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E475 (15.01%) (e475-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: E475 (15.01%) (e475-il)
Reynolds number: 200,000
Max Cl/Cd: 51.35 at α=9°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-e475-il-200000-n5.txt
Download as CSV file: xf-e475-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: E475  (15.01%)                                  
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -17.500  -1.0288   0.09186   0.08674  -0.0345   1.0000   0.0611
 -17.250  -1.0490   0.08527   0.08003  -0.0378   1.0000   0.0626
 -17.000  -1.0690   0.07889   0.07349  -0.0409   1.0000   0.0641
 -16.750  -1.0914   0.07238   0.06691  -0.0441   1.0000   0.0654
 -16.500  -1.1138   0.06599   0.06042  -0.0472   1.0000   0.0666
 -16.250  -1.1341   0.05999   0.05431  -0.0502   1.0000   0.0681
 -16.000  -1.1502   0.05474   0.04893  -0.0526   1.0000   0.0697
 -15.750  -1.1628   0.05015   0.04419  -0.0545   1.0000   0.0719
 -15.500  -1.1718   0.04624   0.04014  -0.0559   1.0000   0.0740
 -15.250  -1.1826   0.04246   0.03627  -0.0569   1.0000   0.0759
 -15.000  -1.1893   0.03942   0.03315  -0.0572   1.0000   0.0783
 -14.750  -1.1922   0.03701   0.03062  -0.0569   1.0000   0.0811
 -14.500  -1.1915   0.03506   0.02854  -0.0561   1.0000   0.0839
 -14.250  -1.1944   0.03310   0.02654  -0.0549   1.0000   0.0867
 -14.000  -1.1935   0.03156   0.02493  -0.0533   1.0000   0.0899
 -13.750  -1.1891   0.03032   0.02357  -0.0516   1.0000   0.0934
 -13.500  -1.1859   0.02914   0.02232  -0.0495   1.0000   0.0967
 -13.250  -1.1823   0.02810   0.02124  -0.0472   1.0000   0.1003
 -13.000  -1.1754   0.02725   0.02030  -0.0449   1.0000   0.1045
 -12.750  -1.1693   0.02645   0.01944  -0.0424   1.0000   0.1082
 -12.500  -1.1646   0.02574   0.01871  -0.0394   1.0000   0.1120
 -12.250  -1.1575   0.02515   0.01804  -0.0366   1.0000   0.1161
 -12.000  -1.1502   0.02460   0.01740  -0.0335   1.0000   0.1198
 -11.750  -1.1470   0.02409   0.01688  -0.0297   1.0000   0.1228
 -11.500  -1.1429   0.02368   0.01643  -0.0259   1.0000   0.1262
 -11.250  -1.1361   0.02329   0.01595  -0.0223   1.0000   0.1298
 -11.000  -1.1272   0.02285   0.01545  -0.0192   1.0000   0.1333
 -10.750  -1.1189   0.02243   0.01502  -0.0159   1.0000   0.1364
 -10.500  -1.1082   0.02206   0.01460  -0.0130   1.0000   0.1400
 -10.250  -1.0954   0.02169   0.01412  -0.0104   1.0000   0.1439
 -10.000  -1.0828   0.02130   0.01368  -0.0078   1.0000   0.1473
  -9.750  -1.0702   0.02095   0.01333  -0.0051   1.0000   0.1508
  -9.500  -1.0557   0.02062   0.01295  -0.0028   1.0000   0.1546
  -9.250  -1.0397   0.02031   0.01251  -0.0006   1.0000   0.1586
  -9.000  -1.0245   0.01996   0.01215   0.0016   1.0000   0.1621
  -8.750  -1.0087   0.01965   0.01183   0.0037   1.0000   0.1656
  -8.500  -0.9916   0.01936   0.01149   0.0057   1.0000   0.1694
  -8.250  -0.9736   0.01910   0.01111   0.0075   1.0000   0.1735
  -8.000  -0.9563   0.01878   0.01079   0.0094   1.0000   0.1769
  -7.750  -0.9385   0.01851   0.01052   0.0112   1.0000   0.1805
  -7.500  -0.9198   0.01827   0.01023   0.0129   1.0000   0.1845
  -7.250  -0.9004   0.01804   0.00991   0.0145   1.0000   0.1884
  -7.000  -0.8816   0.01776   0.00963   0.0162   1.0000   0.1917
  -6.750  -0.8627   0.01752   0.00939   0.0178   1.0000   0.1953
  -6.500  -0.8316   0.01732   0.00916   0.0170   0.9976   0.2000
  -6.250  -0.7969   0.01716   0.00891   0.0155   0.9945   0.2045
  -6.000  -0.7631   0.01690   0.00870   0.0141   0.9911   0.2088
  -5.750  -0.7279   0.01669   0.00849   0.0126   0.9867   0.2136
  -5.500  -0.6874   0.01652   0.00826   0.0099   0.9824   0.2188
  -5.250  -0.6496   0.01625   0.00800   0.0079   0.9763   0.2233
  -5.000  -0.6057   0.01597   0.00776   0.0047   0.9700   0.2289
  -4.750  -0.5658   0.01571   0.00747   0.0024   0.9621   0.2343
  -4.500  -0.5208   0.01539   0.00716  -0.0010   0.9554   0.2394
  -4.250  -0.4865   0.01508   0.00690  -0.0021   0.9473   0.2446
  -4.000  -0.4466   0.01480   0.00663  -0.0044   0.9410   0.2510
  -3.750  -0.4130   0.01452   0.00637  -0.0053   0.9336   0.2561
  -3.500  -0.3801   0.01421   0.00613  -0.0061   0.9253   0.2618
  -3.250  -0.3520   0.01397   0.00589  -0.0059   0.9144   0.2680
  -3.000  -0.3214   0.01368   0.00565  -0.0061   0.9035   0.2741
  -2.750  -0.2969   0.01343   0.00544  -0.0052   0.8874   0.2802
  -2.500  -0.2726   0.01321   0.00522  -0.0041   0.8656   0.2868
  -2.250  -0.2377   0.01286   0.00492  -0.0051   0.8369   0.2950
  -1.750  -0.1551   0.01232   0.00411  -0.0093   0.7253   0.3160
  -1.500  -0.1304   0.01239   0.00393  -0.0082   0.6608   0.3259
  -1.250  -0.1086   0.01251   0.00384  -0.0067   0.6040   0.3375
  -1.000  -0.0875   0.01259   0.00378  -0.0052   0.5555   0.3502
  -0.750  -0.0659   0.01266   0.00374  -0.0038   0.5153   0.3647
  -0.500  -0.0441   0.01272   0.00371  -0.0025   0.4802   0.3807
  -0.250  -0.0220   0.01276   0.00369  -0.0012   0.4489   0.3995
   0.000   0.0000   0.01278   0.00369   0.0000   0.4222   0.4222
   0.250   0.0220   0.01276   0.00369   0.0012   0.3994   0.4489
   0.500   0.0441   0.01272   0.00371   0.0025   0.3807   0.4801
   0.750   0.0659   0.01267   0.00374   0.0038   0.3646   0.5153
   1.000   0.0875   0.01260   0.00378   0.0052   0.3502   0.5555
   1.250   0.1086   0.01251   0.00384   0.0067   0.3374   0.6039
   1.500   0.1304   0.01239   0.00393   0.0082   0.3259   0.6610
   1.750   0.1551   0.01232   0.00411   0.0093   0.3161   0.7255
   2.000   0.1901   0.01248   0.00446   0.0084   0.3059   0.7905
   2.250   0.2377   0.01286   0.00492   0.0051   0.2950   0.8370
   2.500   0.2725   0.01321   0.00522   0.0041   0.2868   0.8658
   2.750   0.2969   0.01343   0.00544   0.0052   0.2802   0.8873
   3.000   0.3216   0.01368   0.00565   0.0061   0.2740   0.9033
   3.250   0.3520   0.01397   0.00589   0.0059   0.2680   0.9146
   3.500   0.3798   0.01421   0.00612   0.0062   0.2617   0.9252
   3.750   0.4129   0.01452   0.00637   0.0053   0.2561   0.9337
   4.000   0.4465   0.01480   0.00662   0.0044   0.2509   0.9410
   4.250   0.4864   0.01507   0.00691   0.0021   0.2448   0.9473
   4.500   0.5208   0.01539   0.00716   0.0009   0.2394   0.9555
   4.750   0.5659   0.01571   0.00747  -0.0024   0.2343   0.9621
   5.000   0.6057   0.01597   0.00776  -0.0047   0.2288   0.9700
   5.250   0.6497   0.01624   0.00800  -0.0079   0.2233   0.9764
   5.500   0.6875   0.01652   0.00826  -0.0100   0.2188   0.9824
   5.750   0.7280   0.01669   0.00848  -0.0126   0.2136   0.9867
   6.000   0.7631   0.01690   0.00869  -0.0142   0.2088   0.9911
   6.250   0.7970   0.01716   0.00890  -0.0156   0.2046   0.9945
   6.500   0.8317   0.01732   0.00915  -0.0170   0.1999   0.9977
   6.750   0.8625   0.01751   0.00938  -0.0178   0.1952   1.0000
   7.000   0.8815   0.01776   0.00962  -0.0161   0.1916   1.0000
   7.250   0.9003   0.01804   0.00990  -0.0145   0.1884   1.0000
   7.500   0.9197   0.01826   0.01022  -0.0129   0.1843   1.0000
   7.750   0.9384   0.01850   0.01051  -0.0112   0.1805   1.0000
   8.000   0.9562   0.01877   0.01078  -0.0094   0.1769   1.0000
   8.250   0.9735   0.01910   0.01111  -0.0075   0.1736   1.0000
   8.500   0.9916   0.01936   0.01149  -0.0057   0.1696   1.0000
   8.750   1.0087   0.01965   0.01183  -0.0037   0.1657   1.0000
   9.000   1.0244   0.01995   0.01214  -0.0016   0.1621   1.0000
   9.250   1.0397   0.02031   0.01251   0.0006   0.1586   1.0000
   9.500   1.0557   0.02062   0.01294   0.0028   0.1547   1.0000
   9.750   1.0701   0.02094   0.01332   0.0051   0.1508   1.0000
  10.000   1.0828   0.02130   0.01368   0.0078   0.1473   1.0000
  10.250   1.0954   0.02169   0.01412   0.0104   0.1440   1.0000
  10.500   1.1083   0.02205   0.01460   0.0130   0.1401   1.0000
  10.750   1.1190   0.02243   0.01502   0.0159   0.1364   1.0000
  11.000   1.1272   0.02285   0.01544   0.0192   0.1332   1.0000
  11.250   1.1363   0.02328   0.01594   0.0223   0.1299   1.0000
  11.500   1.1431   0.02368   0.01643   0.0258   0.1262   1.0000
  11.750   1.1473   0.02409   0.01688   0.0297   0.1228   1.0000
  12.000   1.1504   0.02460   0.01739   0.0335   0.1197   1.0000
  12.250   1.1579   0.02514   0.01803   0.0365   0.1160   1.0000
  12.500   1.1650   0.02573   0.01871   0.0394   0.1120   1.0000
  12.750   1.1698   0.02645   0.01943   0.0423   0.1081   1.0000
  13.000   1.1761   0.02724   0.02029   0.0448   0.1044   1.0000
  13.250   1.1829   0.02809   0.02123   0.0471   0.1002   1.0000
  13.500   1.1866   0.02913   0.02230   0.0494   0.0965   1.0000
  13.750   1.1901   0.03030   0.02355   0.0514   0.0933   1.0000
  14.000   1.1944   0.03155   0.02491   0.0532   0.0898   1.0000
  14.250   1.1953   0.03309   0.02653   0.0547   0.0866   1.0000
  14.500   1.1927   0.03503   0.02851   0.0560   0.0840   1.0000
  14.750   1.1934   0.03697   0.03059   0.0567   0.0810   1.0000
  15.000   1.1905   0.03940   0.03312   0.0570   0.0781   1.0000
  15.250   1.1836   0.04246   0.03627   0.0567   0.0757   1.0000
  15.500   1.1728   0.04624   0.04013   0.0557   0.0738   1.0000
  15.750   1.1645   0.05008   0.04412   0.0544   0.0716   1.0000
  16.000   1.1523   0.05463   0.04882   0.0524   0.0697   1.0000
  16.250   1.1361   0.05989   0.05421   0.0500   0.0680   1.0000
  16.500   1.1160   0.06586   0.06029   0.0471   0.0666   1.0000
  16.750   1.0931   0.07233   0.06686   0.0439   0.0653   1.0000
  17.000   1.0717   0.07870   0.07330   0.0408   0.0641   1.0000
  17.250   1.0509   0.08521   0.07996   0.0375   0.0625   1.0000
  17.500   1.0305   0.09185   0.08672   0.0342   0.0609   1.0000
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