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EPPLER EA 6(-1)-012 AIRFOIL (ea61012-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: EPPLER EA 6(-1)-012 AIRFOIL (ea61012-il)
Reynolds number: 1,000,000
Max Cl/Cd: 70.66 at α=11.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-ea61012-il-1000000-n5.txt
Download as CSV file: xf-ea61012-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: EPPLER EA 6(-1)-012 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
  ------ -------- --------- --------- -------- -------- --------
 -19.250  -1.4341   0.06704   0.06330  -0.0290   1.0000   0.0129
 -19.000  -1.4497   0.06133   0.05746  -0.0319   1.0000   0.0132
 -18.750  -1.4613   0.05651   0.05253  -0.0340   1.0000   0.0134
 -18.500  -1.4701   0.05235   0.04826  -0.0355   1.0000   0.0139
 -18.250  -1.4764   0.04872   0.04454  -0.0366   1.0000   0.0143
 -18.000  -1.4806   0.04557   0.04129  -0.0372   1.0000   0.0148
 -17.750  -1.4820   0.04282   0.03845  -0.0376   1.0000   0.0152
 -17.500  -1.4822   0.04030   0.03584  -0.0378   1.0000   0.0158
 -17.250  -1.4805   0.03806   0.03352  -0.0377   1.0000   0.0162
 -17.000  -1.4783   0.03591   0.03132  -0.0375   1.0000   0.0169
 -16.750  -1.4750   0.03397   0.02932  -0.0371   1.0000   0.0178
 -16.500  -1.4693   0.03227   0.02757  -0.0366   1.0000   0.0186
 -16.250  -1.4624   0.03075   0.02598  -0.0360   1.0000   0.0193
 -16.000  -1.4542   0.02938   0.02455  -0.0353   1.0000   0.0201
 -15.750  -1.4452   0.02810   0.02320  -0.0345   1.0000   0.0205
 -15.500  -1.4359   0.02688   0.02195  -0.0336   1.0000   0.0216
 -15.250  -1.4249   0.02582   0.02087  -0.0327   1.0000   0.0227
 -15.000  -1.4131   0.02486   0.01988  -0.0318   1.0000   0.0237
 -14.750  -1.4009   0.02395   0.01893  -0.0308   1.0000   0.0244
 -14.500  -1.3883   0.02311   0.01803  -0.0298   1.0000   0.0251
 -14.250  -1.3754   0.02234   0.01720  -0.0286   1.0000   0.0256
 -14.000  -1.3622   0.02162   0.01642  -0.0273   1.0000   0.0260
 -13.750  -1.3492   0.02095   0.01570  -0.0259   1.0000   0.0265
 -13.500  -1.3372   0.02025   0.01496  -0.0241   1.0000   0.0271
 -13.250  -1.3231   0.01972   0.01442  -0.0224   1.0000   0.0281
 -13.000  -1.3082   0.01926   0.01395  -0.0207   1.0000   0.0289
 -12.750  -1.2930   0.01883   0.01349  -0.0190   1.0000   0.0296
 -12.500  -1.2754   0.01843   0.01306  -0.0176   1.0000   0.0303
 -12.250  -1.2563   0.01801   0.01261  -0.0165   1.0000   0.0310
 -12.000  -1.2361   0.01763   0.01220  -0.0155   1.0000   0.0316
 -11.750  -1.2155   0.01725   0.01179  -0.0146   1.0000   0.0322
 -11.500  -1.1876   0.01685   0.01134  -0.0151   0.9608   0.0327
 -11.250  -1.1519   0.01663   0.01088  -0.0172   0.8725   0.0332
 -11.000  -1.1315   0.01641   0.01053  -0.0160   0.8496   0.0334
 -10.750  -1.1107   0.01607   0.01011  -0.0150   0.8384   0.0340
 -10.500  -1.0905   0.01562   0.00960  -0.0139   0.8300   0.0353
 -10.250  -1.0679   0.01530   0.00925  -0.0132   0.8235   0.0362
 -10.000  -1.0452   0.01498   0.00888  -0.0124   0.8175   0.0368
  -9.750  -1.0216   0.01470   0.00857  -0.0118   0.8126   0.0375
  -9.500  -0.9977   0.01442   0.00825  -0.0113   0.8079   0.0382
  -9.250  -0.9737   0.01413   0.00792  -0.0107   0.8037   0.0388
  -8.750  -0.9251   0.01356   0.00727  -0.0096   0.7966   0.0398
  -8.500  -0.9003   0.01328   0.00695  -0.0092   0.7930   0.0403
  -8.250  -0.8755   0.01300   0.00663  -0.0087   0.7894   0.0407
  -8.000  -0.8503   0.01276   0.00635  -0.0083   0.7859   0.0412
  -7.750  -0.8249   0.01252   0.00607  -0.0079   0.7826   0.0415
  -7.500  -0.7990   0.01230   0.00583  -0.0076   0.7791   0.0418
  -7.250  -0.7729   0.01210   0.00560  -0.0073   0.7755   0.0421
  -7.000  -0.7481   0.01176   0.00522  -0.0068   0.7721   0.0430
  -6.500  -0.6966   0.01123   0.00466  -0.0060   0.7660   0.0450
  -6.250  -0.6703   0.01101   0.00443  -0.0058   0.7626   0.0459
  -6.000  -0.6438   0.01080   0.00422  -0.0055   0.7591   0.0468
  -5.750  -0.6171   0.01062   0.00401  -0.0052   0.7558   0.0476
  -5.500  -0.5904   0.01044   0.00382  -0.0050   0.7527   0.0485
  -5.250  -0.5633   0.01026   0.00363  -0.0048   0.7493   0.0492
  -5.000  -0.5361   0.01010   0.00346  -0.0047   0.7454   0.0499
  -4.750  -0.5089   0.00995   0.00329  -0.0045   0.7415   0.0505
  -4.500  -0.4818   0.00981   0.00313  -0.0043   0.7380   0.0513
  -4.250  -0.4546   0.00961   0.00294  -0.0041   0.7341   0.0532
  -4.000  -0.4274   0.00944   0.00278  -0.0039   0.7290   0.0549
  -3.750  -0.4001   0.00929   0.00263  -0.0037   0.7238   0.0565
  -3.500  -0.3725   0.00915   0.00249  -0.0036   0.7189   0.0582
  -3.250  -0.3448   0.00903   0.00237  -0.0035   0.7134   0.0597
  -3.000  -0.3174   0.00889   0.00223  -0.0033   0.7083   0.0630
  -2.750  -0.2898   0.00875   0.00212  -0.0032   0.7038   0.0670
  -2.500  -0.2622   0.00860   0.00200  -0.0031   0.6985   0.0737
  -2.250  -0.2350   0.00842   0.00188  -0.0029   0.6932   0.0884
  -2.000  -0.2085   0.00813   0.00174  -0.0026   0.6878   0.1245
  -1.750  -0.1822   0.00782   0.00161  -0.0024   0.6824   0.1718
  -1.500  -0.1559   0.00755   0.00148  -0.0021   0.6746   0.2164
  -1.250  -0.1297   0.00722   0.00136  -0.0018   0.6667   0.2730
  -1.000  -0.1040   0.00688   0.00124  -0.0015   0.6586   0.3433
  -0.750  -0.0776   0.00659   0.00115  -0.0012   0.6482   0.4010
  -0.500  -0.0529   0.00618   0.00101  -0.0007   0.6330   0.4868
  -0.250  -0.0273   0.00596   0.00098  -0.0002   0.6134   0.5643
   0.000   0.0000   0.00594   0.00098   0.0000   0.5934   0.5935
   0.250   0.0273   0.00596   0.00098   0.0002   0.5641   0.6128
   0.500   0.0530   0.00616   0.00101   0.0007   0.4916   0.6338
   0.750   0.0776   0.00659   0.00115   0.0012   0.4009   0.6484
   1.000   0.1040   0.00688   0.00124   0.0015   0.3433   0.6585
   1.250   0.1296   0.00723   0.00136   0.0018   0.2720   0.6663
   1.750   0.1822   0.00781   0.00160   0.0024   0.1730   0.6824
   2.000   0.2086   0.00812   0.00173   0.0026   0.1261   0.6879
   2.250   0.2350   0.00842   0.00188   0.0029   0.0886   0.6932
   2.500   0.2622   0.00860   0.00200   0.0031   0.0738   0.6985
   2.750   0.2898   0.00875   0.00212   0.0032   0.0670   0.7039
   3.000   0.3174   0.00889   0.00223   0.0033   0.0630   0.7083
   3.250   0.3448   0.00903   0.00237   0.0035   0.0597   0.7134
   3.500   0.3726   0.00915   0.00249   0.0036   0.0582   0.7189
   3.750   0.4001   0.00929   0.00263   0.0037   0.0565   0.7238
   4.000   0.4274   0.00944   0.00278   0.0039   0.0549   0.7291
   4.250   0.4547   0.00961   0.00294   0.0041   0.0533   0.7340
   4.500   0.4818   0.00981   0.00313   0.0043   0.0513   0.7379
   4.750   0.5089   0.00995   0.00329   0.0045   0.0506   0.7415
   5.000   0.5361   0.01010   0.00346   0.0047   0.0500   0.7454
   5.250   0.5633   0.01026   0.00363   0.0048   0.0492   0.7493
   5.500   0.5904   0.01044   0.00382   0.0050   0.0485   0.7527
   5.750   0.6172   0.01062   0.00402   0.0052   0.0476   0.7558
   6.000   0.6438   0.01080   0.00422   0.0055   0.0468   0.7591
   6.250   0.6703   0.01101   0.00443   0.0058   0.0459   0.7626
   6.500   0.6967   0.01123   0.00466   0.0060   0.0450   0.7660
   7.000   0.7482   0.01176   0.00522   0.0068   0.0431   0.7721
   7.250   0.7729   0.01211   0.00560   0.0073   0.0421   0.7755
   7.500   0.7990   0.01230   0.00583   0.0076   0.0418   0.7791
   7.750   0.8249   0.01252   0.00607   0.0079   0.0415   0.7826
   8.000   0.8504   0.01276   0.00635   0.0083   0.0412   0.7859
   8.250   0.8755   0.01301   0.00664   0.0087   0.0408   0.7894
   8.500   0.9004   0.01327   0.00695   0.0092   0.0403   0.7930
   8.750   0.9252   0.01355   0.00726   0.0096   0.0398   0.7966
   9.250   0.9739   0.01412   0.00791   0.0107   0.0387   0.8037
   9.500   0.9977   0.01442   0.00825   0.0113   0.0382   0.8079
   9.750   1.0218   0.01469   0.00856   0.0118   0.0375   0.8126
  10.000   1.0453   0.01498   0.00888   0.0124   0.0368   0.8175
  10.250   1.0681   0.01528   0.00923   0.0131   0.0361   0.8235
  10.500   1.0907   0.01561   0.00958   0.0139   0.0352   0.8300
  10.750   1.1107   0.01607   0.01011   0.0150   0.0339   0.8384
  11.000   1.1315   0.01641   0.01053   0.0160   0.0334   0.8496
  11.250   1.1519   0.01663   0.01089   0.0172   0.0332   0.8723
  11.500   1.1872   0.01686   0.01136   0.0152   0.0327   0.9601
  11.750   1.2160   0.01721   0.01175   0.0145   0.0321   1.0000
  12.000   1.2365   0.01760   0.01217   0.0154   0.0315   1.0000
  12.250   1.2564   0.01801   0.01261   0.0165   0.0309   1.0000
  12.500   1.2759   0.01840   0.01303   0.0175   0.0302   1.0000
  12.750   1.2933   0.01883   0.01349   0.0189   0.0296   1.0000
  13.000   1.3088   0.01925   0.01393   0.0206   0.0288   1.0000
  13.250   1.3235   0.01971   0.01441   0.0224   0.0281   1.0000
  13.500   1.3374   0.02026   0.01497   0.0241   0.0272   1.0000
  13.750   1.3494   0.02096   0.01571   0.0258   0.0263   1.0000
  14.000   1.3627   0.02162   0.01642   0.0272   0.0260   1.0000
  14.250   1.3759   0.02233   0.01719   0.0285   0.0256   1.0000
  14.500   1.3887   0.02311   0.01803   0.0297   0.0251   1.0000
  14.750   1.4016   0.02394   0.01891   0.0307   0.0244   1.0000
  15.000   1.4137   0.02485   0.01988   0.0317   0.0237   1.0000
  15.250   1.4257   0.02580   0.02086   0.0326   0.0227   1.0000
  15.500   1.4365   0.02688   0.02197   0.0335   0.0220   1.0000
  15.750   1.4464   0.02806   0.02317   0.0343   0.0209   1.0000
  16.000   1.4553   0.02935   0.02451   0.0351   0.0200   1.0000
  16.250   1.4636   0.03072   0.02595   0.0358   0.0194   1.0000
  16.500   1.4707   0.03224   0.02753   0.0364   0.0186   1.0000
  16.750   1.4762   0.03394   0.02929   0.0369   0.0178   1.0000
  17.000   1.4800   0.03585   0.03126   0.0373   0.0169   1.0000
  17.250   1.4822   0.03799   0.03345   0.0375   0.0163   1.0000
  17.500   1.4840   0.04024   0.03579   0.0376   0.0157   1.0000
  17.750   1.4844   0.04269   0.03833   0.0374   0.0153   1.0000
  18.000   1.4824   0.04551   0.04123   0.0370   0.0147   1.0000
  18.250   1.4787   0.04862   0.04443   0.0364   0.0143   1.0000
  18.500   1.4717   0.05233   0.04823   0.0353   0.0138   1.0000
  18.750   1.4636   0.05640   0.05242   0.0338   0.0135   1.0000
  19.000   1.4521   0.06119   0.05732   0.0317   0.0132   1.0000
  19.250   1.4383   0.06664   0.06290   0.0290   0.0130   1.0000
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