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EH 2.0/12 (eh2012-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: EH 2.0/12 (eh2012-il)
Reynolds number: 1,000,000
Max Cl/Cd: 106.54 at α=7.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-eh2012-il-1000000.txt
Download as CSV file: xf-eh2012-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: EH 2.0/12                                       
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -13.750  -0.9234   0.05695   0.05473  -0.0336   1.0000   0.0075
 -13.500  -0.9537   0.04816   0.04572  -0.0403   1.0000   0.0074
 -13.250  -0.9752   0.04293   0.04030  -0.0423   1.0000   0.0075
 -13.000  -0.9953   0.03884   0.03602  -0.0420   1.0000   0.0074
 -12.750  -1.0090   0.03587   0.03287  -0.0404   1.0000   0.0074
 -12.500  -1.0132   0.03393   0.03079  -0.0382   1.0000   0.0076
 -12.250  -1.0220   0.03178   0.02848  -0.0350   1.0000   0.0075
 -12.000  -1.0278   0.02996   0.02648  -0.0312   1.0000   0.0076
 -11.750  -1.0243   0.02859   0.02496  -0.0284   1.0000   0.0078
 -11.500  -1.0137   0.02742   0.02366  -0.0264   1.0000   0.0079
 -11.250  -1.0027   0.02614   0.02223  -0.0245   1.0000   0.0080
 -11.000  -0.9873   0.02521   0.02119  -0.0229   1.0000   0.0081
 -10.750  -0.9701   0.02441   0.02027  -0.0216   1.0000   0.0082
 -10.500  -0.9652   0.02191   0.01749  -0.0188   1.0000   0.0084
 -10.250  -0.9548   0.02002   0.01541  -0.0166   1.0000   0.0087
 -10.000  -0.9371   0.01903   0.01433  -0.0152   1.0000   0.0090
  -9.750  -0.9174   0.01825   0.01347  -0.0140   1.0000   0.0092
  -9.500  -0.8968   0.01756   0.01272  -0.0129   1.0000   0.0094
  -9.250  -0.8761   0.01688   0.01196  -0.0118   1.0000   0.0096
  -9.000  -0.8550   0.01625   0.01127  -0.0107   1.0000   0.0099
  -8.750  -0.8340   0.01563   0.01057  -0.0095   1.0000   0.0102
  -8.500  -0.8133   0.01503   0.00990  -0.0083   1.0000   0.0105
  -8.250  -0.7926   0.01449   0.00931  -0.0069   1.0000   0.0108
  -8.000  -0.7668   0.01400   0.00876  -0.0067   0.9974   0.0110
  -7.750  -0.7320   0.01317   0.00784  -0.0084   0.9864   0.0115
  -7.500  -0.6961   0.01236   0.00697  -0.0104   0.9706   0.0126
  -7.250  -0.6622   0.01192   0.00647  -0.0118   0.9424   0.0135
  -7.000  -0.6377   0.01167   0.00610  -0.0109   0.9052   0.0144
  -6.750  -0.6151   0.01141   0.00569  -0.0097   0.8720   0.0153
  -6.500  -0.5925   0.01101   0.00519  -0.0085   0.8431   0.0174
  -6.250  -0.5680   0.01080   0.00487  -0.0077   0.8176   0.0190
  -6.000  -0.5437   0.01049   0.00445  -0.0069   0.7940   0.0218
  -5.750  -0.5184   0.01028   0.00418  -0.0064   0.7722   0.0249
  -5.500  -0.4933   0.01002   0.00386  -0.0058   0.7520   0.0297
  -5.250  -0.4673   0.00987   0.00364  -0.0053   0.7331   0.0335
  -5.000  -0.4417   0.00964   0.00338  -0.0049   0.7159   0.0402
  -4.750  -0.4155   0.00948   0.00317  -0.0045   0.6993   0.0464
  -4.500  -0.3890   0.00934   0.00300  -0.0042   0.6834   0.0524
  -4.250  -0.3627   0.00916   0.00281  -0.0038   0.6687   0.0608
  -4.000  -0.3360   0.00904   0.00264  -0.0035   0.6543   0.0678
  -3.750  -0.3094   0.00890   0.00248  -0.0032   0.6405   0.0771
  -3.250  -0.2560   0.00861   0.00219  -0.0027   0.6144   0.1022
  -3.000  -0.2292   0.00846   0.00206  -0.0024   0.6021   0.1181
  -2.750  -0.2026   0.00830   0.00194  -0.0022   0.5906   0.1391
  -2.500  -0.1761   0.00815   0.00182  -0.0019   0.5795   0.1647
  -2.250  -0.1499   0.00794   0.00171  -0.0016   0.5685   0.2010
  -2.000  -0.1241   0.00767   0.00159  -0.0012   0.5580   0.2543
  -1.750  -0.0997   0.00729   0.00147  -0.0007   0.5480   0.3393
  -1.500  -0.0782   0.00664   0.00131   0.0003   0.5384   0.4913
  -1.250  -0.0565   0.00610   0.00122   0.0014   0.5291   0.6269
  -1.000  -0.0324   0.00586   0.00119   0.0023   0.5197   0.7042
  -0.750  -0.0067   0.00575   0.00119   0.0029   0.5102   0.7501
  -0.500   0.0201   0.00572   0.00119   0.0033   0.5013   0.7792
  -0.250   0.0469   0.00572   0.00120   0.0037   0.4921   0.8033
   0.250   0.1017   0.00575   0.00123   0.0042   0.4747   0.8365
   0.500   0.1292   0.00579   0.00126   0.0044   0.4659   0.8503
   0.750   0.1564   0.00582   0.00129   0.0047   0.4580   0.8641
   1.000   0.1831   0.00587   0.00134   0.0051   0.4495   0.8803
   1.250   0.2097   0.00592   0.00140   0.0056   0.4416   0.8952
   1.750   0.2616   0.00606   0.00155   0.0069   0.4261   0.9214
   2.000   0.2885   0.00614   0.00159   0.0072   0.4180   0.9285
   2.250   0.3161   0.00620   0.00164   0.0074   0.4104   0.9339
   2.500   0.3428   0.00629   0.00169   0.0077   0.4027   0.9402
   2.750   0.3709   0.00635   0.00175   0.0078   0.3949   0.9449
   3.000   0.3982   0.00645   0.00182   0.0080   0.3874   0.9504
   3.250   0.4249   0.00653   0.00188   0.0083   0.3797   0.9562
   3.500   0.4545   0.00663   0.00196   0.0079   0.3723   0.9601
   3.750   0.4837   0.00674   0.00204   0.0077   0.3643   0.9645
   4.000   0.5107   0.00684   0.00213   0.0079   0.3572   0.9700
   4.250   0.5436   0.00695   0.00223   0.0068   0.3495   0.9722
   4.500   0.5768   0.00708   0.00233   0.0056   0.3417   0.9744
   4.750   0.6099   0.00721   0.00244   0.0043   0.3335   0.9768
   5.000   0.6424   0.00733   0.00255   0.0033   0.3258   0.9793
   5.250   0.6720   0.00749   0.00268   0.0028   0.3173   0.9829
   5.500   0.7075   0.00761   0.00279   0.0010   0.3094   0.9837
   5.750   0.7423   0.00777   0.00293  -0.0006   0.3011   0.9848
   6.000   0.7768   0.00790   0.00306  -0.0022   0.2925   0.9861
   6.250   0.8107   0.00806   0.00321  -0.0037   0.2841   0.9877
   6.500   0.8437   0.00824   0.00337  -0.0050   0.2748   0.9896
   6.750   0.8762   0.00839   0.00352  -0.0062   0.2655   0.9917
   7.000   0.9072   0.00861   0.00370  -0.0071   0.2524   0.9939
   7.250   0.9409   0.00884   0.00389  -0.0087   0.2369   0.9952
   7.500   0.9738   0.00914   0.00411  -0.0101   0.2189   0.9967
   7.750   1.0063   0.00945   0.00436  -0.0115   0.2008   0.9984
   8.000   1.0386   0.00977   0.00462  -0.0129   0.1849   0.9998
   8.250   1.0587   0.01010   0.00490  -0.0117   0.1700   1.0000
   8.500   1.0762   0.01048   0.00522  -0.0100   0.1532   1.0000
   8.750   1.0924   0.01096   0.00560  -0.0081   0.1339   1.0000
   9.000   1.1076   0.01153   0.00605  -0.0061   0.1113   1.0000
   9.250   1.1218   0.01219   0.00657  -0.0040   0.0878   1.0000
   9.500   1.1337   0.01304   0.00726  -0.0017   0.0614   1.0000
   9.750   1.1439   0.01403   0.00807   0.0009   0.0346   1.0000
  10.000   1.1549   0.01497   0.00891   0.0033   0.0196   1.0000
  10.250   1.1701   0.01563   0.00956   0.0051   0.0153   1.0000
  10.500   1.1855   0.01628   0.01024   0.0068   0.0130   1.0000
  10.750   1.2019   0.01684   0.01085   0.0083   0.0119   1.0000
  11.000   1.2159   0.01752   0.01156   0.0101   0.0109   1.0000
  11.250   1.2248   0.01845   0.01258   0.0126   0.0098   1.0000
  11.500   1.2363   0.01902   0.01321   0.0148   0.0096   1.0000
  11.750   1.2436   0.01970   0.01395   0.0175   0.0091   1.0000
  12.000   1.2501   0.02053   0.01484   0.0200   0.0087   1.0000
  12.250   1.2557   0.02153   0.01591   0.0221   0.0084   1.0000
  12.500   1.2601   0.02276   0.01720   0.0239   0.0081   1.0000
  12.750   1.2631   0.02427   0.01878   0.0253   0.0078   1.0000
  13.000   1.2634   0.02621   0.02081   0.0263   0.0076   1.0000
  13.250   1.2494   0.02977   0.02453   0.0268   0.0071   1.0000
  13.500   1.2544   0.03177   0.02660   0.0268   0.0070   1.0000
  13.750   1.2582   0.03399   0.02892   0.0266   0.0068   1.0000
  14.000   1.2595   0.03657   0.03158   0.0262   0.0067   1.0000
  14.250   1.2584   0.03950   0.03460   0.0256   0.0065   1.0000
  14.500   1.2558   0.04265   0.03783   0.0249   0.0064   1.0000
  14.750   1.2529   0.04591   0.04118   0.0241   0.0061   1.0000
  15.000   1.2390   0.05056   0.04596   0.0228   0.0063   1.0000
  15.250   1.2357   0.05399   0.04946   0.0218   0.0062   1.0000
  15.500   1.2317   0.05754   0.05308   0.0207   0.0058   1.0000
  15.750   1.2207   0.06216   0.05782   0.0191   0.0059   1.0000
  16.000   1.2154   0.06616   0.06188   0.0177   0.0057   1.0000
  16.250   1.2062   0.07075   0.06656   0.0160   0.0057   1.0000
  16.500   1.1940   0.07594   0.07185   0.0140   0.0056   1.0000
  16.750   1.1856   0.08064   0.07663   0.0121   0.0056   1.0000
  17.000   1.1756   0.08569   0.08177   0.0101   0.0055   1.0000
  17.250   1.1687   0.09037   0.08652   0.0081   0.0055   1.0000
  17.500   1.1566   0.09592   0.09216   0.0057   0.0054   1.0000
  17.750   1.1496   0.10076   0.09708   0.0036   0.0054   1.0000
  18.000   1.1371   0.10656   0.10295   0.0010   0.0052   1.0000
  18.250   1.1287   0.11174   0.10821  -0.0014   0.0051   1.0000
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