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E475 (15.01%) (e475-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: E475 (15.01%) (e475-il)
Reynolds number: 1,000,000
Max Cl/Cd: 89.97 at α=11°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-e475-il-1000000.txt
Download as CSV file: xf-e475-il-1000000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.000  -1.2160   0.08422   0.08042  -0.0376   1.0000   0.0255
 -18.750  -1.2543   0.07562   0.07167  -0.0416   1.0000   0.0253
 -18.500  -1.2912   0.06738   0.06327  -0.0454   1.0000   0.0252
 -18.250  -1.3243   0.05963   0.05536  -0.0489   1.0000   0.0253
 -18.000  -1.3514   0.05274   0.04832  -0.0521   1.0000   0.0254
 -17.750  -1.3692   0.04719   0.04262  -0.0547   1.0000   0.0259
 -17.500  -1.3863   0.04198   0.03729  -0.0569   1.0000   0.0267
 -17.250  -1.3993   0.03764   0.03285  -0.0584   1.0000   0.0279
 -17.000  -1.4055   0.03444   0.02956  -0.0589   1.0000   0.0289
 -16.750  -1.4081   0.03188   0.02692  -0.0588   1.0000   0.0306
 -16.500  -1.4131   0.02939   0.02436  -0.0581   1.0000   0.0323
 -16.250  -1.4142   0.02746   0.02238  -0.0569   1.0000   0.0343
 -16.000  -1.4114   0.02597   0.02083  -0.0555   1.0000   0.0363
 -15.750  -1.4113   0.02444   0.01927  -0.0535   1.0000   0.0387
 -15.500  -1.4064   0.02331   0.01808  -0.0515   1.0000   0.0409
 -15.250  -1.4021   0.02222   0.01697  -0.0493   1.0000   0.0436
 -15.000  -1.3967   0.02126   0.01599  -0.0469   1.0000   0.0464
 -14.750  -1.3880   0.02052   0.01521  -0.0447   1.0000   0.0488
 -14.500  -1.3823   0.01968   0.01436  -0.0419   1.0000   0.0519
 -14.250  -1.3739   0.01903   0.01369  -0.0394   1.0000   0.0548
 -14.000  -1.3655   0.01844   0.01307  -0.0366   1.0000   0.0577
 -13.750  -1.3588   0.01783   0.01247  -0.0335   1.0000   0.0611
 -13.500  -1.3512   0.01741   0.01202  -0.0302   1.0000   0.0640
 -13.250  -1.3501   0.01699   0.01159  -0.0257   1.0000   0.0671
 -13.000  -1.3549   0.01668   0.01128  -0.0198   1.0000   0.0699
 -12.750  -1.3591   0.01646   0.01103  -0.0139   1.0000   0.0722
 -12.500  -1.3542   0.01614   0.01068  -0.0098   1.0000   0.0754
 -12.250  -1.3472   0.01573   0.01029  -0.0061   1.0000   0.0796
 -12.000  -1.3358   0.01542   0.00995  -0.0032   1.0000   0.0834
 -11.750  -1.3248   0.01502   0.00957  -0.0002   1.0000   0.0880
 -11.500  -1.3069   0.01467   0.00922   0.0015   0.9997   0.0923
 -11.250  -1.2809   0.01435   0.00889   0.0016   0.9989   0.0964
 -11.000  -1.2558   0.01396   0.00853   0.0018   0.9978   0.1023
 -10.750  -1.2283   0.01371   0.00826   0.0017   0.9968   0.1061
 -10.500  -1.2010   0.01337   0.00793   0.0015   0.9956   0.1112
 -10.250  -1.1734   0.01310   0.00768   0.0013   0.9947   0.1164
 -10.000  -1.1443   0.01290   0.00745   0.0009   0.9938   0.1202
  -9.750  -1.1149   0.01260   0.00719   0.0004   0.9930   0.1264
  -9.500  -1.0885   0.01242   0.00701   0.0006   0.9918   0.1314
  -9.250  -1.0636   0.01216   0.00676   0.0011   0.9901   0.1366
  -9.000  -1.0362   0.01194   0.00656   0.0011   0.9885   0.1410
  -8.750  -1.0068   0.01179   0.00639   0.0007   0.9871   0.1447
  -8.500  -0.9769   0.01158   0.00619   0.0003   0.9857   0.1489
  -8.250  -0.9457   0.01138   0.00600  -0.0005   0.9845   0.1537
  -8.000  -0.9111   0.01123   0.00585  -0.0019   0.9834   0.1579
  -7.750  -0.8738   0.01106   0.00568  -0.0038   0.9823   0.1620
  -7.500  -0.8324   0.01083   0.00549  -0.0067   0.9812   0.1676
  -7.250  -0.8023   0.01061   0.00527  -0.0070   0.9768   0.1716
  -7.000  -0.7577   0.01039   0.00503  -0.0103   0.9738   0.1749
  -6.750  -0.7088   0.01000   0.00470  -0.0146   0.9718   0.1814
  -6.500  -0.6598   0.00970   0.00441  -0.0189   0.9700   0.1861
  -6.250  -0.6210   0.00953   0.00422  -0.0210   0.9682   0.1892
  -6.000  -0.5993   0.00934   0.00406  -0.0196   0.9634   0.1932
  -5.750  -0.5716   0.00915   0.00390  -0.0194   0.9597   0.1975
  -5.500  -0.5416   0.00900   0.00375  -0.0196   0.9565   0.2014
  -5.250  -0.5120   0.00888   0.00361  -0.0197   0.9536   0.2042
  -5.000  -0.4897   0.00874   0.00348  -0.0183   0.9480   0.2076
  -4.750  -0.4642   0.00855   0.00331  -0.0176   0.9424   0.2123
  -4.500  -0.4372   0.00841   0.00318  -0.0171   0.9377   0.2163
  -4.250  -0.4130   0.00831   0.00307  -0.0161   0.9311   0.2193
  -4.000  -0.3868   0.00818   0.00293  -0.0154   0.9242   0.2222
  -3.750  -0.3623   0.00801   0.00279  -0.0144   0.9155   0.2275
  -3.500  -0.3364   0.00787   0.00265  -0.0137   0.9049   0.2320
  -3.250  -0.3107   0.00776   0.00253  -0.0130   0.8898   0.2357
  -3.000  -0.2852   0.00765   0.00239  -0.0121   0.8626   0.2394
  -2.750  -0.2627   0.00765   0.00218  -0.0106   0.7969   0.2449
  -2.500  -0.2423   0.00785   0.00211  -0.0087   0.7230   0.2498
  -2.250  -0.2206   0.00807   0.00208  -0.0073   0.6560   0.2537
  -2.000  -0.1985   0.00819   0.00203  -0.0059   0.5989   0.2603
  -1.750  -0.1748   0.00830   0.00200  -0.0050   0.5507   0.2664
  -1.500  -0.1504   0.00841   0.00197  -0.0041   0.5089   0.2727
  -1.250  -0.1260   0.00847   0.00194  -0.0033   0.4713   0.2816
  -1.000  -0.1010   0.00855   0.00192  -0.0026   0.4365   0.2898
  -0.750  -0.0762   0.00860   0.00191  -0.0019   0.4062   0.3002
  -0.500  -0.0508   0.00862   0.00189  -0.0012   0.3817   0.3121
  -0.250  -0.0254   0.00864   0.00189  -0.0006   0.3607   0.3260
   0.000   0.0000   0.00865   0.00188   0.0000   0.3423   0.3424
   0.250   0.0254   0.00864   0.00189   0.0006   0.3261   0.3607
   0.500   0.0508   0.00862   0.00189   0.0012   0.3118   0.3817
   0.750   0.0762   0.00860   0.00191   0.0019   0.3003   0.4061
   1.000   0.1011   0.00855   0.00192   0.0026   0.2899   0.4359
   1.250   0.1260   0.00847   0.00194   0.0033   0.2817   0.4710
   1.500   0.1504   0.00841   0.00197   0.0041   0.2729   0.5088
   1.750   0.1748   0.00830   0.00200   0.0050   0.2664   0.5505
   2.000   0.1985   0.00819   0.00203   0.0059   0.2603   0.5990
   2.250   0.2206   0.00807   0.00208   0.0073   0.2537   0.6559
   2.500   0.2424   0.00786   0.00211   0.0087   0.2498   0.7224
   2.750   0.2627   0.00765   0.00218   0.0106   0.2449   0.7973
   3.000   0.2852   0.00765   0.00238   0.0121   0.2395   0.8626
   3.250   0.3107   0.00776   0.00253   0.0129   0.2356   0.8897
   3.500   0.3365   0.00787   0.00265   0.0137   0.2320   0.9046
   3.750   0.3623   0.00801   0.00279   0.0144   0.2275   0.9156
   4.000   0.3868   0.00818   0.00293   0.0154   0.2222   0.9243
   4.250   0.4130   0.00831   0.00307   0.0161   0.2193   0.9311
   4.500   0.4372   0.00841   0.00318   0.0171   0.2162   0.9377
   4.750   0.4642   0.00855   0.00332   0.0176   0.2123   0.9425
   5.000   0.4897   0.00874   0.00348   0.0183   0.2077   0.9481
   5.250   0.5121   0.00888   0.00361   0.0197   0.2042   0.9536
   5.500   0.5417   0.00900   0.00374   0.0196   0.2014   0.9565
   5.750   0.5716   0.00915   0.00389   0.0193   0.1974   0.9597
   6.000   0.5994   0.00934   0.00406   0.0195   0.1934   0.9635
   6.250   0.6207   0.00952   0.00422   0.0211   0.1892   0.9681
   6.500   0.6604   0.00970   0.00442   0.0188   0.1861   0.9701
   6.750   0.7088   0.01000   0.00470   0.0146   0.1812   0.9718
   7.000   0.7579   0.01039   0.00503   0.0103   0.1750   0.9739
   7.250   0.8025   0.01061   0.00527   0.0070   0.1716   0.9768
   7.500   0.8325   0.01082   0.00548   0.0067   0.1676   0.9813
   7.750   0.8739   0.01106   0.00568   0.0038   0.1617   0.9823
   8.000   0.9113   0.01122   0.00585   0.0019   0.1579   0.9834
   8.250   0.9458   0.01137   0.00600   0.0005   0.1538   0.9845
   8.500   0.9770   0.01158   0.00618  -0.0003   0.1489   0.9857
   8.750   1.0069   0.01179   0.00639  -0.0008   0.1447   0.9871
   9.000   1.0364   0.01194   0.00656  -0.0011   0.1410   0.9885
   9.250   1.0637   0.01216   0.00676  -0.0011   0.1363   0.9901
   9.500   1.0886   0.01242   0.00700  -0.0006   0.1313   0.9919
   9.750   1.1151   0.01260   0.00719  -0.0004   0.1268   0.9931
  10.000   1.1446   0.01289   0.00744  -0.0010   0.1203   0.9939
  10.250   1.1737   0.01310   0.00767  -0.0014   0.1164   0.9947
  10.500   1.2013   0.01337   0.00793  -0.0016   0.1114   0.9957
  10.750   1.2287   0.01371   0.00825  -0.0017   0.1061   0.9968
  11.000   1.2560   0.01396   0.00853  -0.0018   0.1022   0.9979
  11.250   1.2813   0.01434   0.00887  -0.0016   0.0969   0.9989
  11.500   1.3072   0.01467   0.00922  -0.0015   0.0924   0.9997
  11.750   1.3246   0.01502   0.00956   0.0002   0.0877   1.0000
  12.000   1.3358   0.01541   0.00995   0.0032   0.0833   1.0000
  12.250   1.3471   0.01573   0.01028   0.0062   0.0795   1.0000
  12.500   1.3541   0.01613   0.01068   0.0098   0.0754   1.0000
  12.750   1.3592   0.01646   0.01103   0.0139   0.0724   1.0000
  13.000   1.3551   0.01668   0.01127   0.0198   0.0700   1.0000
  13.250   1.3501   0.01699   0.01159   0.0257   0.0670   1.0000
  13.500   1.3515   0.01741   0.01201   0.0301   0.0637   1.0000
  13.750   1.3592   0.01783   0.01247   0.0334   0.0610   1.0000
  14.000   1.3661   0.01843   0.01306   0.0365   0.0577   1.0000
  14.250   1.3745   0.01903   0.01368   0.0392   0.0547   1.0000
  14.500   1.3832   0.01967   0.01435   0.0418   0.0519   1.0000
  14.750   1.3887   0.02052   0.01521   0.0446   0.0486   1.0000
  15.000   1.3974   0.02126   0.01599   0.0468   0.0461   1.0000
  15.250   1.4024   0.02225   0.01699   0.0492   0.0433   1.0000
  15.500   1.4076   0.02329   0.01807   0.0514   0.0409   1.0000
  15.750   1.4118   0.02447   0.01929   0.0534   0.0384   1.0000
  16.000   1.4119   0.02601   0.02086   0.0553   0.0359   1.0000
  16.250   1.4152   0.02747   0.02238   0.0567   0.0340   1.0000
  16.500   1.4146   0.02937   0.02434   0.0579   0.0322   1.0000
  16.750   1.4103   0.03181   0.02683   0.0586   0.0304   1.0000
  17.000   1.4086   0.03429   0.02940   0.0586   0.0292   1.0000
  17.250   1.4007   0.03767   0.03287   0.0581   0.0277   1.0000
  17.500   1.3885   0.04194   0.03724   0.0566   0.0266   1.0000
  17.750   1.3724   0.04703   0.04245   0.0544   0.0258   1.0000
  18.000   1.3545   0.05262   0.04819   0.0518   0.0254   1.0000
  18.250   1.3278   0.05948   0.05521   0.0486   0.0251   1.0000
  18.500   1.2950   0.06720   0.06309   0.0450   0.0253   1.0000
  18.750   1.2583   0.07542   0.07146   0.0413   0.0252   1.0000
  19.000   1.2200   0.08403   0.08023   0.0373   0.0252   1.0000
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