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E475 (15.01%) (e475-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: E475 (15.01%) (e475-il)
Reynolds number: 1,000,000
Max Cl/Cd: 83.59 at α=10.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-e475-il-1000000-n5.txt
Download as CSV file: xf-e475-il-1000000-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 =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -18.750  -1.1947   0.08406   0.08003  -0.0372   1.0000   0.0178
 -18.500  -1.2292   0.07595   0.07178  -0.0409   1.0000   0.0177
 -18.250  -1.2664   0.06762   0.06329  -0.0446   1.0000   0.0177
 -18.000  -1.2968   0.06020   0.05570  -0.0480   1.0000   0.0174
 -17.750  -1.3227   0.05342   0.04877  -0.0512   1.0000   0.0175
 -17.500  -1.3417   0.04764   0.04284  -0.0539   1.0000   0.0177
 -17.250  -1.3554   0.04278   0.03786  -0.0560   1.0000   0.0183
 -16.750  -1.3731   0.03521   0.03008  -0.0583   1.0000   0.0197
 -16.500  -1.3761   0.03254   0.02732  -0.0583   1.0000   0.0204
 -16.250  -1.3770   0.03032   0.02502  -0.0578   1.0000   0.0213
 -16.000  -1.3770   0.02839   0.02304  -0.0569   1.0000   0.0225
 -15.750  -1.3763   0.02670   0.02128  -0.0555   1.0000   0.0237
 -15.500  -1.3733   0.02532   0.01985  -0.0538   1.0000   0.0250
 -15.250  -1.3691   0.02410   0.01859  -0.0519   1.0000   0.0266
 -15.000  -1.3653   0.02297   0.01742  -0.0497   1.0000   0.0285
 -14.750  -1.3588   0.02205   0.01646  -0.0475   1.0000   0.0303
 -14.500  -1.3530   0.02116   0.01554  -0.0450   1.0000   0.0323
 -14.250  -1.3460   0.02038   0.01474  -0.0425   1.0000   0.0346
 -14.000  -1.3387   0.01968   0.01401  -0.0398   1.0000   0.0369
 -13.750  -1.3317   0.01902   0.01334  -0.0369   1.0000   0.0395
 -13.500  -1.3243   0.01848   0.01277  -0.0338   1.0000   0.0421
 -13.250  -1.3207   0.01795   0.01223  -0.0300   1.0000   0.0447
 -13.000  -1.3205   0.01757   0.01184  -0.0252   1.0000   0.0471
 -12.750  -1.3021   0.01702   0.01129  -0.0241   0.9987   0.0506
 -12.500  -1.2799   0.01647   0.01073  -0.0237   0.9967   0.0549
 -12.250  -1.2579   0.01588   0.01017  -0.0233   0.9945   0.0605
 -12.000  -1.2331   0.01544   0.00972  -0.0232   0.9929   0.0646
 -11.750  -1.2117   0.01496   0.00926  -0.0224   0.9909   0.0688
 -11.500  -1.1878   0.01455   0.00885  -0.0220   0.9891   0.0735
 -11.250  -1.1635   0.01409   0.00842  -0.0217   0.9875   0.0787
 -11.000  -1.1374   0.01374   0.00806  -0.0216   0.9862   0.0830
 -10.750  -1.1113   0.01335   0.00769  -0.0216   0.9851   0.0881
 -10.500  -1.0840   0.01301   0.00736  -0.0218   0.9842   0.0932
 -10.250  -1.0563   0.01264   0.00702  -0.0221   0.9833   0.0995
 -10.000  -1.0278   0.01232   0.00672  -0.0224   0.9826   0.1060
  -9.750  -0.9996   0.01199   0.00642  -0.0228   0.9819   0.1118
  -9.500  -0.9708   0.01173   0.00616  -0.0231   0.9812   0.1165
  -9.250  -0.9461   0.01154   0.00596  -0.0225   0.9795   0.1195
  -9.000  -0.9221   0.01129   0.00573  -0.0218   0.9776   0.1243
  -8.750  -0.8962   0.01108   0.00553  -0.0215   0.9760   0.1286
  -8.500  -0.8687   0.01090   0.00534  -0.0215   0.9746   0.1320
  -8.250  -0.8411   0.01067   0.00513  -0.0215   0.9732   0.1365
  -8.000  -0.8132   0.01048   0.00494  -0.0215   0.9721   0.1408
  -7.750  -0.7846   0.01031   0.00478  -0.0217   0.9710   0.1446
  -7.500  -0.7536   0.01009   0.00457  -0.0223   0.9691   0.1490
  -7.250  -0.7289   0.00987   0.00435  -0.0214   0.9614   0.1533
  -7.000  -0.7030   0.00965   0.00412  -0.0207   0.9515   0.1571
  -6.750  -0.6802   0.00950   0.00393  -0.0193   0.9403   0.1596
  -6.500  -0.6566   0.00933   0.00376  -0.0183   0.9315   0.1636
  -6.250  -0.6315   0.00917   0.00361  -0.0175   0.9245   0.1679
  -6.000  -0.6057   0.00904   0.00347  -0.0169   0.9188   0.1711
  -5.750  -0.5799   0.00892   0.00335  -0.0163   0.9117   0.1738
  -5.500  -0.5541   0.00878   0.00320  -0.0157   0.9043   0.1777
  -5.250  -0.5283   0.00865   0.00308  -0.0151   0.8948   0.1816
  -5.000  -0.5025   0.00853   0.00294  -0.0144   0.8784   0.1848
  -4.750  -0.4788   0.00850   0.00275  -0.0132   0.8274   0.1879
  -4.500  -0.4578   0.00864   0.00262  -0.0115   0.7565   0.1907
  -4.250  -0.4356   0.00874   0.00254  -0.0102   0.6998   0.1944
  -4.000  -0.4125   0.00884   0.00247  -0.0090   0.6485   0.1978
  -3.750  -0.3888   0.00893   0.00241  -0.0081   0.5998   0.2013
  -3.500  -0.3644   0.00904   0.00235  -0.0072   0.5518   0.2043
  -3.000  -0.3145   0.00913   0.00222  -0.0058   0.4800   0.2115
  -2.750  -0.2889   0.00916   0.00217  -0.0052   0.4512   0.2153
  -2.500  -0.2631   0.00921   0.00213  -0.0047   0.4237   0.2190
  -2.250  -0.2372   0.00926   0.00209  -0.0041   0.3971   0.2225
  -1.750  -0.1854   0.00930   0.00201  -0.0031   0.3557   0.2314
  -1.500  -0.1589   0.00932   0.00198  -0.0026   0.3399   0.2357
  -1.250  -0.1325   0.00932   0.00196  -0.0022   0.3256   0.2409
  -1.000  -0.1062   0.00932   0.00194  -0.0017   0.3119   0.2466
  -0.750  -0.0796   0.00935   0.00192  -0.0013   0.2992   0.2515
  -0.250  -0.0266   0.00934   0.00191  -0.0004   0.2807   0.2651
   0.000   0.0000   0.00936   0.00190   0.0000   0.2722   0.2722
   0.250   0.0266   0.00934   0.00191   0.0004   0.2652   0.2807
   0.750   0.0797   0.00935   0.00192   0.0013   0.2515   0.2992
   1.000   0.1062   0.00933   0.00194   0.0017   0.2467   0.3114
   1.250   0.1325   0.00932   0.00196   0.0022   0.2411   0.3255
   1.500   0.1589   0.00932   0.00198   0.0026   0.2358   0.3397
   1.750   0.1854   0.00930   0.00201   0.0031   0.2314   0.3556
   2.250   0.2372   0.00926   0.00209   0.0041   0.2225   0.3970
   2.500   0.2632   0.00921   0.00213   0.0047   0.2190   0.4234
   2.750   0.2889   0.00916   0.00217   0.0052   0.2152   0.4512
   3.000   0.3145   0.00913   0.00222   0.0058   0.2115   0.4801
   3.250   0.3397   0.00911   0.00228   0.0065   0.2076   0.5119
   3.500   0.3647   0.00905   0.00235   0.0072   0.2042   0.5489
   3.750   0.3887   0.00893   0.00241   0.0081   0.2013   0.6003
   4.000   0.4125   0.00883   0.00247   0.0091   0.1978   0.6498
   4.250   0.4356   0.00874   0.00254   0.0102   0.1944   0.7000
   4.750   0.4786   0.00849   0.00275   0.0133   0.1880   0.8293
   5.000   0.5025   0.00853   0.00294   0.0144   0.1849   0.8792
   5.250   0.5284   0.00865   0.00308   0.0151   0.1815   0.8947
   5.500   0.5541   0.00878   0.00320   0.0157   0.1777   0.9043
   5.750   0.5800   0.00892   0.00335   0.0163   0.1738   0.9117
   6.000   0.6057   0.00904   0.00347   0.0169   0.1712   0.9190
   6.250   0.6316   0.00916   0.00360   0.0175   0.1679   0.9243
   6.500   0.6566   0.00933   0.00376   0.0183   0.1636   0.9317
   6.750   0.6803   0.00950   0.00393   0.0193   0.1596   0.9403
   7.000   0.7030   0.00965   0.00412   0.0207   0.1572   0.9516
   7.250   0.7290   0.00987   0.00436   0.0214   0.1533   0.9615
   7.500   0.7537   0.01009   0.00457   0.0223   0.1490   0.9691
   7.750   0.7847   0.01031   0.00478   0.0216   0.1448   0.9710
   8.000   0.8133   0.01047   0.00494   0.0215   0.1410   0.9721
   8.250   0.8412   0.01068   0.00513   0.0214   0.1363   0.9733
   8.500   0.8689   0.01090   0.00534   0.0214   0.1317   0.9746
   8.750   0.8963   0.01108   0.00552   0.0215   0.1283   0.9761
   9.000   0.9223   0.01129   0.00573   0.0218   0.1243   0.9776
   9.250   0.9463   0.01153   0.00595   0.0225   0.1197   0.9796
   9.500   0.9711   0.01173   0.00616   0.0230   0.1165   0.9813
   9.750   0.9999   0.01199   0.00642   0.0227   0.1118   0.9819
  10.000   1.0281   0.01232   0.00672   0.0224   0.1055   0.9826
  10.250   1.0566   0.01264   0.00702   0.0220   0.0992   0.9833
  10.500   1.0844   0.01301   0.00736   0.0217   0.0932   0.9842
  10.750   1.1116   0.01336   0.00770   0.0216   0.0876   0.9851
  11.000   1.1379   0.01374   0.00806   0.0216   0.0832   0.9863
  11.250   1.1639   0.01409   0.00841   0.0216   0.0787   0.9875
  11.750   1.2126   0.01493   0.00924   0.0222   0.0696   0.9908
  12.000   1.2337   0.01545   0.00973   0.0231   0.0644   0.9929
  12.250   1.2585   0.01589   0.01017   0.0232   0.0602   0.9945
  12.500   1.2807   0.01646   0.01073   0.0236   0.0551   0.9967
  12.750   1.3034   0.01698   0.01125   0.0239   0.0513   0.9987
  13.000   1.3211   0.01755   0.01183   0.0251   0.0475   1.0000
  13.250   1.3207   0.01795   0.01224   0.0300   0.0444   1.0000
  13.500   1.3237   0.01852   0.01280   0.0339   0.0414   1.0000
  13.750   1.3321   0.01903   0.01334   0.0368   0.0393   1.0000
  14.000   1.3389   0.01970   0.01402   0.0397   0.0366   1.0000
  14.250   1.3465   0.02038   0.01474   0.0424   0.0345   1.0000
  14.500   1.3540   0.02114   0.01552   0.0449   0.0324   1.0000
  14.750   1.3597   0.02205   0.01645   0.0474   0.0302   1.0000
  15.000   1.3661   0.02297   0.01742   0.0496   0.0283   1.0000
  15.250   1.3700   0.02411   0.01858   0.0518   0.0265   1.0000
  15.500   1.3746   0.02530   0.01982   0.0536   0.0250   1.0000
  15.750   1.3773   0.02671   0.02128   0.0553   0.0235   1.0000
  16.000   1.3768   0.02849   0.02312   0.0567   0.0220   1.0000
  16.250   1.3783   0.03031   0.02501   0.0576   0.0211   1.0000
  16.500   1.3772   0.03256   0.02734   0.0581   0.0202   1.0000
  16.750   1.3729   0.03538   0.03025   0.0580   0.0193   1.0000
  17.000   1.3680   0.03857   0.03353   0.0573   0.0189   1.0000
  17.250   1.3579   0.04270   0.03777   0.0558   0.0182   1.0000
  17.500   1.3448   0.04749   0.04269   0.0536   0.0177   1.0000
  17.750   1.3257   0.05330   0.04864   0.0509   0.0174   1.0000
  18.000   1.3007   0.05997   0.05547   0.0478   0.0174   1.0000
  18.250   1.2687   0.06765   0.06331   0.0442   0.0175   1.0000
  18.500   1.2356   0.07542   0.07124   0.0407   0.0179   1.0000
  18.750   1.1978   0.08399   0.07996   0.0368   0.0177   1.0000
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