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E212 (10.55%) (e212-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: E212 (10.55%) (e212-il)
Reynolds number: 1,000,000
Max Cl/Cd: 100.98 at α=3.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-e212-il-1000000-n5.txt
Download as CSV file: xf-e212-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: E212  (10.55%)                                  
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -13.250  -0.7060   0.08252   0.08040  -0.0439   1.0000   0.0054
 -13.000  -0.7308   0.07415   0.07194  -0.0482   1.0000   0.0054
 -12.750  -0.7627   0.06514   0.06284  -0.0531   1.0000   0.0054
 -12.500  -0.7862   0.05776   0.05536  -0.0572   1.0000   0.0054
 -12.250  -0.8116   0.05039   0.04786  -0.0615   1.0000   0.0054
 -12.000  -0.8438   0.04296   0.04028  -0.0656   1.0000   0.0053
 -11.750  -0.8460   0.03637   0.03348  -0.0749   0.9975   0.0053
 -11.500  -0.8277   0.03220   0.02910  -0.0838   0.9947   0.0054
 -11.250  -0.8098   0.02958   0.02629  -0.0876   0.9917   0.0054
 -11.000  -0.7923   0.02641   0.02286  -0.0912   0.9889   0.0055
 -10.750  -0.7695   0.02399   0.02021  -0.0940   0.9871   0.0055
 -10.500  -0.7439   0.02194   0.01796  -0.0965   0.9859   0.0056
 -10.250  -0.7155   0.02051   0.01638  -0.0986   0.9850   0.0057
 -10.000  -0.6940   0.01938   0.01514  -0.0987   0.9822   0.0058
  -9.750  -0.6686   0.01842   0.01409  -0.0993   0.9797   0.0059
  -9.500  -0.6406   0.01747   0.01304  -0.1004   0.9779   0.0060
  -9.250  -0.6110   0.01666   0.01215  -0.1016   0.9765   0.0061
  -9.000  -0.5806   0.01583   0.01121  -0.1030   0.9753   0.0062
  -8.750  -0.5496   0.01505   0.01035  -0.1044   0.9744   0.0063
  -8.500  -0.5177   0.01438   0.00960  -0.1059   0.9736   0.0065
  -8.250  -0.4949   0.01384   0.00901  -0.1052   0.9697   0.0067
  -8.000  -0.4670   0.01328   0.00838  -0.1056   0.9669   0.0069
  -7.750  -0.4368   0.01269   0.00772  -0.1065   0.9650   0.0071
  -7.500  -0.4054   0.01213   0.00710  -0.1077   0.9634   0.0074
  -7.250  -0.3731   0.01161   0.00651  -0.1089   0.9621   0.0075
  -7.000  -0.3402   0.01115   0.00599  -0.1102   0.9609   0.0077
  -6.750  -0.3184   0.01077   0.00558  -0.1091   0.9545   0.0078
  -6.500  -0.2881   0.01024   0.00498  -0.1098   0.9517   0.0081
  -6.250  -0.2555   0.00973   0.00442  -0.1111   0.9496   0.0085
  -6.000  -0.2207   0.00934   0.00400  -0.1128   0.9480   0.0088
  -5.750  -0.1931   0.00904   0.00367  -0.1128   0.9422   0.0092
  -5.500  -0.1584   0.00874   0.00333  -0.1143   0.9387   0.0097
  -5.250  -0.1215   0.00846   0.00301  -0.1164   0.9355   0.0102
  -5.000  -0.0876   0.00823   0.00275  -0.1177   0.9301   0.0108
  -4.750  -0.0527   0.00796   0.00245  -0.1193   0.9235   0.0124
  -4.500  -0.0184   0.00774   0.00220  -0.1207   0.9159   0.0146
  -4.250   0.0149   0.00736   0.00190  -0.1220   0.9062   0.0403
  -4.000   0.0457   0.00708   0.00170  -0.1228   0.8943   0.0649
  -3.750   0.0757   0.00686   0.00152  -0.1233   0.8811   0.0917
  -3.500   0.1048   0.00666   0.00138  -0.1237   0.8669   0.1221
  -3.250   0.1330   0.00649   0.00126  -0.1238   0.8517   0.1554
  -3.000   0.1608   0.00637   0.00117  -0.1238   0.8361   0.1840
  -2.750   0.1883   0.00629   0.00109  -0.1237   0.8201   0.2086
  -2.500   0.2154   0.00616   0.00103  -0.1237   0.8033   0.2489
  -2.250   0.2425   0.00609   0.00098  -0.1235   0.7863   0.2798
  -2.000   0.2694   0.00608   0.00095  -0.1232   0.7681   0.3003
  -1.750   0.2962   0.00609   0.00093  -0.1230   0.7492   0.3182
  -1.500   0.3230   0.00611   0.00092  -0.1227   0.7297   0.3375
  -1.250   0.3496   0.00614   0.00091  -0.1224   0.7103   0.3579
  -1.000   0.3765   0.00617   0.00092  -0.1222   0.6908   0.3775
  -0.750   0.4033   0.00621   0.00093  -0.1219   0.6708   0.3967
  -0.500   0.4301   0.00626   0.00096  -0.1217   0.6511   0.4157
  -0.250   0.4570   0.00632   0.00099  -0.1214   0.6316   0.4349
   0.000   0.4839   0.00639   0.00102  -0.1212   0.6114   0.4536
   0.250   0.5107   0.00647   0.00107  -0.1209   0.5906   0.4720
   0.500   0.5375   0.00656   0.00113  -0.1207   0.5700   0.4900
   0.750   0.5643   0.00666   0.00119  -0.1205   0.5477   0.5080
   1.000   0.5909   0.00677   0.00127  -0.1202   0.5259   0.5257
   1.250   0.6177   0.00688   0.00135  -0.1200   0.5037   0.5448
   1.500   0.6442   0.00703   0.00144  -0.1197   0.4805   0.5634
   1.750   0.6710   0.00715   0.00154  -0.1195   0.4583   0.5824
   2.000   0.6974   0.00731   0.00165  -0.1192   0.4360   0.6009
   2.250   0.7240   0.00745   0.00177  -0.1190   0.4132   0.6197
   2.500   0.7502   0.00764   0.00191  -0.1186   0.3890   0.6387
   2.750   0.7764   0.00783   0.00205  -0.1183   0.3636   0.6571
   3.000   0.8025   0.00803   0.00220  -0.1180   0.3402   0.6754
   3.250   0.8284   0.00824   0.00237  -0.1176   0.3165   0.6935
   3.500   0.8543   0.00846   0.00255  -0.1173   0.2930   0.7117
   3.750   0.8792   0.00876   0.00276  -0.1168   0.2607   0.7302
   4.000   0.9032   0.00916   0.00301  -0.1161   0.2218   0.7488
   4.250   0.9272   0.00954   0.00328  -0.1155   0.1864   0.7677
   4.500   0.9515   0.00989   0.00355  -0.1148   0.1582   0.7867
   4.750   0.9755   0.01026   0.00383  -0.1141   0.1313   0.8061
   5.000   0.9993   0.01061   0.00412  -0.1134   0.1080   0.8261
   5.250   1.0227   0.01099   0.00444  -0.1126   0.0870   0.8465
   5.500   1.0458   0.01131   0.00474  -0.1117   0.0697   0.8683
   5.750   1.0672   0.01172   0.00509  -0.1105   0.0504   0.8930
   6.000   1.0870   0.01204   0.00541  -0.1088   0.0372   0.9244
   6.250   1.1070   0.01236   0.00572  -0.1072   0.0256   1.0000
   6.500   1.1290   0.01300   0.00625  -0.1063   0.0099   1.0000
   6.750   1.1535   0.01337   0.00662  -0.1057   0.0083   1.0000
   7.000   1.1777   0.01375   0.00702  -0.1051   0.0074   1.0000
   7.250   1.2015   0.01416   0.00746  -0.1044   0.0067   1.0000
   7.500   1.2254   0.01453   0.00786  -0.1037   0.0065   1.0000
   7.750   1.2490   0.01492   0.00828  -0.1030   0.0063   1.0000
   8.000   1.2721   0.01535   0.00874  -0.1023   0.0060   1.0000
   8.250   1.2948   0.01579   0.00923  -0.1014   0.0058   1.0000
   8.500   1.3170   0.01627   0.00974  -0.1005   0.0056   1.0000
   8.750   1.3387   0.01677   0.01028  -0.0995   0.0054   1.0000
   9.000   1.3596   0.01732   0.01087  -0.0984   0.0052   1.0000
   9.250   1.3797   0.01791   0.01151  -0.0972   0.0051   1.0000
   9.500   1.3985   0.01859   0.01225  -0.0958   0.0049   1.0000
   9.750   1.4151   0.01943   0.01316  -0.0940   0.0047   1.0000
  10.000   1.4321   0.02014   0.01394  -0.0923   0.0046   1.0000
  10.250   1.4486   0.02073   0.01458  -0.0905   0.0045   1.0000
  10.500   1.4636   0.02136   0.01528  -0.0885   0.0044   1.0000
  10.750   1.4777   0.02205   0.01603  -0.0863   0.0043   1.0000
  11.000   1.4905   0.02280   0.01685  -0.0841   0.0043   1.0000
  11.250   1.5023   0.02363   0.01776  -0.0817   0.0042   1.0000
  11.500   1.5130   0.02453   0.01874  -0.0793   0.0041   1.0000
  11.750   1.5228   0.02551   0.01980  -0.0769   0.0040   1.0000
  12.000   1.5315   0.02658   0.02096  -0.0744   0.0040   1.0000
  12.250   1.5392   0.02774   0.02220  -0.0720   0.0039   1.0000
  12.500   1.5460   0.02901   0.02357  -0.0697   0.0038   1.0000
  12.750   1.5519   0.03039   0.02504  -0.0674   0.0038   1.0000
  13.000   1.5566   0.03191   0.02667  -0.0652   0.0037   1.0000
  13.250   1.5600   0.03361   0.02847  -0.0631   0.0037   1.0000
  13.500   1.5629   0.03546   0.03041  -0.0613   0.0036   1.0000
  13.750   1.5643   0.03752   0.03258  -0.0596   0.0036   1.0000
  14.000   1.5654   0.03973   0.03489  -0.0582   0.0036   1.0000
  14.250   1.5643   0.04230   0.03758  -0.0571   0.0035   1.0000
  14.500   1.5630   0.04504   0.04043  -0.0563   0.0035   1.0000
  14.750   1.5601   0.04815   0.04366  -0.0558   0.0035   1.0000
  15.000   1.5558   0.05161   0.04724  -0.0557   0.0034   1.0000
  15.250   1.5508   0.05539   0.05114  -0.0560   0.0034   1.0000
  15.500   1.5440   0.05965   0.05553  -0.0568   0.0034   1.0000
  15.750   1.5355   0.06444   0.06045  -0.0581   0.0034   1.0000
  16.000   1.5261   0.06963   0.06577  -0.0598   0.0034   1.0000
  16.250   1.5155   0.07529   0.07157  -0.0620   0.0033   1.0000
  16.500   1.5027   0.08165   0.07807  -0.0648   0.0033   1.0000
  16.750   1.4886   0.08850   0.08507  -0.0681   0.0033   1.0000
  17.000   1.4732   0.09587   0.09259  -0.0718   0.0033   1.0000
  17.250   1.4572   0.10364   0.10050  -0.0758   0.0033   1.0000
  17.500   1.4410   0.11163   0.10863  -0.0802   0.0033   1.0000
  17.750   1.4234   0.12011   0.11725  -0.0849   0.0033   1.0000
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