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EPPLER 396 AIRFOIL (e396-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: EPPLER 396 AIRFOIL (e396-il)
Reynolds number: 1,000,000
Max Cl/Cd: 148 at α=5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-e396-il-1000000-n5.txt
Download as CSV file: xf-e396-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: EPPLER 396 AIRFOIL                              
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -13.750  -0.4973   0.07945   0.07710  -0.0905   0.9861   0.0027
 -13.500  -0.5329   0.06905   0.06659  -0.0980   0.9794   0.0026
 -13.250  -0.5816   0.05645   0.05383  -0.1081   0.9622   0.0026
 -12.750  -0.5933   0.02720   0.02375  -0.1551   0.9125   0.0025
 -12.500  -0.5935   0.02379   0.02005  -0.1596   0.8830   0.0026
 -12.250  -0.5862   0.02201   0.01805  -0.1601   0.8662   0.0025
 -12.000  -0.5730   0.02071   0.01657  -0.1601   0.8544   0.0026
 -11.500  -0.5364   0.01883   0.01442  -0.1601   0.8352   0.0028
 -11.250  -0.5162   0.01798   0.01343  -0.1601   0.8270   0.0029
 -11.000  -0.4948   0.01715   0.01248  -0.1601   0.8191   0.0030
 -10.750  -0.4719   0.01650   0.01171  -0.1602   0.8124   0.0031
 -10.500  -0.4485   0.01582   0.01092  -0.1602   0.8054   0.0032
 -10.250  -0.4244   0.01522   0.01019  -0.1603   0.7992   0.0033
 -10.000  -0.3995   0.01466   0.00952  -0.1604   0.7933   0.0034
  -9.750  -0.3742   0.01418   0.00894  -0.1605   0.7874   0.0035
  -9.500  -0.3483   0.01370   0.00837  -0.1606   0.7822   0.0035
  -9.250  -0.3227   0.01312   0.00769  -0.1608   0.7765   0.0038
  -8.750  -0.2696   0.01224   0.00666  -0.1611   0.7668   0.0044
  -8.500  -0.2427   0.01187   0.00620  -0.1613   0.7617   0.0048
  -8.000  -0.1880   0.01122   0.00542  -0.1617   0.7529   0.0058
  -7.750  -0.1604   0.01088   0.00503  -0.1619   0.7482   0.0069
  -7.500  -0.1329   0.01061   0.00470  -0.1620   0.7438   0.0082
  -7.250  -0.1050   0.01030   0.00437  -0.1623   0.7398   0.0105
  -7.000  -0.0770   0.01001   0.00406  -0.1626   0.7356   0.0138
  -6.750  -0.0491   0.00975   0.00378  -0.1628   0.7312   0.0178
  -6.500  -0.0211   0.00954   0.00354  -0.1630   0.7273   0.0218
  -6.250   0.0074   0.00929   0.00331  -0.1633   0.7235   0.0271
  -6.000   0.0357   0.00908   0.00309  -0.1635   0.7193   0.0326
  -5.750   0.0640   0.00892   0.00290  -0.1637   0.7153   0.0377
  -5.500   0.0924   0.00872   0.00271  -0.1640   0.7117   0.0462
  -5.250   0.1211   0.00853   0.00255  -0.1643   0.7078   0.0553
  -5.000   0.1496   0.00840   0.00240  -0.1645   0.7038   0.0624
  -4.750   0.1780   0.00827   0.00226  -0.1647   0.7000   0.0715
  -4.500   0.2068   0.00812   0.00213  -0.1650   0.6966   0.0827
  -4.250   0.2356   0.00800   0.00202  -0.1653   0.6928   0.0924
  -4.000   0.2642   0.00791   0.00192  -0.1655   0.6889   0.1018
  -3.750   0.2926   0.00782   0.00182  -0.1657   0.6852   0.1139
  -3.500   0.3215   0.00771   0.00174  -0.1660   0.6818   0.1257
  -3.250   0.3503   0.00762   0.00167  -0.1663   0.6779   0.1397
  -3.000   0.3789   0.00754   0.00161  -0.1665   0.6740   0.1549
  -2.500   0.4362   0.00741   0.00151  -0.1669   0.6666   0.1820
  -2.250   0.4650   0.00734   0.00148  -0.1672   0.6625   0.1981
  -2.000   0.4934   0.00730   0.00145  -0.1674   0.6584   0.2122
  -1.750   0.5219   0.00727   0.00143  -0.1675   0.6546   0.2279
  -1.500   0.5507   0.00722   0.00141  -0.1678   0.6505   0.2413
  -1.250   0.5792   0.00719   0.00140  -0.1680   0.6460   0.2570
  -1.000   0.6073   0.00719   0.00141  -0.1681   0.6418   0.2721
  -0.750   0.6360   0.00715   0.00141  -0.1683   0.6377   0.2881
  -0.500   0.6645   0.00714   0.00142  -0.1685   0.6331   0.3034
  -0.250   0.6925   0.00714   0.00144  -0.1686   0.6284   0.3202
   0.000   0.7209   0.00712   0.00147  -0.1688   0.6240   0.3380
   0.250   0.7493   0.00712   0.00150  -0.1690   0.6190   0.3558
   0.500   0.7771   0.00714   0.00154  -0.1690   0.6139   0.3734
   0.750   0.8053   0.00714   0.00158  -0.1692   0.6089   0.3923
   1.000   0.8333   0.00715   0.00164  -0.1693   0.6031   0.4116
   1.250   0.8608   0.00718   0.00169  -0.1693   0.5975   0.4321
   1.500   0.8888   0.00720   0.00175  -0.1694   0.5913   0.4536
   1.750   0.9161   0.00724   0.00183  -0.1694   0.5847   0.4756
   2.250   0.9709   0.00732   0.00200  -0.1694   0.5707   0.5242
   2.500   0.9981   0.00736   0.00210  -0.1693   0.5625   0.5489
   2.750   1.0245   0.00745   0.00220  -0.1691   0.5531   0.5748
   3.000   1.0511   0.00752   0.00232  -0.1690   0.5431   0.6022
   3.250   1.0777   0.00760   0.00244  -0.1688   0.5339   0.6306
   3.500   1.1036   0.00770   0.00259  -0.1686   0.5238   0.6602
   3.750   1.1289   0.00782   0.00274  -0.1682   0.5116   0.6905
   4.250   1.1795   0.00805   0.00308  -0.1674   0.4874   0.7598
   4.500   1.2038   0.00817   0.00327  -0.1668   0.4754   0.7999
   4.750   1.2264   0.00830   0.00347  -0.1658   0.4616   0.8477
   5.000   1.2432   0.00840   0.00365  -0.1635   0.4455   0.9208
   5.250   1.2642   0.00861   0.00385  -0.1622   0.4272   1.0000
   5.500   1.2863   0.00893   0.00409  -0.1613   0.4088   1.0000
   5.750   1.3081   0.00926   0.00434  -0.1603   0.3898   1.0000
   6.000   1.3282   0.00966   0.00464  -0.1590   0.3681   1.0000
   6.250   1.3459   0.01015   0.00499  -0.1573   0.3404   1.0000
   6.500   1.3608   0.01070   0.00540  -0.1550   0.3108   1.0000
   6.750   1.3748   0.01122   0.00580  -0.1526   0.2856   1.0000
   7.000   1.3860   0.01184   0.00628  -0.1497   0.2570   1.0000
   7.250   1.3982   0.01244   0.00676  -0.1471   0.2333   1.0000
   7.500   1.4099   0.01307   0.00728  -0.1444   0.2107   1.0000
   7.750   1.4193   0.01382   0.00789  -0.1414   0.1844   1.0000
   8.000   1.4299   0.01454   0.00852  -0.1387   0.1633   1.0000
   8.250   1.4396   0.01533   0.00920  -0.1360   0.1432   1.0000
   8.500   1.4501   0.01609   0.00989  -0.1335   0.1273   1.0000
   8.750   1.4601   0.01692   0.01065  -0.1310   0.1111   1.0000
   9.000   1.4679   0.01791   0.01155  -0.1282   0.0933   1.0000
   9.250   1.4778   0.01882   0.01242  -0.1259   0.0811   1.0000
   9.500   1.4875   0.01978   0.01334  -0.1237   0.0701   1.0000
   9.750   1.4966   0.02084   0.01436  -0.1215   0.0595   1.0000
  10.000   1.5050   0.02197   0.01545  -0.1193   0.0496   1.0000
  10.250   1.5126   0.02321   0.01665  -0.1172   0.0402   1.0000
  10.500   1.5200   0.02451   0.01792  -0.1151   0.0320   1.0000
  10.750   1.5282   0.02581   0.01921  -0.1133   0.0260   1.0000
  11.000   1.5372   0.02709   0.02049  -0.1116   0.0214   1.0000
  11.250   1.5451   0.02850   0.02190  -0.1099   0.0172   1.0000
  11.500   1.5532   0.02993   0.02333  -0.1083   0.0142   1.0000
  11.750   1.5622   0.03133   0.02476  -0.1069   0.0120   1.0000
  12.000   1.5697   0.03289   0.02635  -0.1054   0.0097   1.0000
  12.250   1.5788   0.03436   0.02786  -0.1041   0.0087   1.0000
  12.500   1.5862   0.03602   0.02955  -0.1028   0.0070   1.0000
  12.750   1.5939   0.03768   0.03125  -0.1016   0.0060   1.0000
  13.000   1.6020   0.03936   0.03298  -0.1005   0.0053   1.0000
  13.250   1.6092   0.04118   0.03484  -0.0995   0.0047   1.0000
  13.500   1.6158   0.04308   0.03679  -0.0985   0.0041   1.0000
  13.750   1.6230   0.04497   0.03874  -0.0976   0.0037   1.0000
  14.000   1.6294   0.04699   0.04082  -0.0967   0.0032   1.0000
  14.250   1.6352   0.04912   0.04301  -0.0959   0.0029   1.0000
  14.500   1.6402   0.05140   0.04535  -0.0952   0.0025   1.0000
  14.750   1.6458   0.05365   0.04767  -0.0946   0.0023   1.0000
  15.000   1.6506   0.05604   0.05012  -0.0940   0.0021   1.0000
  15.250   1.6550   0.05852   0.05267  -0.0936   0.0019   1.0000
  15.500   1.6584   0.06119   0.05542  -0.0932   0.0017   1.0000
  15.750   1.6611   0.06401   0.05831  -0.0929   0.0016   1.0000
  16.000   1.6635   0.06691   0.06129  -0.0927   0.0014   1.0000
  16.250   1.6663   0.06982   0.06428  -0.0926   0.0014   1.0000
  16.500   1.6682   0.07292   0.06746  -0.0926   0.0013   1.0000
  16.750   1.6697   0.07612   0.07075  -0.0927   0.0012   1.0000
  17.000   1.6706   0.07946   0.07419  -0.0930   0.0012   1.0000
  17.250   1.6710   0.08292   0.07773  -0.0933   0.0011   1.0000
  17.500   1.6704   0.08660   0.08150  -0.0938   0.0011   1.0000
  17.750   1.6691   0.09043   0.08543  -0.0944   0.0010   1.0000
  18.000   1.6672   0.09442   0.08951  -0.0952   0.0010   1.0000
  18.250   1.6649   0.09853   0.09372  -0.0961   0.0009   1.0000
  18.500   1.6618   0.10282   0.09810  -0.0972   0.0009   1.0000
  18.750   1.6582   0.10722   0.10261  -0.0984   0.0008   1.0000
  19.000   1.6538   0.11183   0.10731  -0.0998   0.0008   1.0000
  19.250   1.6489   0.11656   0.11215  -0.1014   0.0008   1.0000
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