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E216 (10.4%) (e216-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: E216 (10.4%) (e216-il)
Reynolds number: 1,000,000
Max Cl/Cd: 127.41 at α=2.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-e216-il-1000000-n5.txt
Download as CSV file: xf-e216-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: E216  (10.4%)                                   
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -10.000  -0.2998   0.06818   0.06633  -0.0997   0.9767   0.0055
  -9.750  -0.4042   0.02967   0.02722  -0.1434   0.9560   0.0050
  -9.500  -0.3707   0.02444   0.02156  -0.1550   0.9544   0.0052
  -9.250  -0.3524   0.02183   0.01869  -0.1574   0.9487   0.0053
  -9.000  -0.3228   0.01990   0.01652  -0.1605   0.9465   0.0054
  -8.750  -0.2913   0.01822   0.01462  -0.1633   0.9450   0.0055
  -8.500  -0.2589   0.01680   0.01301  -0.1659   0.9439   0.0056
  -8.250  -0.2262   0.01585   0.01190  -0.1679   0.9429   0.0057
  -8.000  -0.1926   0.01492   0.01084  -0.1700   0.9420   0.0058
  -7.750  -0.1640   0.01408   0.00987  -0.1709   0.9390   0.0058
  -7.500  -0.1346   0.01297   0.00861  -0.1722   0.9355   0.0060
  -7.250  -0.1019   0.01210   0.00762  -0.1740   0.9332   0.0062
  -7.000  -0.0674   0.01139   0.00683  -0.1759   0.9315   0.0063
  -6.750  -0.0316   0.01082   0.00618  -0.1780   0.9301   0.0065
  -6.500   0.0055   0.01029   0.00559  -0.1803   0.9288   0.0067
  -6.250   0.0375   0.00990   0.00514  -0.1814   0.9253   0.0070
  -6.000   0.0699   0.00951   0.00470  -0.1826   0.9213   0.0074
  -5.750   0.1063   0.00910   0.00422  -0.1847   0.9183   0.0077
  -5.500   0.1454   0.00870   0.00376  -0.1873   0.9158   0.0080
  -5.250   0.1846   0.00838   0.00338  -0.1899   0.9130   0.0083
  -5.000   0.2187   0.00802   0.00296  -0.1915   0.9073   0.0088
  -4.750   0.2587   0.00774   0.00263  -0.1943   0.9026   0.0094
  -4.500   0.2967   0.00753   0.00237  -0.1966   0.8971   0.0102
  -4.250   0.3309   0.00737   0.00214  -0.1980   0.8891   0.0110
  -4.000   0.3652   0.00720   0.00193  -0.1994   0.8811   0.0129
  -3.750   0.3984   0.00701   0.00174  -0.2007   0.8717   0.0229
  -3.500   0.4296   0.00681   0.00158  -0.2015   0.8614   0.0458
  -3.250   0.4605   0.00665   0.00146  -0.2023   0.8504   0.0718
  -3.000   0.4900   0.00655   0.00137  -0.2027   0.8383   0.0951
  -2.750   0.5189   0.00645   0.00130  -0.2030   0.8251   0.1276
  -2.500   0.5470   0.00637   0.00126  -0.2031   0.8114   0.1590
  -2.250   0.5747   0.00632   0.00123  -0.2031   0.7975   0.1894
  -2.000   0.6020   0.00630   0.00121  -0.2030   0.7831   0.2183
  -1.750   0.6290   0.00629   0.00122  -0.2029   0.7682   0.2500
  -1.500   0.6555   0.00632   0.00123  -0.2026   0.7527   0.2726
  -1.250   0.6816   0.00638   0.00125  -0.2022   0.7364   0.2945
  -1.000   0.7075   0.00645   0.00128  -0.2018   0.7195   0.3139
  -0.750   0.7334   0.00652   0.00132  -0.2013   0.7021   0.3358
  -0.500   0.7593   0.00660   0.00138  -0.2009   0.6843   0.3582
  -0.250   0.7853   0.00669   0.00144  -0.2005   0.6663   0.3803
   0.000   0.8112   0.00680   0.00151  -0.2001   0.6483   0.4019
   0.250   0.8369   0.00691   0.00159  -0.1996   0.6302   0.4223
   0.500   0.8628   0.00704   0.00168  -0.1992   0.6124   0.4422
   0.750   0.8885   0.00717   0.00178  -0.1988   0.5945   0.4622
   1.000   0.9145   0.00730   0.00188  -0.1984   0.5764   0.4825
   1.250   0.9403   0.00745   0.00199  -0.1980   0.5573   0.5037
   1.500   0.9657   0.00763   0.00212  -0.1975   0.5361   0.5238
   1.750   0.9910   0.00782   0.00226  -0.1970   0.5154   0.5442
   2.000   1.0167   0.00799   0.00241  -0.1966   0.4956   0.5653
   2.250   1.0422   0.00818   0.00256  -0.1962   0.4759   0.5858
   2.500   1.0677   0.00838   0.00272  -0.1957   0.4569   0.6059
   2.750   1.0929   0.00859   0.00290  -0.1952   0.4373   0.6268
   3.000   1.1180   0.00881   0.00308  -0.1947   0.4163   0.6477
   3.250   1.1425   0.00909   0.00329  -0.1941   0.3932   0.6678
   3.500   1.1673   0.00933   0.00349  -0.1936   0.3723   0.6886
   3.750   1.1919   0.00958   0.00372  -0.1930   0.3525   0.7098
   4.000   1.2161   0.00987   0.00395  -0.1923   0.3317   0.7312
   4.250   1.2402   0.01014   0.00420  -0.1916   0.3117   0.7534
   4.500   1.2641   0.01043   0.00445  -0.1909   0.2922   0.7760
   4.750   1.2866   0.01081   0.00476  -0.1899   0.2662   0.7994
   5.000   1.3074   0.01130   0.00512  -0.1886   0.2320   0.8233
   5.250   1.3268   0.01187   0.00553  -0.1871   0.1956   0.8481
   5.500   1.3472   0.01226   0.00588  -0.1857   0.1729   0.8756
   5.750   1.3655   0.01260   0.00619  -0.1838   0.1550   0.9097
   6.000   1.3794   0.01288   0.00646  -0.1809   0.1379   1.0000
   6.250   1.3998   0.01337   0.00684  -0.1796   0.1181   1.0000
   6.500   1.4187   0.01395   0.00730  -0.1780   0.0967   1.0000
   6.750   1.4382   0.01446   0.00773  -0.1766   0.0811   1.0000
   7.000   1.4575   0.01497   0.00817  -0.1751   0.0679   1.0000
   7.250   1.4760   0.01554   0.00866  -0.1734   0.0546   1.0000
   7.500   1.4935   0.01618   0.00922  -0.1716   0.0407   1.0000
   7.750   1.5112   0.01677   0.00976  -0.1699   0.0311   1.0000
   8.000   1.5274   0.01747   0.01039  -0.1679   0.0210   1.0000
   8.250   1.5423   0.01827   0.01113  -0.1657   0.0110   1.0000
   8.500   1.5599   0.01886   0.01174  -0.1640   0.0090   1.0000
   8.750   1.5768   0.01947   0.01238  -0.1621   0.0078   1.0000
   9.000   1.5944   0.02003   0.01298  -0.1605   0.0073   1.0000
   9.250   1.6116   0.02063   0.01362  -0.1588   0.0070   1.0000
   9.500   1.6277   0.02129   0.01432  -0.1569   0.0066   1.0000
   9.750   1.6432   0.02199   0.01508  -0.1550   0.0063   1.0000
  10.000   1.6579   0.02277   0.01590  -0.1530   0.0060   1.0000
  10.250   1.6714   0.02363   0.01682  -0.1508   0.0058   1.0000
  10.500   1.6844   0.02454   0.01779  -0.1487   0.0056   1.0000
  10.750   1.6979   0.02540   0.01871  -0.1466   0.0055   1.0000
  11.000   1.7108   0.02631   0.01970  -0.1446   0.0054   1.0000
  11.250   1.7229   0.02731   0.02076  -0.1425   0.0053   1.0000
  11.500   1.7342   0.02837   0.02190  -0.1404   0.0052   1.0000
  11.750   1.7448   0.02952   0.02311  -0.1382   0.0051   1.0000
  12.000   1.7544   0.03076   0.02443  -0.1361   0.0050   1.0000
  12.250   1.7633   0.03209   0.02584  -0.1339   0.0049   1.0000
  12.500   1.7716   0.03350   0.02733  -0.1318   0.0048   1.0000
  12.750   1.7794   0.03498   0.02889  -0.1298   0.0046   1.0000
  13.000   1.7865   0.03656   0.03055  -0.1278   0.0045   1.0000
  13.250   1.7922   0.03832   0.03240  -0.1258   0.0044   1.0000
  13.500   1.7970   0.04023   0.03439  -0.1239   0.0043   1.0000
  13.750   1.8001   0.04236   0.03661  -0.1221   0.0042   1.0000
  14.000   1.8023   0.04468   0.03903  -0.1203   0.0042   1.0000
  14.250   1.8027   0.04730   0.04176  -0.1187   0.0041   1.0000
  14.500   1.8016   0.05019   0.04476  -0.1173   0.0040   1.0000
  14.750   1.7980   0.05351   0.04820  -0.1160   0.0040   1.0000
  15.000   1.7910   0.05742   0.05225  -0.1149   0.0039   1.0000
  15.250   1.7874   0.06108   0.05604  -0.1143   0.0038   1.0000
  15.500   1.7870   0.06443   0.05950  -0.1140   0.0038   1.0000
  15.750   1.7826   0.06847   0.06366  -0.1139   0.0038   1.0000
  16.000   1.7782   0.07265   0.06796  -0.1140   0.0038   1.0000
  16.250   1.7732   0.07710   0.07254  -0.1145   0.0037   1.0000
  16.500   1.7654   0.08216   0.07773  -0.1154   0.0037   1.0000
  16.750   1.7576   0.08737   0.08308  -0.1165   0.0037   1.0000
  17.000   1.7490   0.09285   0.08869  -0.1180   0.0037   1.0000
  17.250   1.7398   0.09861   0.09458  -0.1197   0.0036   1.0000
  17.500   1.7278   0.10503   0.10114  -0.1220   0.0037   1.0000
  17.750   1.7178   0.11122   0.10746  -0.1244   0.0036   1.0000
  18.000   1.7057   0.11787   0.11425  -0.1273   0.0036   1.0000
  18.250   1.6944   0.12450   0.12101  -0.1303   0.0036   1.0000
  18.500   1.6835   0.13113   0.12778  -0.1336   0.0035   1.0000
  18.750   1.6706   0.13827   0.13505  -0.1373   0.0035   1.0000
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