13265   0.12998  -0.0733   0.0036   1.0000
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