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EH 0.0/9.0 (eh0009-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: EH 0.0/9.0 (eh0009-il)
Reynolds number: 1,000,000
Max Cl/Cd: 67.61 at α=7°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-eh0009-il-1000000-n5.txt
Download as CSV file: xf-eh0009-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: EH 0.0/9.0                                      
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -14.750  -0.9105   0.10675   0.10498   0.0108   1.0000   0.0016
 -14.500  -0.9505   0.09327   0.09141   0.0037   1.0000   0.0016
 -14.250  -0.9806   0.08214   0.08020  -0.0024   1.0000   0.0015
 -14.000  -1.0317   0.06627   0.06412  -0.0124   1.0000   0.0015
 -13.750  -1.0475   0.05847   0.05620  -0.0179   1.0000   0.0015
 -13.500  -1.0717   0.04997   0.04751  -0.0242   1.0000   0.0015
 -13.250  -1.0894   0.04398   0.04134  -0.0279   1.0000   0.0015
 -13.000  -1.1030   0.03963   0.03682  -0.0296   1.0000   0.0015
 -12.750  -1.1204   0.03574   0.03273  -0.0294   1.0000   0.0015
 -12.500  -1.1296   0.03320   0.03003  -0.0278   1.0000   0.0015
 -12.250  -1.1385   0.03104   0.02769  -0.0248   1.0000   0.0015
 -12.000  -1.1443   0.02914   0.02561  -0.0213   1.0000   0.0015
 -11.750  -1.1402   0.02733   0.02361  -0.0192   1.0000   0.0015
 -11.500  -1.1319   0.02570   0.02179  -0.0173   1.0000   0.0015
 -11.250  -1.1212   0.02412   0.02002  -0.0156   1.0000   0.0016
 -11.000  -1.1076   0.02274   0.01847  -0.0141   1.0000   0.0016
 -10.750  -1.0923   0.02147   0.01701  -0.0128   1.0000   0.0017
 -10.500  -1.0754   0.02032   0.01570  -0.0116   1.0000   0.0017
 -10.250  -1.0568   0.01933   0.01458  -0.0106   1.0000   0.0017
 -10.000  -1.0358   0.01861   0.01377  -0.0098   1.0000   0.0018
  -9.750  -1.0158   0.01773   0.01276  -0.0089   1.0000   0.0018
  -9.500  -0.9982   0.01642   0.01127  -0.0075   1.0000   0.0021
  -9.250  -0.9770   0.01562   0.01038  -0.0067   1.0000   0.0022
  -9.000  -0.9541   0.01509   0.00981  -0.0061   1.0000   0.0026
  -8.750  -0.9312   0.01454   0.00920  -0.0054   1.0000   0.0028
  -8.500  -0.9081   0.01400   0.00856  -0.0048   1.0000   0.0030
  -8.250  -0.8847   0.01353   0.00804  -0.0041   1.0000   0.0033
  -8.000  -0.8611   0.01308   0.00752  -0.0035   1.0000   0.0036
  -7.750  -0.8372   0.01269   0.00709  -0.0029   1.0000   0.0038
  -7.500  -0.8141   0.01218   0.00651  -0.0021   1.0000   0.0042
  -7.250  -0.7910   0.01172   0.00601  -0.0013   1.0000   0.0048
  -7.000  -0.7676   0.01135   0.00562  -0.0006   1.0000   0.0053
  -6.750  -0.7442   0.01101   0.00526   0.0002   1.0000   0.0060
  -6.500  -0.7206   0.01073   0.00495   0.0010   1.0000   0.0066
  -6.250  -0.6976   0.01038   0.00455   0.0019   1.0000   0.0078
  -6.000  -0.6661   0.01001   0.00419   0.0009   0.9970   0.0099
  -5.750  -0.6334   0.00974   0.00390  -0.0004   0.9936   0.0115
  -5.500  -0.6030   0.00939   0.00356  -0.0011   0.9893   0.0158
  -5.250  -0.5710   0.00913   0.00329  -0.0021   0.9849   0.0188
  -5.000  -0.5388   0.00885   0.00302  -0.0032   0.9798   0.0249
  -4.750  -0.5076   0.00855   0.00275  -0.0040   0.9715   0.0359
  -4.500  -0.4768   0.00825   0.00251  -0.0048   0.9611   0.0518
  -4.250  -0.4479   0.00789   0.00227  -0.0051   0.9479   0.0805
  -4.000  -0.4208   0.00762   0.00206  -0.0050   0.9323   0.1051
  -3.750  -0.3951   0.00738   0.00188  -0.0045   0.9149   0.1308
  -3.500  -0.3700   0.00712   0.00169  -0.0040   0.8971   0.1645
  -3.250  -0.3442   0.00694   0.00154  -0.0036   0.8793   0.1893
  -3.000  -0.3188   0.00670   0.00139  -0.0031   0.8610   0.2291
  -2.750  -0.2929   0.00653   0.00127  -0.0027   0.8421   0.2609
  -2.500  -0.2668   0.00638   0.00114  -0.0024   0.8220   0.2937
  -2.250  -0.2407   0.00621   0.00104  -0.0020   0.8019   0.3314
  -2.000  -0.2142   0.00610   0.00096  -0.0017   0.7811   0.3620
  -1.500  -0.1610   0.00590   0.00082  -0.0012   0.7392   0.4221
  -1.250  -0.1343   0.00583   0.00076  -0.0010   0.7162   0.4514
  -1.000  -0.1075   0.00578   0.00071  -0.0008   0.6920   0.4800
  -0.750  -0.0807   0.00574   0.00068  -0.0006   0.6671   0.5079
  -0.500  -0.0538   0.00571   0.00066  -0.0004   0.6423   0.5356
  -0.250  -0.0269   0.00568   0.00064  -0.0002   0.6175   0.5643
   0.000   0.0000   0.00567   0.00063   0.0000   0.5921   0.5922
   0.250   0.0268   0.00568   0.00064   0.0002   0.5643   0.6176
   0.500   0.0537   0.00571   0.00066   0.0004   0.5356   0.6422
   0.750   0.0806   0.00574   0.00068   0.0006   0.5074   0.6672
   1.000   0.1075   0.00578   0.00071   0.0008   0.4801   0.6919
   1.250   0.1342   0.00583   0.00076   0.0010   0.4516   0.7160
   1.500   0.1609   0.00590   0.00082   0.0013   0.4219   0.7390
   2.000   0.2141   0.00610   0.00096   0.0018   0.3619   0.7811
   2.250   0.2406   0.00622   0.00104   0.0020   0.3310   0.8020
   2.500   0.2667   0.00638   0.00114   0.0024   0.2936   0.8221
   2.750   0.2928   0.00653   0.00127   0.0027   0.2610   0.8422
   3.000   0.3187   0.00670   0.00139   0.0031   0.2301   0.8611
   3.250   0.3441   0.00694   0.00154   0.0036   0.1898   0.8794
   3.500   0.3699   0.00712   0.00168   0.0040   0.1652   0.8973
   3.750   0.3951   0.00738   0.00188   0.0046   0.1307   0.9150
   4.000   0.4208   0.00762   0.00206   0.0050   0.1050   0.9323
   4.250   0.4479   0.00788   0.00226   0.0051   0.0815   0.9480
   4.500   0.4769   0.00825   0.00251   0.0048   0.0522   0.9612
   4.750   0.5078   0.00855   0.00275   0.0040   0.0359   0.9716
   5.000   0.5390   0.00885   0.00302   0.0031   0.0249   0.9799
   5.250   0.5712   0.00913   0.00329   0.0020   0.0188   0.9850
   5.500   0.6033   0.00939   0.00356   0.0010   0.0157   0.9894
   6.000   0.6665   0.01001   0.00419  -0.0010   0.0099   0.9972
   6.250   0.6972   0.01039   0.00455  -0.0018   0.0077   1.0000
   6.500   0.7202   0.01074   0.00496  -0.0009   0.0066   1.0000
   6.750   0.7439   0.01102   0.00527  -0.0001   0.0060   1.0000
   7.000   0.7674   0.01135   0.00562   0.0006   0.0054   1.0000
   7.250   0.7909   0.01172   0.00602   0.0013   0.0048   1.0000
   7.500   0.8141   0.01218   0.00651   0.0021   0.0042   1.0000
   7.750   0.8373   0.01268   0.00707   0.0029   0.0038   1.0000
   8.000   0.8610   0.01310   0.00755   0.0035   0.0036   1.0000
   8.250   0.8846   0.01355   0.00806   0.0041   0.0033   1.0000
   8.500   0.9082   0.01402   0.00859   0.0047   0.0030   1.0000
   8.750   0.9313   0.01456   0.00922   0.0054   0.0028   1.0000
   9.000   0.9545   0.01506   0.00977   0.0060   0.0025   1.0000
   9.250   0.9771   0.01565   0.01041   0.0067   0.0023   1.0000
   9.500   0.9987   0.01639   0.01124   0.0075   0.0021   1.0000
   9.750   1.0160   0.01774   0.01278   0.0088   0.0018   1.0000
  10.000   1.0368   0.01851   0.01366   0.0096   0.0018   1.0000
  10.250   1.0569   0.01935   0.01461   0.0105   0.0018   1.0000
  10.500   1.0757   0.02033   0.01571   0.0115   0.0017   1.0000
  10.750   1.0926   0.02149   0.01703   0.0127   0.0017   1.0000
  11.000   1.1085   0.02269   0.01841   0.0140   0.0016   1.0000
  11.250   1.1221   0.02408   0.01998   0.0155   0.0016   1.0000
  11.500   1.1330   0.02564   0.02172   0.0171   0.0016   1.0000
  11.750   1.1407   0.02736   0.02364   0.0191   0.0015   1.0000
  12.000   1.1447   0.02919   0.02566   0.0212   0.0015   1.0000
  12.250   1.1396   0.03105   0.02770   0.0247   0.0015   1.0000
  12.500   1.1314   0.03315   0.02997   0.0275   0.0015   1.0000
  12.750   1.1204   0.03584   0.03284   0.0293   0.0015   1.0000
  13.000   1.1058   0.03944   0.03663   0.0294   0.0015   1.0000
  13.250   1.0921   0.04378   0.04113   0.0279   0.0015   1.0000
  13.500   1.0682   0.05078   0.04835   0.0234   0.0015   1.0000
  13.750   1.0508   0.05810   0.05582   0.0180   0.0015   1.0000
  14.000   1.0258   0.06791   0.06579   0.0110   0.0015   1.0000
  14.250   0.9884   0.08080   0.07884   0.0029   0.0015   1.0000
  14.500   0.9508   0.09361   0.09175  -0.0042   0.0016   1.0000
  14.750   0.9117   0.10691   0.10514  -0.0111   0.0016   1.0000
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