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EPPLER 584 AIRFOIL (e584-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: EPPLER 584 AIRFOIL (e584-il)
Reynolds number: 500,000
Max Cl/Cd: 101.76 at α=6.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-e584-il-500000-n5.txt
Download as CSV file: xf-e584-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: EPPLER 584 AIRFOIL                              
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.750  -0.0788   0.09309   0.08911  -0.1161   0.6946   0.0081
 -11.500  -0.0764   0.08993   0.08595  -0.1174   0.6914   0.0079
 -11.250  -0.0751   0.08658   0.08260  -0.1187   0.6885   0.0078
 -11.000  -0.0788   0.08219   0.07821  -0.1204   0.6860   0.0076
 -10.750  -0.0809   0.07829   0.07431  -0.1220   0.6834   0.0074
 -10.250  -0.2393   0.04235   0.03813  -0.1366   0.6811   0.0059
 -10.000  -0.2793   0.03724   0.03274  -0.1328   0.6790   0.0058
  -9.750  -0.2949   0.03474   0.03005  -0.1290   0.6768   0.0058
  -9.500  -0.3125   0.03231   0.02739  -0.1239   0.6746   0.0057
  -9.250  -0.3219   0.03002   0.02482  -0.1196   0.6727   0.0057
  -9.000  -0.3268   0.02737   0.02180  -0.1157   0.6711   0.0057
  -8.750  -0.3221   0.02535   0.01945  -0.1128   0.6695   0.0057
  -8.250  -0.2985   0.02217   0.01572  -0.1087   0.6666   0.0056
  -8.000  -0.2815   0.02096   0.01429  -0.1072   0.6654   0.0056
  -7.750  -0.2630   0.01981   0.01293  -0.1060   0.6640   0.0057
  -7.500  -0.2428   0.01886   0.01181  -0.1049   0.6627   0.0057
  -7.250  -0.2216   0.01806   0.01088  -0.1040   0.6612   0.0057
  -7.000  -0.2000   0.01732   0.01000  -0.1032   0.6596   0.0058
  -6.750  -0.1779   0.01668   0.00925  -0.1024   0.6579   0.0058
  -6.500  -0.1554   0.01613   0.00860  -0.1016   0.6564   0.0059
  -6.250  -0.1326   0.01561   0.00798  -0.1009   0.6549   0.0060
  -6.000  -0.1095   0.01515   0.00745  -0.1003   0.6535   0.0060
  -5.750  -0.0872   0.01460   0.00683  -0.0995   0.6522   0.0062
  -5.500  -0.0640   0.01419   0.00639  -0.0989   0.6510   0.0064
  -5.250  -0.0402   0.01383   0.00601  -0.0983   0.6495   0.0068
  -5.000  -0.0161   0.01353   0.00567  -0.0978   0.6479   0.0071
  -4.750   0.0083   0.01324   0.00534  -0.0973   0.6461   0.0077
  -4.500   0.0331   0.01300   0.00505  -0.0969   0.6446   0.0082
  -4.250   0.0577   0.01273   0.00476  -0.0965   0.6431   0.0093
  -4.000   0.0830   0.01253   0.00451  -0.0962   0.6415   0.0107
  -3.750   0.1084   0.01235   0.00430  -0.0959   0.6398   0.0134
  -3.500   0.1339   0.01216   0.00412  -0.0957   0.6382   0.0205
  -3.250   0.1582   0.01191   0.00396  -0.0952   0.6366   0.0354
  -3.000   0.1825   0.01165   0.00382  -0.0948   0.6348   0.0589
  -2.750   0.2065   0.01135   0.00370  -0.0944   0.6329   0.0987
  -2.500   0.2300   0.01101   0.00358  -0.0939   0.6310   0.1588
  -2.250   0.2531   0.01062   0.00347  -0.0935   0.6291   0.2379
  -2.000   0.2755   0.01015   0.00335  -0.0929   0.6273   0.3457
  -1.750   0.2969   0.00953   0.00319  -0.0924   0.6256   0.4901
  -1.500   0.3147   0.00876   0.00324  -0.0907   0.6239   0.7092
  -1.250   0.3383   0.00898   0.00364  -0.0894   0.6220   0.7814
  -1.000   0.3660   0.00909   0.00372  -0.0894   0.6198   0.7984
  -0.750   0.3939   0.00919   0.00377  -0.0895   0.6175   0.8090
  -0.500   0.4207   0.00936   0.00391  -0.0892   0.6153   0.8192
  -0.250   0.4448   0.00967   0.00422  -0.0880   0.6133   0.8319
   0.000   0.4678   0.01000   0.00455  -0.0865   0.6114   0.8441
   0.250   0.4929   0.01016   0.00469  -0.0858   0.6095   0.8497
   0.500   0.5205   0.01015   0.00466  -0.0860   0.6068   0.8516
   0.750   0.5486   0.01013   0.00462  -0.0863   0.6040   0.8533
   1.000   0.5770   0.01011   0.00458  -0.0868   0.6013   0.8547
   1.250   0.6055   0.01009   0.00452  -0.0872   0.5987   0.8557
   1.500   0.6327   0.01008   0.00447  -0.0873   0.5964   0.8565
   1.750   0.6597   0.01007   0.00447  -0.0874   0.5934   0.8572
   2.000   0.6868   0.01006   0.00447  -0.0875   0.5900   0.8578
   2.250   0.7135   0.01005   0.00446  -0.0875   0.5866   0.8586
   2.500   0.7400   0.01005   0.00444  -0.0874   0.5835   0.8594
   2.750   0.7668   0.01005   0.00443  -0.0875   0.5803   0.8600
   3.000   0.7936   0.01007   0.00446  -0.0876   0.5762   0.8607
   3.250   0.8200   0.01008   0.00447  -0.0876   0.5722   0.8613
   3.500   0.8459   0.01010   0.00447  -0.0875   0.5682   0.8620
   3.750   0.8719   0.01014   0.00451  -0.0874   0.5639   0.8628
   4.000   0.8974   0.01018   0.00456  -0.0873   0.5587   0.8638
   4.250   0.9225   0.01023   0.00459  -0.0870   0.5537   0.8645
   4.500   0.9478   0.01029   0.00466  -0.0869   0.5486   0.8652
   4.750   0.9730   0.01036   0.00475  -0.0867   0.5429   0.8660
   5.000   0.9970   0.01045   0.00482  -0.0863   0.5370   0.8667
   5.250   1.0217   0.01053   0.00492  -0.0860   0.5313   0.8674
   5.500   1.0454   0.01062   0.00503  -0.0856   0.5244   0.8681
   5.750   1.0683   0.01073   0.00514  -0.0850   0.5180   0.8689
   6.000   1.0905   0.01083   0.00526  -0.0843   0.5096   0.8696
   6.250   1.1102   0.01096   0.00538  -0.0830   0.5016   0.8706
   6.500   1.1293   0.01110   0.00552  -0.0817   0.4922   0.8716
   6.750   1.1468   0.01127   0.00569  -0.0800   0.4824   0.8724
   7.000   1.1625   0.01151   0.00592  -0.0781   0.4724   0.8732
   7.250   1.1783   0.01177   0.00618  -0.0762   0.4607   0.8740
   7.500   1.1943   0.01205   0.00646  -0.0744   0.4502   0.8749
   7.750   1.2077   0.01240   0.00680  -0.0721   0.4388   0.8758
   8.000   1.2204   0.01279   0.00718  -0.0699   0.4269   0.8768
   8.250   1.2327   0.01322   0.00759  -0.0676   0.4137   0.8779
   8.500   1.2435   0.01371   0.00807  -0.0652   0.4005   0.8790
   8.750   1.2525   0.01429   0.00864  -0.0626   0.3866   0.8803
   9.000   1.2604   0.01496   0.00928  -0.0599   0.3727   0.8815
   9.250   1.2667   0.01574   0.01004  -0.0572   0.3581   0.8828
   9.500   1.2727   0.01660   0.01087  -0.0545   0.3445   0.8843
   9.750   1.2771   0.01760   0.01185  -0.0519   0.3297   0.8859
  10.000   1.2807   0.01873   0.01294  -0.0493   0.3148   0.8872
  10.500   1.2861   0.02121   0.01539  -0.0443   0.2852   0.8897
  10.750   1.2883   0.02260   0.01676  -0.0420   0.2707   0.8910
  11.000   1.2906   0.02406   0.01821  -0.0399   0.2564   0.8924
  11.250   1.2943   0.02550   0.01965  -0.0380   0.2441   0.8938
  11.500   1.2970   0.02708   0.02120  -0.0362   0.2311   0.8952
  11.750   1.2987   0.02879   0.02289  -0.0344   0.2172   0.8966
  12.000   1.3008   0.03054   0.02461  -0.0329   0.2038   0.8981
  12.250   1.3031   0.03236   0.02641  -0.0314   0.1905   0.8995
  12.500   1.3052   0.03426   0.02828  -0.0301   0.1773   0.9009
  12.750   1.3064   0.03628   0.03026  -0.0289   0.1630   0.9023
  13.000   1.3076   0.03830   0.03225  -0.0276   0.1493   0.9036
  13.250   1.3102   0.04025   0.03419  -0.0266   0.1375   0.9051
  13.500   1.3147   0.04208   0.03603  -0.0257   0.1277   0.9067
  13.750   1.3166   0.04418   0.03812  -0.0248   0.1168   0.9083
  14.000   1.3196   0.04625   0.04019  -0.0240   0.1079   0.9101
  14.250   1.3223   0.04839   0.04234  -0.0233   0.0986   0.9122
  14.500   1.3268   0.05043   0.04440  -0.0227   0.0909   0.9142
  14.750   1.3284   0.05280   0.04677  -0.0222   0.0822   0.9163
  15.250   1.3321   0.05762   0.05161  -0.0214   0.0661   0.9206
  15.500   1.3329   0.06026   0.05427  -0.0211   0.0584   0.9231
  15.750   1.3350   0.06281   0.05684  -0.0210   0.0521   0.9258
  16.000   1.3354   0.06564   0.05969  -0.0210   0.0460   0.9287
  16.500   1.3397   0.07113   0.06526  -0.0213   0.0367   0.9359
  16.750   1.3410   0.07405   0.06823  -0.0217   0.0331   0.9410
  17.250   1.3452   0.08017   0.07450  -0.0231   0.0264   0.9576
  17.500   1.3442   0.08338   0.07776  -0.0237   0.0234   1.0000
  17.750   1.3438   0.08678   0.08121  -0.0245   0.0203   1.0000
  18.000   1.3441   0.09011   0.08461  -0.0253   0.0184   1.0000
  18.250   1.3426   0.09373   0.08827  -0.0263   0.0161   1.0000
  18.500   1.3427   0.09719   0.09181  -0.0273   0.0146   1.0000
  18.750   1.3407   0.10097   0.09565  -0.0285   0.0129   1.0000
  19.000   1.3393   0.10472   0.09946  -0.0297   0.0113   1.0000
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