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EH 2.0/10 (eh2010-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: EH 2.0/10 (eh2010-il)
Reynolds number: 1,000,000
Max Cl/Cd: 94.92 at α=6.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-eh2010-il-1000000-n5.txt
Download as CSV file: xf-eh2010-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: EH 2.0/10                                       
  
 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  -1.0393   0.03795   0.03565  -0.0266   1.0000   0.0033
 -12.000  -1.0461   0.03437   0.03180  -0.0244   1.0000   0.0034
 -11.750  -1.0445   0.03156   0.02874  -0.0224   1.0000   0.0034
 -11.500  -1.0378   0.02922   0.02618  -0.0207   1.0000   0.0035
 -11.250  -1.0280   0.02712   0.02383  -0.0191   1.0000   0.0035
 -11.000  -1.0120   0.02578   0.02233  -0.0179   1.0000   0.0036
 -10.750  -0.9968   0.02425   0.02061  -0.0166   1.0000   0.0036
 -10.500  -0.9789   0.02303   0.01924  -0.0155   1.0000   0.0036
 -10.250  -0.9601   0.02188   0.01793  -0.0145   1.0000   0.0037
 -10.000  -0.9463   0.01984   0.01562  -0.0128   1.0000   0.0039
  -9.750  -0.9267   0.01869   0.01430  -0.0118   1.0000   0.0041
  -9.500  -0.9051   0.01783   0.01335  -0.0110   1.0000   0.0043
  -9.250  -0.8822   0.01719   0.01264  -0.0103   1.0000   0.0045
  -9.000  -0.8585   0.01670   0.01209  -0.0097   1.0000   0.0047
  -8.750  -0.8353   0.01608   0.01138  -0.0090   1.0000   0.0049
  -8.500  -0.8117   0.01553   0.01076  -0.0084   1.0000   0.0052
  -8.250  -0.7883   0.01494   0.01009  -0.0077   1.0000   0.0053
  -8.000  -0.7553   0.01427   0.00932  -0.0091   0.9768   0.0056
  -7.750  -0.7200   0.01365   0.00856  -0.0108   0.9340   0.0057
  -7.500  -0.6976   0.01331   0.00802  -0.0096   0.8843   0.0059
  -7.250  -0.6749   0.01295   0.00745  -0.0085   0.8456   0.0060
  -7.000  -0.6511   0.01262   0.00693  -0.0077   0.8136   0.0061
  -6.750  -0.6275   0.01208   0.00621  -0.0068   0.7855   0.0064
  -6.500  -0.6028   0.01168   0.00567  -0.0062   0.7602   0.0069
  -6.250  -0.5774   0.01138   0.00527  -0.0057   0.7381   0.0075
  -6.000  -0.5516   0.01114   0.00494  -0.0053   0.7175   0.0082
  -5.750  -0.5256   0.01090   0.00460  -0.0049   0.6990   0.0088
  -5.500  -0.4993   0.01067   0.00427  -0.0045   0.6812   0.0093
  -5.250  -0.4734   0.01037   0.00389  -0.0041   0.6646   0.0107
  -5.000  -0.4470   0.01016   0.00362  -0.0038   0.6488   0.0123
  -4.750  -0.4204   0.00999   0.00338  -0.0036   0.6340   0.0136
  -4.500  -0.3935   0.00984   0.00315  -0.0033   0.6202   0.0146
  -4.250  -0.3670   0.00963   0.00289  -0.0030   0.6067   0.0170
  -4.000  -0.3401   0.00946   0.00268  -0.0028   0.5940   0.0191
  -3.750  -0.3131   0.00933   0.00248  -0.0026   0.5815   0.0209
  -3.500  -0.2862   0.00917   0.00229  -0.0024   0.5700   0.0251
  -3.250  -0.2593   0.00902   0.00212  -0.0022   0.5583   0.0316
  -3.000  -0.2323   0.00888   0.00197  -0.0020   0.5469   0.0403
  -2.750  -0.2052   0.00874   0.00183  -0.0018   0.5363   0.0497
  -2.500  -0.1779   0.00864   0.00171  -0.0016   0.5262   0.0582
  -2.250  -0.1506   0.00854   0.00159  -0.0015   0.5162   0.0668
  -2.000  -0.1233   0.00844   0.00149  -0.0014   0.5058   0.0788
  -1.750  -0.0960   0.00834   0.00140  -0.0012   0.4963   0.0925
  -1.500  -0.0689   0.00822   0.00131  -0.0011   0.4867   0.1150
  -1.250  -0.0420   0.00806   0.00124  -0.0009   0.4772   0.1510
  -1.000  -0.0151   0.00790   0.00117  -0.0008   0.4685   0.1889
  -0.750   0.0117   0.00774   0.00110  -0.0006   0.4596   0.2317
  -0.500   0.0381   0.00752   0.00104  -0.0004   0.4508   0.2950
  -0.250   0.0624   0.00703   0.00095   0.0000   0.4428   0.4319
   0.000   0.0837   0.00631   0.00087   0.0011   0.4344   0.6351
   0.250   0.1073   0.00597   0.00087   0.0020   0.4268   0.7442
   0.500   0.1326   0.00587   0.00090   0.0027   0.4184   0.7994
   0.750   0.1591   0.00583   0.00093   0.0031   0.4102   0.8304
   1.000   0.1858   0.00584   0.00097   0.0035   0.4027   0.8548
   1.250   0.2123   0.00585   0.00102   0.0039   0.3941   0.8764
   1.500   0.2386   0.00588   0.00107   0.0044   0.3868   0.8987
   1.750   0.2651   0.00594   0.00113   0.0049   0.3784   0.9137
   2.000   0.2927   0.00599   0.00117   0.0050   0.3707   0.9204
   2.500   0.3482   0.00614   0.00127   0.0051   0.3549   0.9319
   2.750   0.3759   0.00622   0.00133   0.0052   0.3475   0.9379
   3.000   0.4038   0.00631   0.00139   0.0052   0.3393   0.9432
   3.250   0.4321   0.00640   0.00147   0.0051   0.3319   0.9486
   3.500   0.4596   0.00650   0.00154   0.0052   0.3235   0.9543
   3.750   0.4891   0.00660   0.00164   0.0048   0.3157   0.9584
   4.000   0.5183   0.00672   0.00173   0.0045   0.3076   0.9630
   4.250   0.5464   0.00682   0.00182   0.0044   0.2992   0.9681
   4.500   0.5772   0.00695   0.00193   0.0037   0.2910   0.9711
   4.750   0.6081   0.00709   0.00206   0.0029   0.2815   0.9741
   5.000   0.6382   0.00722   0.00218   0.0024   0.2725   0.9775
   5.250   0.6668   0.00737   0.00232   0.0021   0.2637   0.9815
   5.500   0.6983   0.00755   0.00247   0.0011   0.2530   0.9835
   5.750   0.7299   0.00778   0.00265   0.0001   0.2336   0.9852
   6.000   0.7610   0.00806   0.00285  -0.0009   0.2138   0.9871
   6.250   0.7916   0.00834   0.00306  -0.0018   0.1961   0.9893
   6.500   0.8205   0.00879   0.00337  -0.0024   0.1631   0.9919
   6.750   0.8487   0.00936   0.00375  -0.0031   0.1265   0.9943
   7.000   0.8773   0.01015   0.00430  -0.0040   0.0806   0.9964
   7.250   0.9054   0.01096   0.00489  -0.0048   0.0423   0.9987
   7.500   0.9317   0.01156   0.00539  -0.0051   0.0232   1.0000
   7.750   0.9521   0.01197   0.00578  -0.0039   0.0167   1.0000
   8.000   0.9731   0.01235   0.00616  -0.0029   0.0127   1.0000
   8.250   0.9940   0.01276   0.00659  -0.0018   0.0091   1.0000
   8.500   1.0148   0.01320   0.00703  -0.0008   0.0065   1.0000
   8.750   1.0355   0.01366   0.00750   0.0003   0.0048   1.0000
   9.000   1.0567   0.01409   0.00796   0.0012   0.0041   1.0000
   9.250   1.0779   0.01452   0.00844   0.0021   0.0036   1.0000
   9.500   1.0988   0.01501   0.00896   0.0030   0.0031   1.0000
   9.750   1.1192   0.01553   0.00953   0.0039   0.0028   1.0000
  10.000   1.1383   0.01618   0.01024   0.0050   0.0025   1.0000
  10.250   1.1576   0.01678   0.01092   0.0060   0.0024   1.0000
  10.500   1.1769   0.01735   0.01155   0.0070   0.0023   1.0000
  10.750   1.1951   0.01799   0.01226   0.0081   0.0023   1.0000
  11.000   1.2120   0.01869   0.01303   0.0093   0.0022   1.0000
  11.250   1.2285   0.01937   0.01377   0.0105   0.0020   1.0000
  11.500   1.2417   0.02021   0.01470   0.0121   0.0020   1.0000
  11.750   1.2544   0.02100   0.01556   0.0138   0.0019   1.0000
  12.000   1.2607   0.02186   0.01650   0.0164   0.0019   1.0000
  12.250   1.2649   0.02285   0.01756   0.0190   0.0018   1.0000
  12.500   1.2685   0.02402   0.01884   0.0211   0.0018   1.0000
  12.750   1.2702   0.02556   0.02047   0.0227   0.0017   1.0000
  13.000   1.2737   0.02720   0.02220   0.0235   0.0016   1.0000
  13.250   1.2764   0.02916   0.02424   0.0239   0.0016   1.0000
  13.500   1.2750   0.03175   0.02695   0.0239   0.0016   1.0000
  13.750   1.2726   0.03469   0.03001   0.0234   0.0017   1.0000
  14.000   1.2724   0.03755   0.03296   0.0227   0.0016   1.0000
  14.250   1.2653   0.04135   0.03689   0.0216   0.0016   1.0000
  14.500   1.2635   0.04458   0.04019   0.0206   0.0015   1.0000
  14.750   1.2571   0.04847   0.04419   0.0193   0.0015   1.0000
  15.000   1.2488   0.05268   0.04852   0.0178   0.0015   1.0000
  15.250   1.2363   0.05756   0.05349   0.0159   0.0013   1.0000
  15.500   1.2296   0.06171   0.05776   0.0143   0.0014   1.0000
  15.750   1.2183   0.06671   0.06285   0.0122   0.0014   1.0000
  16.000   1.1916   0.07425   0.07054   0.0089   0.0013   1.0000
  16.250   1.1879   0.07849   0.07487   0.0070   0.0013   1.0000
  16.500   1.1807   0.08335   0.07982   0.0048   0.0013   1.0000
  16.750   1.1602   0.09063   0.08723   0.0013   0.0013   1.0000
  17.000   1.1557   0.09531   0.09198  -0.0009   0.0013   1.0000
  17.250   1.1456   0.10105   0.09783  -0.0037   0.0013   1.0000
  17.500   1.1355   0.10697   0.10385  -0.0066   0.0013   1.0000
  17.750   1.1223   0.11359   0.11057  -0.0100   0.0013   1.0000
  18.000   1.1095   0.12030   0.11738  -0.0135   0.0013   1.0000
  18.250   1.1039   0.12572   0.12288  -0.0163   0.0014   1.0000
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