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EPPLER 562 AIRFOIL (e562-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: EPPLER 562 AIRFOIL (e562-il)
Reynolds number: 1,000,000
Max Cl/Cd: 129.42 at α=7°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-e562-il-1000000.txt
Download as CSV file: xf-e562-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: EPPLER 562 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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -18.000  -0.7070   0.13516   0.13289  -0.0342   1.0000   0.0087
 -17.750  -0.7290   0.12668   0.12429  -0.0383   1.0000   0.0087
 -17.500  -0.7468   0.11933   0.11684  -0.0418   1.0000   0.0087
 -17.250  -0.7595   0.11320   0.11063  -0.0447   1.0000   0.0088
 -17.000  -0.7731   0.10710   0.10444  -0.0476   1.0000   0.0087
 -16.750  -0.7811   0.10203   0.09931  -0.0500   1.0000   0.0088
 -16.500  -0.7918   0.09669   0.09389  -0.0524   1.0000   0.0088
 -16.250  -0.8011   0.09159   0.08873  -0.0548   1.0000   0.0090
 -16.000  -0.8118   0.08654   0.08360  -0.0571   1.0000   0.0089
 -15.750  -0.8223   0.08167   0.07865  -0.0593   1.0000   0.0089
 -15.500  -0.8288   0.07728   0.07420  -0.0613   1.0000   0.0092
 -15.250  -0.8384   0.07283   0.06967  -0.0631   1.0000   0.0091
 -15.000  -0.8479   0.06843   0.06521  -0.0649   1.0000   0.0092
 -14.750  -0.8583   0.06414   0.06085  -0.0666   1.0000   0.0092
 -14.500  -0.8661   0.06024   0.05688  -0.0681   1.0000   0.0094
 -14.250  -0.8765   0.05637   0.05294  -0.0694   1.0000   0.0095
 -14.000  -0.8878   0.05262   0.04912  -0.0704   1.0000   0.0095
 -13.750  -0.9024   0.04875   0.04518  -0.0712   1.0000   0.0095
 -13.500  -0.9149   0.04527   0.04164  -0.0717   1.0000   0.0095
 -13.250  -0.9314   0.04175   0.03805  -0.0717   1.0000   0.0095
 -13.000  -0.9454   0.03876   0.03499  -0.0712   1.0000   0.0097
 -12.750  -0.9653   0.03508   0.03123  -0.0714   0.9993   0.0096
 -12.500  -0.9488   0.03168   0.02772  -0.0776   0.9955   0.0098
 -12.250  -0.9226   0.02813   0.02404  -0.0855   0.9925   0.0100
 -12.000  -0.8924   0.02584   0.02163  -0.0913   0.9891   0.0102
 -11.750  -0.8630   0.02343   0.01906  -0.0966   0.9863   0.0104
 -11.500  -0.8317   0.02131   0.01685  -0.1012   0.9846   0.0110
 -11.250  -0.7969   0.02052   0.01602  -0.1041   0.9838   0.0115
 -11.000  -0.7750   0.01954   0.01498  -0.1043   0.9788   0.0118
 -10.750  -0.7435   0.01869   0.01407  -0.1062   0.9766   0.0123
 -10.500  -0.7098   0.01791   0.01322  -0.1084   0.9751   0.0127
 -10.250  -0.6752   0.01730   0.01255  -0.1105   0.9739   0.0131
 -10.000  -0.6411   0.01598   0.01116  -0.1134   0.9729   0.0141
  -9.750  -0.6181   0.01534   0.01048  -0.1130   0.9676   0.0147
  -9.500  -0.5862   0.01476   0.00986  -0.1143   0.9649   0.0154
  -9.250  -0.5519   0.01426   0.00931  -0.1160   0.9632   0.0162
  -9.000  -0.5172   0.01339   0.00839  -0.1182   0.9617   0.0174
  -8.750  -0.4813   0.01285   0.00783  -0.1202   0.9606   0.0186
  -8.500  -0.4598   0.01242   0.00736  -0.1191   0.9532   0.0196
  -8.250  -0.4266   0.01179   0.00670  -0.1205   0.9505   0.0213
  -8.000  -0.3921   0.01127   0.00616  -0.1221   0.9483   0.0231
  -7.750  -0.3677   0.01089   0.00573  -0.1215   0.9407   0.0245
  -7.500  -0.3349   0.01032   0.00516  -0.1227   0.9365   0.0279
  -7.250  -0.2995   0.00981   0.00466  -0.1244   0.9322   0.0335
  -7.000  -0.2651   0.00923   0.00415  -0.1261   0.9250   0.0496
  -6.750  -0.2214   0.00856   0.00362  -0.1298   0.9203   0.0797
  -6.500  -0.1780   0.00808   0.00324  -0.1334   0.9118   0.1066
  -6.250  -0.1285   0.00767   0.00290  -0.1383   0.9029   0.1360
  -6.000  -0.0877   0.00735   0.00264  -0.1413   0.8873   0.1660
  -5.750  -0.0539   0.00718   0.00245  -0.1426   0.8680   0.1872
  -5.500  -0.0240   0.00708   0.00231  -0.1430   0.8480   0.2042
  -5.250   0.0038   0.00702   0.00220  -0.1429   0.8286   0.2198
  -5.000   0.0307   0.00699   0.00210  -0.1426   0.8101   0.2340
  -4.750   0.0572   0.00697   0.00202  -0.1423   0.7923   0.2466
  -4.500   0.0838   0.00696   0.00196  -0.1419   0.7754   0.2590
  -4.250   0.1103   0.00694   0.00189  -0.1415   0.7590   0.2709
  -4.000   0.1368   0.00694   0.00184  -0.1411   0.7431   0.2809
  -3.500   0.1904   0.00695   0.00175  -0.1405   0.7127   0.3000
  -3.250   0.2175   0.00698   0.00171  -0.1402   0.6984   0.3075
  -3.000   0.2446   0.00698   0.00168  -0.1399   0.6843   0.3166
  -2.750   0.2717   0.00702   0.00165  -0.1397   0.6711   0.3237
  -2.500   0.2988   0.00704   0.00163  -0.1394   0.6582   0.3327
  -2.250   0.3259   0.00709   0.00162  -0.1391   0.6449   0.3418
  -2.000   0.3533   0.00710   0.00162  -0.1390   0.6323   0.3518
  -1.750   0.3808   0.00714   0.00162  -0.1388   0.6205   0.3593
  -1.500   0.4081   0.00718   0.00162  -0.1386   0.6086   0.3671
  -1.250   0.4352   0.00725   0.00163  -0.1383   0.5967   0.3744
  -1.000   0.4630   0.00727   0.00165  -0.1382   0.5857   0.3827
  -0.750   0.4904   0.00734   0.00166  -0.1380   0.5748   0.3897
  -0.500   0.5175   0.00739   0.00169  -0.1378   0.5637   0.3974
  -0.250   0.5452   0.00745   0.00172  -0.1377   0.5532   0.4047
   0.000   0.5727   0.00750   0.00176  -0.1375   0.5433   0.4128
   0.500   0.6275   0.00763   0.00184  -0.1371   0.5231   0.4278
   0.750   0.6546   0.00772   0.00190  -0.1369   0.5136   0.4358
   1.000   0.6820   0.00778   0.00195  -0.1367   0.5039   0.4435
   1.250   0.7093   0.00786   0.00201  -0.1366   0.4949   0.4516
   1.500   0.7363   0.00795   0.00208  -0.1363   0.4857   0.4593
   1.750   0.7637   0.00802   0.00215  -0.1362   0.4772   0.4675
   2.000   0.7904   0.00812   0.00223  -0.1359   0.4682   0.4754
   2.250   0.8179   0.00818   0.00231  -0.1357   0.4603   0.4844
   2.500   0.8444   0.00830   0.00240  -0.1354   0.4518   0.4928
   2.750   0.8718   0.00836   0.00249  -0.1353   0.4444   0.5022
   3.000   0.8982   0.00848   0.00260  -0.1349   0.4361   0.5119
   3.250   0.9255   0.00856   0.00269  -0.1348   0.4291   0.5219
   3.500   0.9519   0.00867   0.00281  -0.1344   0.4212   0.5331
   3.750   0.9787   0.00875   0.00292  -0.1342   0.4143   0.5452
   4.000   1.0051   0.00886   0.00304  -0.1339   0.4066   0.5579
   4.500   1.0579   0.00907   0.00331  -0.1333   0.3922   0.5889
   4.750   1.0838   0.00919   0.00346  -0.1329   0.3851   0.6070
   5.000   1.1102   0.00928   0.00361  -0.1326   0.3777   0.6282
   5.250   1.1356   0.00941   0.00378  -0.1321   0.3701   0.6525
   5.500   1.1617   0.00950   0.00394  -0.1318   0.3626   0.6800
   5.750   1.1865   0.00964   0.00414  -0.1312   0.3547   0.7133
   6.000   1.2122   0.00971   0.00432  -0.1308   0.3472   0.7534
   6.250   1.2357   0.00983   0.00454  -0.1299   0.3392   0.8037
   6.500   1.2571   0.00981   0.00473  -0.1285   0.3321   0.8795
   6.750   1.2756   0.00986   0.00487  -0.1264   0.3234   1.0000
   7.000   1.3007   0.01005   0.00505  -0.1259   0.3151   1.0000
   7.250   1.3245   0.01029   0.00526  -0.1252   0.3062   1.0000
   7.500   1.3481   0.01052   0.00547  -0.1245   0.2969   1.0000
   7.750   1.3710   0.01076   0.00569  -0.1235   0.2880   1.0000
   8.000   1.3923   0.01106   0.00594  -0.1224   0.2780   1.0000
   8.250   1.4144   0.01131   0.00618  -0.1213   0.2679   1.0000
   8.500   1.4353   0.01161   0.00646  -0.1201   0.2577   1.0000
   8.750   1.4548   0.01198   0.00677  -0.1186   0.2451   1.0000
   9.000   1.4732   0.01239   0.00711  -0.1170   0.2301   1.0000
   9.250   1.4912   0.01283   0.00749  -0.1153   0.2161   1.0000
   9.500   1.5086   0.01329   0.00789  -0.1135   0.2023   1.0000
   9.750   1.5248   0.01379   0.00833  -0.1116   0.1880   1.0000
  10.000   1.5401   0.01434   0.00881  -0.1095   0.1735   1.0000
  10.250   1.5543   0.01494   0.00934  -0.1074   0.1580   1.0000
  10.500   1.5667   0.01562   0.00994  -0.1049   0.1422   1.0000
  10.750   1.5776   0.01637   0.01062  -0.1023   0.1264   1.0000
  11.000   1.5869   0.01721   0.01137  -0.0996   0.1114   1.0000
  11.250   1.5969   0.01802   0.01213  -0.0970   0.0996   1.0000
  11.500   1.6057   0.01890   0.01297  -0.0943   0.0887   1.0000
  11.750   1.6137   0.01984   0.01387  -0.0917   0.0791   1.0000
  12.250   1.6284   0.02189   0.01587  -0.0866   0.0633   1.0000
  12.500   1.6353   0.02300   0.01699  -0.0842   0.0572   1.0000
  12.750   1.6401   0.02430   0.01827  -0.0818   0.0512   1.0000
  13.000   1.6466   0.02554   0.01954  -0.0797   0.0465   1.0000
  13.250   1.6493   0.02712   0.02111  -0.0774   0.0414   1.0000
  13.500   1.6542   0.02862   0.02265  -0.0755   0.0376   1.0000
  13.750   1.6562   0.03043   0.02448  -0.0736   0.0339   1.0000
  14.000   1.6585   0.03232   0.02640  -0.0720   0.0303   1.0000
  14.250   1.6598   0.03440   0.02851  -0.0705   0.0276   1.0000
  14.500   1.6609   0.03660   0.03076  -0.0693   0.0250   1.0000
  14.750   1.6603   0.03908   0.03329  -0.0682   0.0228   1.0000
  15.000   1.6608   0.04158   0.03585  -0.0673   0.0210   1.0000
  15.250   1.6580   0.04453   0.03885  -0.0666   0.0192   1.0000
  15.500   1.6576   0.04735   0.04175  -0.0662   0.0180   1.0000
  15.750   1.6555   0.05048   0.04495  -0.0660   0.0168   1.0000
  16.000   1.6511   0.05400   0.04853  -0.0659   0.0158   1.0000
  16.250   1.6474   0.05756   0.05217  -0.0661   0.0149   1.0000
  16.500   1.6444   0.06114   0.05585  -0.0664   0.0142   1.0000
  16.750   1.6388   0.06518   0.05997  -0.0670   0.0134   1.0000
  17.000   1.6317   0.06956   0.06443  -0.0678   0.0127   1.0000
  17.250   1.6234   0.07423   0.06919  -0.0688   0.0121   1.0000
  17.500   1.6193   0.07839   0.07345  -0.0699   0.0116   1.0000
  17.750   1.6128   0.08301   0.07817  -0.0712   0.0111   1.0000
  18.000   1.6049   0.08795   0.08320  -0.0727   0.0107   1.0000
  18.250   1.5954   0.09322   0.08856  -0.0744   0.0102   1.0000
  18.500   1.5830   0.09908   0.09451  -0.0765   0.0098   1.0000
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