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E222 (10.17%) (e222-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: E222 (10.17%) (e222-il)
Reynolds number: 1,000,000
Max Cl/Cd: 99.89 at α=4°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-e222-il-1000000-n5.txt
Download as CSV file: xf-e222-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: E222  (10.17%)                                  
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -11.750  -0.6757   0.06607   0.06422  -0.0478   1.0000   0.0066
 -11.500  -0.7267   0.05077   0.04874  -0.0588   1.0000   0.0065
 -11.250  -0.7558   0.04225   0.04006  -0.0662   1.0000   0.0065
 -11.000  -0.7947   0.03811   0.03580  -0.0656   1.0000   0.0064
 -10.750  -0.7864   0.03384   0.03125  -0.0703   0.9975   0.0065
 -10.500  -0.7684   0.03053   0.02766  -0.0739   0.9950   0.0065
 -10.250  -0.7492   0.02796   0.02483  -0.0760   0.9926   0.0066
 -10.000  -0.7276   0.02600   0.02265  -0.0773   0.9899   0.0066
  -9.750  -0.7033   0.02419   0.02063  -0.0788   0.9876   0.0067
  -9.500  -0.6770   0.02258   0.01882  -0.0803   0.9859   0.0067
  -9.250  -0.6484   0.02133   0.01741  -0.0818   0.9845   0.0068
  -9.000  -0.6262   0.01855   0.01431  -0.0829   0.9822   0.0069
  -8.750  -0.6040   0.01713   0.01272  -0.0828   0.9780   0.0071
  -8.500  -0.5760   0.01615   0.01165  -0.0837   0.9754   0.0074
  -8.250  -0.5459   0.01543   0.01084  -0.0848   0.9734   0.0075
  -8.000  -0.5150   0.01461   0.00994  -0.0860   0.9718   0.0077
  -7.750  -0.4869   0.01391   0.00916  -0.0865   0.9690   0.0078
  -7.500  -0.4614   0.01327   0.00845  -0.0863   0.9639   0.0080
  -7.250  -0.4313   0.01264   0.00774  -0.0872   0.9607   0.0083
  -7.000  -0.3994   0.01203   0.00704  -0.0883   0.9581   0.0085
  -6.750  -0.3716   0.01153   0.00649  -0.0885   0.9525   0.0088
  -6.500  -0.3408   0.01101   0.00591  -0.0894   0.9476   0.0091
  -6.250  -0.3085   0.01056   0.00539  -0.0905   0.9428   0.0094
  -6.000  -0.2786   0.01014   0.00490  -0.0911   0.9354   0.0096
  -5.750  -0.2474   0.00976   0.00445  -0.0919   0.9282   0.0098
  -5.500  -0.2180   0.00943   0.00406  -0.0923   0.9186   0.0099
  -5.250  -0.1892   0.00915   0.00371  -0.0926   0.9085   0.0101
  -5.000  -0.1609   0.00890   0.00339  -0.0927   0.8977   0.0102
  -4.750  -0.1334   0.00858   0.00298  -0.0927   0.8862   0.0105
  -4.500  -0.1062   0.00829   0.00259  -0.0925   0.8739   0.0114
  -4.250  -0.0790   0.00809   0.00233  -0.0924   0.8616   0.0120
  -4.000  -0.0517   0.00794   0.00211  -0.0922   0.8489   0.0126
  -3.750  -0.0246   0.00781   0.00192  -0.0920   0.8359   0.0134
  -3.500   0.0026   0.00772   0.00175  -0.0918   0.8223   0.0142
  -3.250   0.0297   0.00764   0.00160  -0.0916   0.8087   0.0151
  -3.000   0.0567   0.00754   0.00147  -0.0914   0.7946   0.0198
  -2.750   0.0834   0.00730   0.00130  -0.0912   0.7804   0.0545
  -2.500   0.1100   0.00708   0.00118  -0.0911   0.7659   0.0956
  -2.250   0.1366   0.00683   0.00107  -0.0909   0.7512   0.1507
  -2.000   0.1635   0.00669   0.00100  -0.0908   0.7361   0.1904
  -1.750   0.1903   0.00654   0.00094  -0.0907   0.7208   0.2367
  -1.500   0.2170   0.00636   0.00089  -0.0906   0.7049   0.2963
  -1.250   0.2439   0.00628   0.00087  -0.0904   0.6888   0.3360
  -1.000   0.2707   0.00617   0.00085  -0.0903   0.6726   0.3907
  -0.750   0.2977   0.00612   0.00085  -0.0902   0.6562   0.4284
  -0.500   0.3249   0.00610   0.00086  -0.0900   0.6396   0.4587
  -0.250   0.3520   0.00610   0.00087  -0.0899   0.6225   0.4875
   0.000   0.3790   0.00612   0.00089  -0.0897   0.6043   0.5154
   0.250   0.4059   0.00616   0.00093  -0.0895   0.5857   0.5423
   0.500   0.4329   0.00619   0.00097  -0.0893   0.5673   0.5697
   0.750   0.4599   0.00623   0.00102  -0.0892   0.5485   0.5979
   1.000   0.4867   0.00629   0.00108  -0.0890   0.5297   0.6243
   1.250   0.5136   0.00636   0.00115  -0.0888   0.5109   0.6494
   1.500   0.5404   0.00644   0.00122  -0.0886   0.4909   0.6735
   2.000   0.5934   0.00665   0.00140  -0.0880   0.4484   0.7218
   2.250   0.6196   0.00677   0.00152  -0.0877   0.4267   0.7466
   2.750   0.6715   0.00705   0.00176  -0.0869   0.3818   0.7933
   3.000   0.6973   0.00720   0.00189  -0.0865   0.3592   0.8149
   3.250   0.7224   0.00739   0.00204  -0.0860   0.3344   0.8362
   3.500   0.7474   0.00758   0.00220  -0.0854   0.3115   0.8577
   3.750   0.7718   0.00775   0.00235  -0.0847   0.2908   0.8797
   4.000   0.7951   0.00796   0.00253  -0.0837   0.2667   0.9028
   4.250   0.8163   0.00826   0.00273  -0.0824   0.2321   0.9280
   4.500   0.8374   0.00862   0.00295  -0.0810   0.1913   0.9619
   4.750   0.8651   0.00903   0.00319  -0.0813   0.1572   1.0000
   5.000   0.8905   0.00934   0.00342  -0.0809   0.1376   1.0000
   5.250   0.9147   0.00976   0.00371  -0.0804   0.1110   1.0000
   5.500   0.9386   0.01022   0.00402  -0.0798   0.0847   1.0000
   5.750   0.9624   0.01067   0.00435  -0.0792   0.0630   1.0000
   6.000   0.9865   0.01109   0.00467  -0.0787   0.0460   1.0000
   6.250   1.0101   0.01154   0.00503  -0.0781   0.0315   1.0000
   6.500   1.0329   0.01207   0.00548  -0.0773   0.0157   1.0000
   6.750   1.0558   0.01259   0.00594  -0.0765   0.0076   1.0000
   7.000   1.0799   0.01297   0.00633  -0.0759   0.0061   1.0000
   7.250   1.1042   0.01331   0.00671  -0.0754   0.0056   1.0000
   7.500   1.1282   0.01367   0.00710  -0.0748   0.0052   1.0000
   7.750   1.1516   0.01407   0.00754  -0.0741   0.0049   1.0000
   8.000   1.1747   0.01449   0.00800  -0.0734   0.0046   1.0000
   8.250   1.1972   0.01495   0.00849  -0.0726   0.0044   1.0000
   8.500   1.2189   0.01547   0.00906  -0.0716   0.0041   1.0000
   8.750   1.2397   0.01606   0.00970  -0.0705   0.0039   1.0000
   9.000   1.2589   0.01678   0.01051  -0.0692   0.0037   1.0000
   9.250   1.2791   0.01735   0.01115  -0.0681   0.0036   1.0000
   9.500   1.2990   0.01792   0.01176  -0.0669   0.0036   1.0000
   9.750   1.3182   0.01851   0.01242  -0.0656   0.0035   1.0000
  10.000   1.3364   0.01914   0.01311  -0.0642   0.0034   1.0000
  10.250   1.3533   0.01983   0.01387  -0.0626   0.0033   1.0000
  10.500   1.3679   0.02054   0.01465  -0.0606   0.0032   1.0000
  10.750   1.3802   0.02128   0.01547  -0.0583   0.0032   1.0000
  11.000   1.3915   0.02208   0.01636  -0.0558   0.0031   1.0000
  11.250   1.4018   0.02295   0.01731  -0.0533   0.0030   1.0000
  11.500   1.4110   0.02389   0.01834  -0.0508   0.0029   1.0000
  11.750   1.4205   0.02483   0.01936  -0.0485   0.0028   1.0000
  12.000   1.4286   0.02588   0.02050  -0.0462   0.0028   1.0000
  12.250   1.4362   0.02701   0.02170  -0.0439   0.0027   1.0000
  12.500   1.4429   0.02823   0.02302  -0.0418   0.0026   1.0000
  12.750   1.4486   0.02958   0.02446  -0.0397   0.0026   1.0000
  13.000   1.4533   0.03108   0.02604  -0.0378   0.0025   1.0000
  13.250   1.4566   0.03277   0.02783  -0.0361   0.0025   1.0000
  13.500   1.4581   0.03471   0.02989  -0.0345   0.0025   1.0000
  13.750   1.4582   0.03689   0.03218  -0.0331   0.0024   1.0000
  14.000   1.4582   0.03924   0.03464  -0.0321   0.0024   1.0000
  14.250   1.4567   0.04188   0.03739  -0.0313   0.0024   1.0000
  14.500   1.4530   0.04494   0.04057  -0.0309   0.0023   1.0000
  14.750   1.4481   0.04836   0.04412  -0.0310   0.0023   1.0000
  15.000   1.4414   0.05221   0.04810  -0.0314   0.0023   1.0000
  15.250   1.4342   0.05641   0.05242  -0.0324   0.0023   1.0000
  15.500   1.4251   0.06113   0.05728  -0.0338   0.0023   1.0000
  15.750   1.4140   0.06647   0.06277  -0.0358   0.0023   1.0000
  16.000   1.4007   0.07250   0.06894  -0.0384   0.0023   1.0000
  16.250   1.3867   0.07896   0.07554  -0.0414   0.0023   1.0000
  16.500   1.3725   0.08580   0.08252  -0.0449   0.0023   1.0000
  16.750   1.3565   0.09327   0.09014  -0.0488   0.0023   1.0000
  17.000   1.3389   0.10132   0.09833  -0.0532   0.0023   1.0000
  17.250   1.3227   0.10939   0.10654  -0.0576   0.0023   1.0000
  17.500   1.3037   0.11824   0.11553  -0.0627   0.0023   1.0000
  17.750   1.2869   0.12681   0.12422  -0.0676   0.0023   1.0000
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