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EPPLER EA 6(-1)-009 AIRFOIL (ea61009-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: EPPLER EA 6(-1)-009 AIRFOIL (ea61009-il)
Reynolds number: 1,000,000
Max Cl/Cd: 76.02 at α=9°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-ea61009-il-1000000-n5.txt
Download as CSV file: xf-ea61009-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: EPPLER EA 6(-1)-009 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
  ------ -------- --------- --------- -------- -------- --------
 -16.500  -1.2783   0.06855   0.06583  -0.0090   1.0000   0.0044
 -16.250  -1.3102   0.05842   0.05549  -0.0162   1.0000   0.0044
 -16.000  -1.3365   0.05084   0.04771  -0.0210   1.0000   0.0044
 -15.750  -1.3520   0.04579   0.04250  -0.0233   1.0000   0.0044
 -15.500  -1.3660   0.04151   0.03806  -0.0246   1.0000   0.0044
 -15.250  -1.3755   0.03817   0.03458  -0.0247   1.0000   0.0045
 -15.000  -1.3844   0.03523   0.03148  -0.0241   1.0000   0.0046
 -14.750  -1.3886   0.03296   0.02909  -0.0229   1.0000   0.0047
 -14.500  -1.3917   0.03102   0.02702  -0.0212   1.0000   0.0048
 -14.250  -1.3927   0.02945   0.02534  -0.0189   1.0000   0.0048
 -14.000  -1.3903   0.02812   0.02391  -0.0163   1.0000   0.0050
 -13.750  -1.3810   0.02684   0.02252  -0.0148   1.0000   0.0051
 -13.500  -1.3684   0.02569   0.02127  -0.0135   1.0000   0.0053
 -13.250  -1.3539   0.02460   0.02007  -0.0123   1.0000   0.0054
 -13.000  -1.3376   0.02360   0.01897  -0.0114   1.0000   0.0056
 -12.750  -1.3198   0.02268   0.01796  -0.0105   1.0000   0.0058
 -12.500  -1.3009   0.02183   0.01703  -0.0097   1.0000   0.0060
 -12.250  -1.2811   0.02103   0.01614  -0.0090   1.0000   0.0062
 -12.000  -1.2603   0.02030   0.01532  -0.0084   1.0000   0.0064
 -11.750  -1.2393   0.01954   0.01448  -0.0078   1.0000   0.0066
 -11.500  -1.2189   0.01863   0.01347  -0.0071   1.0000   0.0072
 -11.250  -1.1971   0.01787   0.01265  -0.0065   1.0000   0.0076
 -11.000  -1.1748   0.01716   0.01189  -0.0060   1.0000   0.0081
 -10.750  -1.1518   0.01653   0.01120  -0.0056   1.0000   0.0085
 -10.500  -1.1282   0.01596   0.01057  -0.0052   1.0000   0.0090
 -10.250  -1.1040   0.01545   0.00999  -0.0048   1.0000   0.0094
 -10.000  -1.0798   0.01490   0.00938  -0.0045   1.0000   0.0103
  -9.750  -1.0558   0.01431   0.00877  -0.0041   1.0000   0.0118
  -9.500  -1.0315   0.01376   0.00821  -0.0038   1.0000   0.0135
  -9.250  -1.0065   0.01330   0.00774  -0.0035   1.0000   0.0168
  -9.000  -0.9810   0.01290   0.00739  -0.0033   1.0000   0.0215
  -8.750  -0.9551   0.01257   0.00703  -0.0031   1.0000   0.0235
  -8.500  -0.9286   0.01231   0.00679  -0.0030   1.0000   0.0257
  -8.250  -0.9017   0.01213   0.00663  -0.0029   1.0000   0.0279
  -8.000  -0.8666   0.01196   0.00641  -0.0046   0.9420   0.0298
  -7.750  -0.8409   0.01186   0.00618  -0.0042   0.9161   0.0307
  -7.500  -0.8151   0.01174   0.00599  -0.0038   0.9024   0.0312
  -7.250  -0.7894   0.01147   0.00568  -0.0034   0.8924   0.0325
  -6.750  -0.7360   0.01122   0.00539  -0.0030   0.8767   0.0346
  -6.500  -0.7090   0.01112   0.00526  -0.0028   0.8701   0.0356
  -6.250  -0.6814   0.01105   0.00518  -0.0027   0.8643   0.0367
  -6.000  -0.6544   0.01089   0.00497  -0.0026   0.8583   0.0375
  -5.750  -0.6276   0.01066   0.00469  -0.0024   0.8530   0.0379
  -5.500  -0.6005   0.01043   0.00443  -0.0022   0.8477   0.0383
  -5.250  -0.5735   0.01022   0.00418  -0.0021   0.8424   0.0386
  -5.000  -0.5463   0.01002   0.00394  -0.0020   0.8369   0.0389
  -4.750  -0.5190   0.00983   0.00372  -0.0018   0.8303   0.0391
  -4.500  -0.4918   0.00966   0.00350  -0.0017   0.8242   0.0393
  -4.250  -0.4650   0.00928   0.00309  -0.0015   0.8182   0.0407
  -4.000  -0.4376   0.00905   0.00283  -0.0014   0.8125   0.0420
  -3.750  -0.4100   0.00889   0.00266  -0.0013   0.8074   0.0434
  -3.500  -0.3824   0.00875   0.00250  -0.0012   0.7981   0.0446
  -3.250  -0.3549   0.00862   0.00232  -0.0010   0.7835   0.0454
  -3.000  -0.3273   0.00849   0.00216  -0.0009   0.7701   0.0463
  -2.750  -0.2996   0.00838   0.00201  -0.0008   0.7596   0.0472
  -2.500  -0.2718   0.00828   0.00187  -0.0007   0.7469   0.0480
  -2.250  -0.2440   0.00818   0.00174  -0.0006   0.7318   0.0489
  -2.000  -0.2162   0.00811   0.00162  -0.0005   0.7124   0.0496
  -1.750  -0.1887   0.00810   0.00150  -0.0004   0.6786   0.0503
  -1.500  -0.1613   0.00814   0.00140  -0.0002   0.6371   0.0508
  -1.250  -0.1341   0.00823   0.00131  -0.0001   0.5788   0.0520
  -1.000  -0.1076   0.00853   0.00125   0.0000   0.4639   0.0543
  -0.750  -0.0804   0.00873   0.00124   0.0000   0.3945   0.0565
  -0.500  -0.0539   0.00916   0.00125   0.0000   0.2620   0.0588
  -0.250  -0.0266   0.00937   0.00127   0.0000   0.1975   0.0634
   0.000   0.0000   0.00920   0.00120   0.0000   0.1494   0.1498
   0.250   0.0266   0.00937   0.00127   0.0000   0.0634   0.1973
   0.500   0.0539   0.00916   0.00125   0.0000   0.0588   0.2620
   0.750   0.0804   0.00874   0.00124   0.0000   0.0565   0.3939
   1.000   0.1076   0.00853   0.00125   0.0000   0.0543   0.4627
   1.250   0.1340   0.00822   0.00131   0.0001   0.0520   0.5798
   1.500   0.1612   0.00814   0.00140   0.0002   0.0508   0.6374
   1.750   0.1886   0.00809   0.00150   0.0004   0.0503   0.6793
   2.000   0.2161   0.00811   0.00162   0.0005   0.0496   0.7123
   2.250   0.2439   0.00818   0.00174   0.0006   0.0489   0.7323
   2.500   0.2718   0.00827   0.00187   0.0007   0.0480   0.7472
   2.750   0.2995   0.00838   0.00201   0.0008   0.0472   0.7596
   3.000   0.3273   0.00849   0.00216   0.0009   0.0463   0.7700
   3.250   0.3549   0.00862   0.00232   0.0010   0.0455   0.7832
   3.500   0.3823   0.00874   0.00250   0.0012   0.0446   0.7982
   3.750   0.4100   0.00889   0.00266   0.0013   0.0434   0.8073
   4.000   0.4376   0.00905   0.00283   0.0014   0.0420   0.8124
   4.250   0.4649   0.00928   0.00309   0.0015   0.0407   0.8181
   4.500   0.4917   0.00967   0.00351   0.0017   0.0393   0.8242
   4.750   0.5189   0.00983   0.00372   0.0018   0.0391   0.8304
   5.000   0.5462   0.01002   0.00394   0.0020   0.0389   0.8369
   5.250   0.5734   0.01022   0.00418   0.0021   0.0386   0.8424
   5.500   0.6004   0.01043   0.00443   0.0023   0.0383   0.8476
   5.750   0.6275   0.01066   0.00469   0.0024   0.0379   0.8529
   6.000   0.6542   0.01090   0.00497   0.0026   0.0375   0.8583
   6.250   0.6813   0.01105   0.00518   0.0028   0.0368   0.8643
   6.500   0.7088   0.01112   0.00526   0.0028   0.0356   0.8701
   6.750   0.7358   0.01122   0.00539   0.0030   0.0346   0.8766
   7.250   0.7893   0.01147   0.00568   0.0034   0.0325   0.8924
   7.500   0.8149   0.01174   0.00599   0.0038   0.0312   0.9024
   7.750   0.8407   0.01185   0.00618   0.0042   0.0307   0.9164
   8.000   0.8663   0.01196   0.00641   0.0047   0.0298   0.9427
   8.250   0.9014   0.01213   0.00663   0.0030   0.0279   1.0000
   8.500   0.9283   0.01231   0.00679   0.0031   0.0257   1.0000
   8.750   0.9548   0.01256   0.00703   0.0032   0.0235   1.0000
   9.000   0.9807   0.01290   0.00739   0.0034   0.0215   1.0000
   9.250   1.0061   0.01329   0.00774   0.0036   0.0169   1.0000
   9.500   1.0311   0.01375   0.00821   0.0039   0.0136   1.0000
   9.750   1.0554   0.01430   0.00876   0.0042   0.0119   1.0000
  10.000   1.0793   0.01490   0.00938   0.0046   0.0103   1.0000
  10.250   1.1035   0.01544   0.00999   0.0049   0.0094   1.0000
  10.500   1.1276   0.01595   0.01056   0.0053   0.0090   1.0000
  10.750   1.1512   0.01653   0.01120   0.0057   0.0085   1.0000
  11.000   1.1742   0.01715   0.01188   0.0062   0.0081   1.0000
  11.250   1.1965   0.01786   0.01265   0.0067   0.0076   1.0000
  11.500   1.2182   0.01862   0.01346   0.0072   0.0072   1.0000
  11.750   1.2387   0.01952   0.01446   0.0079   0.0066   1.0000
  12.000   1.2596   0.02029   0.01531   0.0085   0.0064   1.0000
  12.250   1.2802   0.02104   0.01614   0.0092   0.0062   1.0000
  12.500   1.3001   0.02182   0.01701   0.0099   0.0060   1.0000
  12.750   1.3190   0.02267   0.01795   0.0106   0.0058   1.0000
  13.000   1.3367   0.02359   0.01897   0.0115   0.0056   1.0000
  13.250   1.3531   0.02457   0.02005   0.0125   0.0055   1.0000
  13.500   1.3676   0.02565   0.02123   0.0136   0.0053   1.0000
  13.750   1.3799   0.02685   0.02253   0.0150   0.0051   1.0000
  14.000   1.3896   0.02807   0.02385   0.0165   0.0050   1.0000
  14.250   1.3919   0.02941   0.02530   0.0190   0.0049   1.0000
  14.500   1.3911   0.03097   0.02698   0.0213   0.0048   1.0000
  14.750   1.3888   0.03285   0.02898   0.0231   0.0047   1.0000
  15.000   1.3830   0.03527   0.03153   0.0243   0.0045   1.0000
  15.250   1.3728   0.03835   0.03477   0.0248   0.0044   1.0000
  15.500   1.3675   0.04126   0.03781   0.0247   0.0045   1.0000
  15.750   1.3501   0.04594   0.04266   0.0233   0.0044   1.0000
  16.000   1.3345   0.05105   0.04793   0.0209   0.0044   1.0000
  16.250   1.3130   0.05786   0.05492   0.0167   0.0044   1.0000
  16.500   1.2821   0.06771   0.06497   0.0097   0.0045   1.0000
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