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E226 (10.19%) (e226-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: E226 (10.19%) (e226-il)
Reynolds number: 500,000
Max Cl/Cd: 67.25 at α=4.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-e226-il-500000-n5.txt
Download as CSV file: xf-e226-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: E226  (10.19%)                                  
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -12.250  -0.7644   0.07335   0.07082  -0.0235   1.0000   0.0073
 -12.000  -0.8324   0.05407   0.05108  -0.0390   1.0000   0.0068
 -11.750  -0.8435   0.04894   0.04581  -0.0431   1.0000   0.0069
 -11.500  -0.8627   0.04380   0.04047  -0.0459   1.0000   0.0069
 -11.250  -0.8700   0.04106   0.03759  -0.0462   1.0000   0.0070
 -11.000  -0.8824   0.03829   0.03464  -0.0447   1.0000   0.0070
 -10.750  -0.8912   0.03595   0.03210  -0.0419   1.0000   0.0070
 -10.500  -0.8893   0.03386   0.02981  -0.0402   1.0000   0.0071
 -10.250  -0.8848   0.03166   0.02738  -0.0385   1.0000   0.0071
 -10.000  -0.8770   0.02959   0.02507  -0.0369   1.0000   0.0072
  -9.750  -0.8664   0.02766   0.02291  -0.0353   1.0000   0.0072
  -9.500  -0.8531   0.02601   0.02105  -0.0338   1.0000   0.0073
  -9.250  -0.8383   0.02447   0.01932  -0.0324   1.0000   0.0073
  -9.000  -0.8221   0.02313   0.01780  -0.0310   1.0000   0.0075
  -8.750  -0.8052   0.02190   0.01641  -0.0296   1.0000   0.0077
  -8.500  -0.7880   0.02077   0.01514  -0.0282   1.0000   0.0078
  -8.250  -0.7706   0.01973   0.01397  -0.0266   1.0000   0.0079
  -8.000  -0.7530   0.01881   0.01294  -0.0251   1.0000   0.0081
  -7.750  -0.7354   0.01797   0.01198  -0.0234   1.0000   0.0083
  -7.500  -0.7136   0.01714   0.01106  -0.0227   0.9988   0.0084
  -7.250  -0.6824   0.01630   0.01012  -0.0238   0.9947   0.0087
  -7.000  -0.6522   0.01553   0.00927  -0.0247   0.9901   0.0089
  -6.750  -0.6203   0.01485   0.00851  -0.0259   0.9863   0.0090
  -6.500  -0.5907   0.01395   0.00753  -0.0268   0.9811   0.0093
  -6.250  -0.5607   0.01318   0.00671  -0.0276   0.9751   0.0100
  -6.000  -0.5299   0.01264   0.00612  -0.0285   0.9693   0.0105
  -5.750  -0.4997   0.01216   0.00558  -0.0292   0.9621   0.0110
  -5.500  -0.4692   0.01172   0.00507  -0.0299   0.9549   0.0114
  -5.250  -0.4397   0.01134   0.00462  -0.0303   0.9462   0.0119
  -5.000  -0.4113   0.01102   0.00423  -0.0304   0.9367   0.0125
  -4.750  -0.3835   0.01068   0.00382  -0.0303   0.9269   0.0137
  -4.500  -0.3569   0.01040   0.00349  -0.0300   0.9156   0.0155
  -4.250  -0.3313   0.01001   0.00315  -0.0295   0.9039   0.0287
  -4.000  -0.3069   0.00948   0.00282  -0.0290   0.8919   0.0727
  -3.750  -0.2818   0.00910   0.00256  -0.0285   0.8801   0.1117
  -3.500  -0.2563   0.00880   0.00235  -0.0280   0.8679   0.1464
  -3.250  -0.2309   0.00850   0.00216  -0.0276   0.8553   0.1869
  -3.000  -0.2050   0.00824   0.00199  -0.0272   0.8425   0.2243
  -2.750  -0.1802   0.00785   0.00184  -0.0268   0.8296   0.2949
  -2.500  -0.1549   0.00754   0.00171  -0.0263   0.8164   0.3561
  -2.250  -0.1287   0.00738   0.00161  -0.0260   0.8029   0.3894
  -2.000  -0.1022   0.00725   0.00151  -0.0256   0.7891   0.4202
  -1.750  -0.0758   0.00712   0.00143  -0.0253   0.7749   0.4532
  -1.500  -0.0494   0.00702   0.00136  -0.0249   0.7602   0.4849
  -1.250  -0.0229   0.00692   0.00130  -0.0246   0.7451   0.5167
  -1.000   0.0036   0.00684   0.00126  -0.0242   0.7295   0.5478
  -0.750   0.0301   0.00676   0.00122  -0.0239   0.7137   0.5784
  -0.500   0.0565   0.00670   0.00120  -0.0235   0.6975   0.6091
  -0.250   0.0829   0.00665   0.00119  -0.0231   0.6810   0.6397
   0.000   0.1092   0.00661   0.00119  -0.0227   0.6640   0.6696
   0.250   0.1354   0.00659   0.00120  -0.0223   0.6467   0.6988
   0.500   0.1615   0.00658   0.00122  -0.0218   0.6290   0.7271
   0.750   0.1876   0.00658   0.00125  -0.0213   0.6103   0.7546
   1.000   0.2136   0.00659   0.00129  -0.0208   0.5909   0.7815
   1.250   0.2395   0.00663   0.00134  -0.0202   0.5709   0.8076
   1.500   0.2652   0.00668   0.00140  -0.0196   0.5505   0.8324
   1.750   0.2910   0.00674   0.00147  -0.0190   0.5292   0.8560
   2.000   0.3167   0.00683   0.00155  -0.0184   0.5081   0.8791
   2.250   0.3430   0.00693   0.00163  -0.0179   0.4852   0.9008
   2.500   0.3708   0.00707   0.00173  -0.0178   0.4619   0.9218
   2.750   0.4009   0.00724   0.00185  -0.0182   0.4360   0.9405
   3.000   0.4334   0.00744   0.00197  -0.0192   0.4091   0.9552
   3.250   0.4668   0.00766   0.00209  -0.0205   0.3810   0.9668
   3.500   0.5000   0.00789   0.00224  -0.0218   0.3533   0.9764
   3.750   0.5326   0.00814   0.00240  -0.0229   0.3258   0.9850
   4.000   0.5669   0.00845   0.00257  -0.0246   0.2901   0.9909
   4.250   0.5992   0.00891   0.00280  -0.0259   0.2379   0.9972
   4.500   0.6264   0.00937   0.00305  -0.0262   0.1923   1.0000
   4.750   0.6478   0.00979   0.00330  -0.0251   0.1576   1.0000
   5.000   0.6698   0.01017   0.00357  -0.0241   0.1301   1.0000
   5.250   0.6917   0.01057   0.00385  -0.0232   0.1048   1.0000
   5.500   0.7142   0.01095   0.00414  -0.0223   0.0849   1.0000
   5.750   0.7362   0.01141   0.00449  -0.0213   0.0622   1.0000
   6.000   0.7578   0.01194   0.00489  -0.0203   0.0395   1.0000
   6.250   0.7785   0.01261   0.00541  -0.0193   0.0160   1.0000
   6.500   0.8012   0.01307   0.00585  -0.0184   0.0120   1.0000
   6.750   0.8246   0.01347   0.00629  -0.0177   0.0109   1.0000
   7.000   0.8476   0.01391   0.00677  -0.0169   0.0100   1.0000
   7.250   0.8699   0.01445   0.00739  -0.0160   0.0092   1.0000
   7.500   0.8926   0.01494   0.00794  -0.0152   0.0089   1.0000
   7.750   0.9150   0.01546   0.00853  -0.0144   0.0086   1.0000
   8.000   0.9368   0.01603   0.00917  -0.0135   0.0083   1.0000
   8.250   0.9582   0.01663   0.00985  -0.0126   0.0079   1.0000
   8.500   0.9793   0.01725   0.01053  -0.0117   0.0075   1.0000
   8.750   0.9994   0.01795   0.01129  -0.0106   0.0072   1.0000
   9.000   1.0183   0.01873   0.01214  -0.0095   0.0069   1.0000
   9.250   1.0359   0.01962   0.01311  -0.0082   0.0067   1.0000
   9.500   1.0509   0.02072   0.01429  -0.0066   0.0065   1.0000
   9.750   1.0638   0.02197   0.01565  -0.0047   0.0064   1.0000
  10.000   1.0799   0.02286   0.01663  -0.0033   0.0063   1.0000
  10.250   1.0948   0.02380   0.01767  -0.0017   0.0062   1.0000
  10.500   1.1071   0.02491   0.01889   0.0001   0.0062   1.0000
  10.750   1.1172   0.02595   0.02004   0.0023   0.0060   1.0000
  11.000   1.1244   0.02712   0.02133   0.0048   0.0060   1.0000
  11.250   1.1312   0.02834   0.02267   0.0071   0.0059   1.0000
  11.500   1.1359   0.02980   0.02427   0.0092   0.0058   1.0000
  11.750   1.1398   0.03138   0.02599   0.0112   0.0057   1.0000
  12.000   1.1427   0.03312   0.02788   0.0128   0.0056   1.0000
  12.250   1.1442   0.03509   0.02998   0.0142   0.0056   1.0000
  12.500   1.1440   0.03733   0.03238   0.0152   0.0054   1.0000
  12.750   1.1419   0.03993   0.03515   0.0159   0.0054   1.0000
  13.000   1.1386   0.04284   0.03821   0.0160   0.0054   1.0000
  13.250   1.1343   0.04604   0.04158   0.0157   0.0054   1.0000
  13.500   1.1284   0.04968   0.04538   0.0149   0.0054   1.0000
  13.750   1.1199   0.05394   0.04981   0.0134   0.0053   1.0000
  14.000   1.1097   0.05873   0.05477   0.0113   0.0053   1.0000
  14.250   1.0996   0.06382   0.06002   0.0087   0.0053   1.0000
  14.500   1.0861   0.06980   0.06617   0.0054   0.0053   1.0000
  14.750   1.0705   0.07650   0.07304   0.0016   0.0053   1.0000
  15.000   1.0544   0.08370   0.08039  -0.0027   0.0054   1.0000
  15.250   1.0371   0.09157   0.08843  -0.0074   0.0054   1.0000
  15.500   1.0191   0.10008   0.09707  -0.0126   0.0053   1.0000
  15.750   0.9970   0.10982   0.10696  -0.0184   0.0053   1.0000
  16.000   0.9738   0.12038   0.11768  -0.0245   0.0054   1.0000
  16.250   0.9480   0.13209   0.12953  -0.0312   0.0055   1.0000
  16.500   0.9140   0.14708   0.14466  -0.0393   0.0057   1.0000
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