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E10(08%) (e228-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: E10(08%) (e228-il)
Reynolds number: 500,000
Max Cl/Cd: 61.22 at α=5.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-e228-il-500000-n5.txt
Download as CSV file: xf-e228-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: E10(08%)                                        
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.500  -0.9001   0.10192   0.09948   0.0111   1.0000   0.0044
 -14.250  -0.9400   0.08840   0.08583   0.0032   1.0000   0.0043
 -14.000  -0.9699   0.07741   0.07471  -0.0036   1.0000   0.0042
 -13.750  -0.9998   0.06683   0.06395  -0.0107   1.0000   0.0041
 -13.500  -1.0203   0.05864   0.05557  -0.0165   1.0000   0.0042
 -13.250  -1.0401   0.05154   0.04828  -0.0213   1.0000   0.0042
 -13.000  -1.0573   0.04587   0.04241  -0.0245   1.0000   0.0042
 -12.750  -1.0611   0.04265   0.03904  -0.0256   1.0000   0.0042
 -12.500  -1.0745   0.03888   0.03507  -0.0258   1.0000   0.0042
 -12.250  -1.0789   0.03645   0.03246  -0.0249   1.0000   0.0043
 -12.000  -1.0852   0.03410   0.02992  -0.0230   1.0000   0.0044
 -11.750  -1.0878   0.03220   0.02783  -0.0205   1.0000   0.0044
 -11.500  -1.0890   0.03043   0.02589  -0.0175   1.0000   0.0045
 -11.250  -1.0901   0.02820   0.02343  -0.0146   1.0000   0.0047
 -11.000  -1.0823   0.02651   0.02157  -0.0126   1.0000   0.0049
 -10.750  -1.0698   0.02516   0.02004  -0.0111   1.0000   0.0050
 -10.500  -1.0533   0.02416   0.01893  -0.0099   1.0000   0.0053
 -10.250  -1.0352   0.02327   0.01794  -0.0088   1.0000   0.0055
 -10.000  -1.0173   0.02227   0.01682  -0.0077   1.0000   0.0058
  -9.750  -0.9979   0.02142   0.01586  -0.0068   1.0000   0.0062
  -9.500  -0.9783   0.02052   0.01485  -0.0058   1.0000   0.0066
  -9.250  -0.9582   0.01966   0.01386  -0.0048   1.0000   0.0071
  -9.000  -0.9374   0.01886   0.01294  -0.0039   1.0000   0.0074
  -8.750  -0.9153   0.01821   0.01220  -0.0032   1.0000   0.0077
  -8.500  -0.8958   0.01722   0.01112  -0.0021   1.0000   0.0087
  -8.250  -0.8726   0.01672   0.01058  -0.0016   1.0000   0.0095
  -8.000  -0.8492   0.01621   0.01002  -0.0010   1.0000   0.0105
  -7.750  -0.8261   0.01567   0.00940  -0.0003   1.0000   0.0113
  -7.500  -0.8027   0.01516   0.00881   0.0004   1.0000   0.0120
  -7.250  -0.7791   0.01469   0.00827   0.0010   1.0000   0.0124
  -7.000  -0.7581   0.01389   0.00737   0.0021   1.0000   0.0137
  -6.750  -0.7351   0.01340   0.00687   0.0028   1.0000   0.0151
  -6.500  -0.7120   0.01300   0.00642   0.0036   1.0000   0.0163
  -6.250  -0.6812   0.01258   0.00594   0.0027   0.9901   0.0176
  -6.000  -0.6486   0.01214   0.00543   0.0015   0.9802   0.0191
  -5.750  -0.6168   0.01169   0.00494   0.0005   0.9700   0.0218
  -5.500  -0.5866   0.01134   0.00454  -0.0001   0.9587   0.0247
  -5.250  -0.5589   0.01097   0.00418  -0.0001   0.9465   0.0334
  -5.000  -0.5335   0.01059   0.00385   0.0004   0.9338   0.0509
  -4.750  -0.5093   0.01022   0.00356   0.0011   0.9211   0.0734
  -4.500  -0.4854   0.00987   0.00329   0.0019   0.9084   0.1002
  -4.250  -0.4614   0.00954   0.00305   0.0026   0.8960   0.1281
  -4.000  -0.4367   0.00928   0.00282   0.0033   0.8837   0.1526
  -3.750  -0.4123   0.00897   0.00260   0.0040   0.8713   0.1863
  -3.500  -0.3873   0.00871   0.00242   0.0045   0.8585   0.2183
  -3.250  -0.3620   0.00845   0.00225   0.0051   0.8457   0.2523
  -3.000  -0.3370   0.00817   0.00208   0.0056   0.8327   0.2946
  -2.750  -0.3120   0.00789   0.00192   0.0061   0.8194   0.3411
  -2.500  -0.2863   0.00769   0.00180   0.0066   0.8058   0.3770
  -2.250  -0.2603   0.00752   0.00168   0.0070   0.7918   0.4082
  -2.000  -0.2342   0.00737   0.00158   0.0074   0.7776   0.4388
  -1.750  -0.2081   0.00723   0.00148   0.0078   0.7631   0.4702
  -1.500  -0.1819   0.00710   0.00140   0.0082   0.7482   0.5019
  -1.250  -0.1557   0.00698   0.00133   0.0086   0.7332   0.5337
  -1.000  -0.1296   0.00687   0.00127   0.0091   0.7176   0.5660
  -0.750  -0.1035   0.00677   0.00122   0.0095   0.7016   0.5990
  -0.500  -0.0774   0.00668   0.00119   0.0099   0.6848   0.6315
  -0.250  -0.0514   0.00659   0.00116   0.0104   0.6675   0.6641
   0.000  -0.0254   0.00653   0.00115   0.0109   0.6495   0.6956
   0.250   0.0006   0.00649   0.00115   0.0114   0.6315   0.7264
   0.500   0.0267   0.00645   0.00116   0.0119   0.6126   0.7556
   0.750   0.0528   0.00643   0.00118   0.0124   0.5931   0.7838
   1.000   0.0790   0.00644   0.00121   0.0129   0.5736   0.8109
   1.250   0.1055   0.00646   0.00125   0.0134   0.5529   0.8366
   1.500   0.1323   0.00650   0.00132   0.0138   0.5320   0.8613
   1.750   0.1601   0.00658   0.00138   0.0139   0.5100   0.8849
   2.000   0.1900   0.00668   0.00147   0.0136   0.4871   0.9055
   2.250   0.2221   0.00684   0.00158   0.0128   0.4615   0.9228
   2.500   0.2558   0.00703   0.00170   0.0116   0.4338   0.9361
   2.750   0.2896   0.00723   0.00181   0.0103   0.4054   0.9465
   3.000   0.3215   0.00745   0.00194   0.0094   0.3773   0.9561
   3.250   0.3553   0.00769   0.00209   0.0080   0.3466   0.9629
   3.500   0.3862   0.00793   0.00224   0.0073   0.3187   0.9704
   3.750   0.4203   0.00819   0.00240   0.0058   0.2875   0.9753
   4.000   0.4507   0.00848   0.00258   0.0051   0.2573   0.9816
   4.250   0.4851   0.00879   0.00279   0.0035   0.2258   0.9850
   4.500   0.5185   0.00912   0.00300   0.0020   0.1923   0.9886
   4.750   0.5507   0.00948   0.00324   0.0008   0.1608   0.9924
   5.000   0.5837   0.00985   0.00349  -0.0006   0.1321   0.9953
   5.250   0.6174   0.01022   0.00376  -0.0022   0.1074   0.9981
   5.500   0.6483   0.01059   0.00408  -0.0031   0.0873   1.0000
   5.750   0.6706   0.01096   0.00438  -0.0022   0.0698   1.0000
   6.000   0.6925   0.01138   0.00471  -0.0013   0.0532   1.0000
   6.250   0.7147   0.01176   0.00505  -0.0004   0.0422   1.0000
   6.500   0.7371   0.01212   0.00540   0.0005   0.0342   1.0000
   6.750   0.7592   0.01252   0.00578   0.0014   0.0271   1.0000
   7.000   0.7808   0.01298   0.00623   0.0024   0.0201   1.0000
   7.250   0.8024   0.01343   0.00668   0.0034   0.0151   1.0000
   7.500   0.8240   0.01390   0.00717   0.0044   0.0115   1.0000
   7.750   0.8449   0.01446   0.00775   0.0055   0.0090   1.0000
   8.000   0.8661   0.01497   0.00833   0.0066   0.0080   1.0000
   8.250   0.8868   0.01552   0.00895   0.0077   0.0072   1.0000
   8.500   0.9069   0.01615   0.00966   0.0089   0.0066   1.0000
   8.750   0.9252   0.01697   0.01058   0.0103   0.0059   1.0000
   9.000   0.9427   0.01785   0.01157   0.0118   0.0055   1.0000
   9.250   0.9618   0.01850   0.01231   0.0131   0.0053   1.0000
   9.500   0.9804   0.01920   0.01310   0.0143   0.0050   1.0000
   9.750   0.9983   0.01995   0.01394   0.0156   0.0047   1.0000
  10.000   1.0142   0.02088   0.01499   0.0171   0.0046   1.0000
  10.250   1.0295   0.02184   0.01606   0.0187   0.0044   1.0000
  10.500   1.0441   0.02280   0.01713   0.0202   0.0042   1.0000
  10.750   1.0570   0.02387   0.01835   0.0220   0.0041   1.0000
  11.000   1.0686   0.02497   0.01957   0.0237   0.0040   1.0000
  11.250   1.0776   0.02618   0.02091   0.0257   0.0039   1.0000
  11.500   1.0808   0.02745   0.02230   0.0286   0.0038   1.0000
  11.750   1.0836   0.02872   0.02369   0.0310   0.0037   1.0000
  12.000   1.0839   0.03036   0.02547   0.0332   0.0037   1.0000
  12.250   1.0828   0.03228   0.02751   0.0347   0.0035   1.0000
  12.500   1.0816   0.03444   0.02982   0.0356   0.0035   1.0000
  12.750   1.0778   0.03710   0.03263   0.0360   0.0034   1.0000
  13.000   1.0680   0.04073   0.03644   0.0355   0.0033   1.0000
  13.250   1.0559   0.04511   0.04100   0.0341   0.0033   1.0000
  13.500   1.0571   0.04809   0.04411   0.0329   0.0035   1.0000
  13.750   1.0351   0.05472   0.05094   0.0293   0.0033   1.0000
  14.000   1.0282   0.05950   0.05586   0.0265   0.0033   1.0000
  14.250   1.0063   0.06711   0.06365   0.0220   0.0032   1.0000
  14.500   0.9942   0.07334   0.07001   0.0182   0.0033   1.0000
  14.750   0.9836   0.07950   0.07629   0.0147   0.0034   1.0000
  15.000   0.9654   0.08729   0.08421   0.0102   0.0034   1.0000
  15.250   0.9427   0.09633   0.09339   0.0052   0.0034   1.0000
  15.500   0.9228   0.10508   0.10227   0.0005   0.0035   1.0000
  15.750   0.8974   0.11545   0.11274  -0.0050   0.0035   1.0000
  16.000   0.8696   0.12689   0.12430  -0.0108   0.0035   1.0000
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