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E214 (11.1%) (e214-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: E214 (11.1%) (e214-il)
Reynolds number: 1,000,000
Max Cl/Cd: 122.24 at α=3.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-e214-il-1000000-n5.txt
Download as CSV file: xf-e214-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: E214  (11.1%)                                   
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -13.500  -0.4021   0.14812   0.14639  -0.0285   0.9999   0.0037
 -13.250  -0.3926   0.14485   0.14311  -0.0306   0.9995   0.0038
 -12.250  -0.7410   0.03214   0.02970  -0.1130   0.9850   0.0053
 -12.000  -0.7277   0.02860   0.02590  -0.1178   0.9814   0.0054
 -11.750  -0.7147   0.02571   0.02276  -0.1202   0.9765   0.0056
 -11.500  -0.6873   0.02454   0.02150  -0.1222   0.9745   0.0058
 -11.250  -0.6579   0.02351   0.02039  -0.1243   0.9731   0.0060
 -11.000  -0.6274   0.02260   0.01940  -0.1263   0.9720   0.0062
 -10.750  -0.6094   0.02184   0.01855  -0.1255   0.9668   0.0063
 -10.500  -0.5840   0.02086   0.01747  -0.1264   0.9638   0.0065
 -10.250  -0.5558   0.02006   0.01658  -0.1276   0.9619   0.0068
 -10.000  -0.5275   0.01902   0.01538  -0.1289   0.9604   0.0071
  -9.750  -0.4981   0.01801   0.01423  -0.1304   0.9592   0.0074
  -9.500  -0.4785   0.01718   0.01328  -0.1295   0.9537   0.0076
  -9.250  -0.4510   0.01640   0.01238  -0.1302   0.9506   0.0078
  -9.000  -0.4205   0.01563   0.01148  -0.1315   0.9487   0.0080
  -8.750  -0.3880   0.01478   0.01050  -0.1333   0.9471   0.0082
  -8.500  -0.3558   0.01410   0.00975  -0.1349   0.9449   0.0087
  -8.250  -0.3283   0.01373   0.00934  -0.1352   0.9401   0.0090
  -8.000  -0.2960   0.01339   0.00896  -0.1365   0.9368   0.0093
  -7.750  -0.2622   0.01287   0.00835  -0.1381   0.9338   0.0097
  -7.500  -0.2312   0.01235   0.00775  -0.1392   0.9294   0.0101
  -7.250  -0.2011   0.01185   0.00716  -0.1400   0.9238   0.0105
  -7.000  -0.1687   0.01140   0.00661  -0.1413   0.9189   0.0109
  -6.750  -0.1399   0.01108   0.00623  -0.1417   0.9124   0.0113
  -6.500  -0.1095   0.01082   0.00590  -0.1424   0.9057   0.0115
  -6.250  -0.0811   0.01051   0.00551  -0.1427   0.8984   0.0117
  -6.000  -0.0531   0.00983   0.00470  -0.1431   0.8904   0.0121
  -5.750  -0.0260   0.00934   0.00414  -0.1431   0.8815   0.0126
  -5.500   0.0019   0.00903   0.00376  -0.1433   0.8724   0.0130
  -5.250   0.0295   0.00879   0.00344  -0.1433   0.8620   0.0135
  -5.000   0.0568   0.00859   0.00318  -0.1433   0.8509   0.0141
  -4.750   0.0840   0.00840   0.00292  -0.1432   0.8386   0.0147
  -4.500   0.1109   0.00824   0.00266  -0.1430   0.8251   0.0152
  -4.250   0.1376   0.00810   0.00244  -0.1428   0.8106   0.0157
  -4.000   0.1642   0.00800   0.00224  -0.1426   0.7957   0.0160
  -3.750   0.1906   0.00791   0.00207  -0.1423   0.7805   0.0163
  -3.500   0.2170   0.00782   0.00188  -0.1420   0.7658   0.0168
  -3.250   0.2435   0.00774   0.00171  -0.1417   0.7514   0.0179
  -3.000   0.2702   0.00768   0.00158  -0.1414   0.7378   0.0195
  -2.750   0.2969   0.00763   0.00148  -0.1412   0.7251   0.0221
  -2.500   0.3237   0.00749   0.00138  -0.1411   0.7130   0.0440
  -2.250   0.3506   0.00739   0.00130  -0.1410   0.7013   0.0695
  -2.000   0.3776   0.00726   0.00124  -0.1409   0.6898   0.1072
  -1.750   0.4048   0.00715   0.00119  -0.1409   0.6787   0.1428
  -1.500   0.4320   0.00703   0.00116  -0.1409   0.6681   0.1897
  -1.250   0.4592   0.00691   0.00113  -0.1409   0.6575   0.2430
  -1.000   0.4866   0.00667   0.00112  -0.1411   0.6469   0.3348
  -0.750   0.5140   0.00640   0.00114  -0.1413   0.6366   0.4545
  -0.500   0.5412   0.00638   0.00119  -0.1412   0.6265   0.5034
   0.000   0.5956   0.00646   0.00125  -0.1410   0.6061   0.5404
   0.250   0.6227   0.00651   0.00130  -0.1408   0.5962   0.5547
   0.500   0.6496   0.00658   0.00134  -0.1406   0.5858   0.5685
   0.750   0.6767   0.00664   0.00139  -0.1405   0.5752   0.5818
   1.000   0.7037   0.00671   0.00145  -0.1403   0.5645   0.5937
   1.250   0.7304   0.00679   0.00151  -0.1401   0.5526   0.6060
   1.500   0.7569   0.00689   0.00159  -0.1398   0.5404   0.6184
   1.750   0.7833   0.00699   0.00167  -0.1396   0.5277   0.6315
   2.000   0.8098   0.00708   0.00176  -0.1393   0.5149   0.6453
   2.250   0.8362   0.00718   0.00185  -0.1391   0.5021   0.6578
   2.500   0.8624   0.00731   0.00195  -0.1388   0.4883   0.6688
   2.750   0.8884   0.00744   0.00206  -0.1385   0.4735   0.6802
   3.000   0.9139   0.00760   0.00219  -0.1380   0.4567   0.6920
   3.250   0.9393   0.00777   0.00232  -0.1376   0.4387   0.7043
   3.500   0.9647   0.00794   0.00246  -0.1372   0.4215   0.7181
   3.750   0.9901   0.00810   0.00262  -0.1368   0.4056   0.7335
   4.000   1.0149   0.00831   0.00279  -0.1363   0.3866   0.7498
   4.250   1.0391   0.00854   0.00298  -0.1356   0.3652   0.7682
   4.500   1.0624   0.00882   0.00320  -0.1348   0.3391   0.7904
   4.750   1.0858   0.00905   0.00344  -0.1341   0.3166   0.8174
   5.000   1.1080   0.00931   0.00368  -0.1330   0.2943   0.8507
   5.250   1.1267   0.00954   0.00393  -0.1312   0.2699   0.9033
   5.500   1.1464   0.00978   0.00414  -0.1296   0.2451   1.0000
   5.750   1.1680   0.01025   0.00447  -0.1286   0.2157   1.0000
   6.000   1.1885   0.01078   0.00483  -0.1274   0.1844   1.0000
   6.250   1.2102   0.01121   0.00516  -0.1264   0.1617   1.0000
   6.500   1.2311   0.01168   0.00552  -0.1253   0.1402   1.0000
   6.750   1.2505   0.01224   0.00593  -0.1240   0.1143   1.0000
   7.000   1.2692   0.01282   0.00638  -0.1225   0.0902   1.0000
   7.250   1.2893   0.01329   0.00678  -0.1212   0.0753   1.0000
   7.500   1.3086   0.01375   0.00718  -0.1198   0.0629   1.0000
   7.750   1.3268   0.01421   0.00759  -0.1182   0.0525   1.0000
   8.000   1.3441   0.01470   0.00803  -0.1164   0.0428   1.0000
   8.250   1.3603   0.01523   0.00851  -0.1145   0.0330   1.0000
   8.500   1.3767   0.01576   0.00901  -0.1126   0.0259   1.0000
   8.750   1.3935   0.01626   0.00950  -0.1108   0.0210   1.0000
   9.000   1.4097   0.01678   0.01002  -0.1089   0.0170   1.0000
   9.250   1.4246   0.01740   0.01062  -0.1069   0.0122   1.0000
   9.500   1.4386   0.01806   0.01127  -0.1048   0.0082   1.0000
   9.750   1.4523   0.01874   0.01196  -0.1026   0.0057   1.0000
  10.000   1.4661   0.01942   0.01268  -0.1006   0.0045   1.0000
  10.250   1.4806   0.02006   0.01337  -0.0987   0.0041   1.0000
  10.500   1.4943   0.02075   0.01411  -0.0967   0.0037   1.0000
  10.750   1.5069   0.02153   0.01494  -0.0946   0.0034   1.0000
  11.000   1.5189   0.02236   0.01582  -0.0926   0.0032   1.0000
  11.250   1.5293   0.02331   0.01684  -0.0903   0.0029   1.0000
  11.500   1.5402   0.02425   0.01784  -0.0883   0.0028   1.0000
  11.750   1.5516   0.02517   0.01883  -0.0865   0.0027   1.0000
  12.000   1.5619   0.02621   0.01995  -0.0845   0.0026   1.0000
  12.250   1.5717   0.02730   0.02110  -0.0827   0.0024   1.0000
  12.500   1.5802   0.02853   0.02241  -0.0808   0.0023   1.0000
  12.750   1.5883   0.02984   0.02379  -0.0790   0.0023   1.0000
  13.000   1.5953   0.03126   0.02530  -0.0772   0.0022   1.0000
  13.250   1.6018   0.03280   0.02692  -0.0755   0.0021   1.0000
  13.500   1.6074   0.03447   0.02867  -0.0740   0.0021   1.0000
  13.750   1.6123   0.03626   0.03055  -0.0725   0.0020   1.0000
  14.000   1.6162   0.03822   0.03260  -0.0711   0.0020   1.0000
  14.250   1.6188   0.04039   0.03487  -0.0699   0.0019   1.0000
  14.500   1.6208   0.04271   0.03729  -0.0688   0.0018   1.0000
  14.750   1.6214   0.04530   0.03998  -0.0679   0.0018   1.0000
  15.000   1.6209   0.04812   0.04291  -0.0672   0.0018   1.0000
  15.250   1.6189   0.05124   0.04614  -0.0667   0.0017   1.0000
  15.500   1.6157   0.05463   0.04965  -0.0665   0.0017   1.0000
  15.750   1.6103   0.05848   0.05362  -0.0665   0.0016   1.0000
  16.000   1.6056   0.06239   0.05765  -0.0668   0.0016   1.0000
  16.250   1.5956   0.06720   0.06261  -0.0675   0.0016   1.0000
  16.500   1.5860   0.07219   0.06774  -0.0685   0.0016   1.0000
  16.750   1.5786   0.07703   0.07271  -0.0697   0.0015   1.0000
  17.000   1.5720   0.08189   0.07769  -0.0712   0.0015   1.0000
  17.250   1.5639   0.08713   0.08305  -0.0729   0.0015   1.0000
  17.500   1.5552   0.09265   0.08870  -0.0749   0.0015   1.0000
  17.750   1.5453   0.09855   0.09472  -0.0773   0.0015   1.0000
  18.000   1.5338   0.10488   0.10119  -0.0800   0.0015   1.0000
  18.250   1.5221   0.11139   0.10783  -0.0830   0.0015   1.0000
  18.500   1.5100   0.11812   0.11469  -0.0863   0.0015   1.0000
  18.750   1.4971   0.12517   0.12188  -0.0899   0.0015   1.0000
  19.000   1.4834   0.13246   0.12931  -0.0939   0.0015   1.0000
  19.250   1.4701   0.13981   0.13678  -0.0980   0.0015   1.0000
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