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EH 1.0/9.0 (eh1090-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: EH 1.0/9.0 (eh1090-il)
Reynolds number: 1,000,000
Max Cl/Cd: 73.4 at α=4.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-eh1090-il-1000000-n5.txt
Download as CSV file: xf-eh1090-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: EH 1.0/9.0                                      
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -12.250  -0.8921   0.06725   0.06569  -0.0108   1.0000   0.0029
 -12.000  -0.8784   0.06569   0.06413  -0.0119   1.0000   0.0029
 -11.750  -0.9772   0.04185   0.03978  -0.0269   1.0000   0.0028
 -11.500  -0.9981   0.03845   0.03619  -0.0241   1.0000   0.0027
 -11.250  -0.9923   0.03711   0.03475  -0.0224   1.0000   0.0028
 -11.000  -0.9939   0.03426   0.03168  -0.0205   1.0000   0.0028
 -10.750  -1.0044   0.02977   0.02675  -0.0179   1.0000   0.0029
 -10.500  -1.0047   0.02613   0.02271  -0.0155   1.0000   0.0031
 -10.250  -0.9892   0.02465   0.02105  -0.0144   1.0000   0.0032
 -10.000  -0.9710   0.02349   0.01976  -0.0135   1.0000   0.0033
  -9.750  -0.9501   0.02272   0.01890  -0.0129   1.0000   0.0035
  -9.500  -0.9302   0.02168   0.01773  -0.0121   1.0000   0.0036
  -9.250  -0.9106   0.02051   0.01640  -0.0112   1.0000   0.0037
  -9.000  -0.8892   0.01962   0.01539  -0.0104   1.0000   0.0038
  -8.750  -0.8673   0.01877   0.01442  -0.0097   1.0000   0.0040
  -8.500  -0.8461   0.01773   0.01323  -0.0088   1.0000   0.0041
  -8.250  -0.8243   0.01675   0.01211  -0.0080   1.0000   0.0042
  -8.000  -0.8016   0.01597   0.01122  -0.0073   1.0000   0.0044
  -7.750  -0.7791   0.01513   0.01023  -0.0065   1.0000   0.0045
  -7.500  -0.7561   0.01441   0.00941  -0.0057   1.0000   0.0046
  -7.250  -0.7330   0.01373   0.00863  -0.0049   1.0000   0.0048
  -7.000  -0.7097   0.01311   0.00793  -0.0042   1.0000   0.0049
  -6.750  -0.6857   0.01271   0.00747  -0.0035   1.0000   0.0050
  -6.500  -0.6594   0.01222   0.00693  -0.0033   0.9979   0.0051
  -6.250  -0.6285   0.01149   0.00609  -0.0042   0.9893   0.0053
  -6.000  -0.5972   0.01069   0.00516  -0.0051   0.9777   0.0059
  -5.750  -0.5648   0.01023   0.00465  -0.0062   0.9606   0.0064
  -5.500  -0.5353   0.00990   0.00424  -0.0066   0.9363   0.0069
  -5.250  -0.5104   0.00966   0.00389  -0.0058   0.9069   0.0074
  -5.000  -0.4860   0.00946   0.00358  -0.0050   0.8785   0.0079
  -4.750  -0.4609   0.00929   0.00329  -0.0043   0.8517   0.0084
  -4.500  -0.4354   0.00911   0.00296  -0.0037   0.8266   0.0092
  -4.250  -0.4097   0.00892   0.00269  -0.0032   0.8021   0.0117
  -4.000  -0.3835   0.00875   0.00245  -0.0028   0.7788   0.0160
  -3.750  -0.3574   0.00856   0.00223  -0.0025   0.7565   0.0254
  -3.500  -0.3311   0.00838   0.00203  -0.0022   0.7346   0.0379
  -3.250  -0.3045   0.00824   0.00185  -0.0020   0.7141   0.0498
  -3.000  -0.2778   0.00809   0.00170  -0.0017   0.6939   0.0665
  -2.750  -0.2512   0.00792   0.00155  -0.0015   0.6751   0.0900
  -2.250  -0.1981   0.00755   0.00129  -0.0011   0.6381   0.1537
  -2.000  -0.1714   0.00739   0.00117  -0.0010   0.6211   0.1908
  -1.750  -0.1449   0.00717   0.00107  -0.0008   0.6040   0.2388
  -1.500  -0.1182   0.00700   0.00098  -0.0006   0.5880   0.2827
  -1.250  -0.0918   0.00679   0.00090  -0.0005   0.5719   0.3413
  -1.000  -0.0662   0.00645   0.00080  -0.0002   0.5562   0.4319
  -0.750  -0.0403   0.00619   0.00074   0.0001   0.5409   0.5100
  -0.500  -0.0140   0.00601   0.00070   0.0004   0.5256   0.5716
  -0.250   0.0126   0.00589   0.00068   0.0006   0.5111   0.6184
   0.000   0.0391   0.00578   0.00067   0.0008   0.4971   0.6673
   0.250   0.0655   0.00567   0.00067   0.0012   0.4834   0.7171
   0.500   0.0916   0.00558   0.00070   0.0016   0.4699   0.7645
   0.750   0.1182   0.00555   0.00073   0.0020   0.4560   0.7966
   1.000   0.1448   0.00555   0.00076   0.0023   0.4417   0.8251
   1.250   0.1712   0.00556   0.00081   0.0027   0.4274   0.8508
   1.500   0.1978   0.00559   0.00086   0.0031   0.4139   0.8734
   1.750   0.2243   0.00564   0.00092   0.0035   0.4005   0.8917
   2.000   0.2510   0.00570   0.00098   0.0039   0.3866   0.9064
   2.250   0.2778   0.00580   0.00105   0.0042   0.3702   0.9182
   2.500   0.3047   0.00591   0.00112   0.0044   0.3504   0.9282
   2.750   0.3318   0.00605   0.00120   0.0046   0.3305   0.9371
   3.000   0.3595   0.00615   0.00129   0.0047   0.3176   0.9459
   3.250   0.3872   0.00628   0.00138   0.0047   0.3035   0.9550
   3.500   0.4169   0.00640   0.00148   0.0043   0.2903   0.9614
   3.750   0.4455   0.00655   0.00159   0.0041   0.2762   0.9684
   4.000   0.4764   0.00674   0.00173   0.0034   0.2548   0.9728
   4.250   0.5067   0.00697   0.00188   0.0027   0.2293   0.9775
   4.500   0.5351   0.00729   0.00206   0.0024   0.1953   0.9827
   4.750   0.5658   0.00788   0.00234   0.0013   0.1323   0.9855
   5.000   0.5967   0.00832   0.00263   0.0002   0.0954   0.9883
   5.250   0.6272   0.00869   0.00290  -0.0006   0.0708   0.9912
   5.500   0.6565   0.00919   0.00325  -0.0013   0.0402   0.9941
   5.750   0.6878   0.00964   0.00361  -0.0024   0.0207   0.9962
   6.000   0.7189   0.01003   0.00395  -0.0033   0.0116   0.9985
   6.250   0.7484   0.01035   0.00430  -0.0039   0.0093   1.0000
   6.500   0.7709   0.01069   0.00465  -0.0029   0.0078   1.0000
   6.750   0.7935   0.01106   0.00507  -0.0020   0.0070   1.0000
   7.000   0.8167   0.01136   0.00541  -0.0012   0.0067   1.0000
   7.250   0.8399   0.01169   0.00577  -0.0005   0.0061   1.0000
   7.500   0.8631   0.01203   0.00614   0.0003   0.0055   1.0000
   7.750   0.8860   0.01244   0.00660   0.0010   0.0051   1.0000
   8.000   0.9084   0.01297   0.00718   0.0018   0.0045   1.0000
   8.250   0.9302   0.01359   0.00789   0.0027   0.0041   1.0000
   8.500   0.9533   0.01405   0.00841   0.0033   0.0040   1.0000
   8.750   0.9760   0.01456   0.00898   0.0040   0.0038   1.0000
   9.000   0.9985   0.01509   0.00958   0.0047   0.0036   1.0000
   9.250   1.0203   0.01569   0.01025   0.0054   0.0034   1.0000
   9.500   1.0420   0.01631   0.01094   0.0061   0.0032   1.0000
   9.750   1.0632   0.01695   0.01167   0.0069   0.0030   1.0000
  10.000   1.0844   0.01756   0.01234   0.0076   0.0028   1.0000
  10.250   1.1046   0.01827   0.01312   0.0084   0.0027   1.0000
  10.500   1.1237   0.01906   0.01398   0.0094   0.0025   1.0000
  10.750   1.1385   0.02027   0.01532   0.0108   0.0023   1.0000
  11.000   1.1510   0.02162   0.01682   0.0124   0.0022   1.0000
  11.250   1.1585   0.02334   0.01872   0.0145   0.0021   1.0000
  11.500   1.1732   0.02423   0.01971   0.0158   0.0021   1.0000
  11.750   1.1829   0.02544   0.02104   0.0176   0.0021   1.0000
  12.000   1.1867   0.02663   0.02235   0.0202   0.0020   1.0000
  12.250   1.1861   0.02810   0.02395   0.0230   0.0020   1.0000
  12.500   1.1901   0.02943   0.02540   0.0246   0.0020   1.0000
  12.750   1.1850   0.03171   0.02783   0.0260   0.0020   1.0000
  13.000   1.1787   0.03453   0.03081   0.0265   0.0019   1.0000
  13.250   1.1813   0.03674   0.03312   0.0262   0.0019   1.0000
  13.500   1.1763   0.04011   0.03663   0.0253   0.0019   1.0000
  13.750   1.1537   0.04621   0.04297   0.0228   0.0019   1.0000
  14.000   1.1603   0.04866   0.04547   0.0214   0.0018   1.0000
  14.250   1.1466   0.05419   0.05116   0.0185   0.0019   1.0000
  14.500   1.1297   0.06054   0.05766   0.0149   0.0018   1.0000
  14.750   1.1169   0.06650   0.06374   0.0115   0.0019   1.0000
  15.000   1.1004   0.07329   0.07067   0.0076   0.0019   1.0000
  15.250   1.0712   0.08269   0.08023   0.0023   0.0019   1.0000
  15.500   1.0566   0.08984   0.08748  -0.0018   0.0019   1.0000
  15.750   1.0451   0.09666   0.09439  -0.0057   0.0019   1.0000
  16.000   1.0201   0.10658   0.10443  -0.0112   0.0019   1.0000
  16.250   0.9907   0.11804   0.11603  -0.0175   0.0019   1.0000
  16.500   0.9600   0.13047   0.12856  -0.0242   0.0020   1.0000
  16.750   0.9213   0.14591   0.14414  -0.0323   0.0021   1.0000
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