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EPPLER 583 AIRFOIL (e583-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: EPPLER 583 AIRFOIL (e583-il)
Reynolds number: 1,000,000
Max Cl/Cd: 132.03 at α=5.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-e583-il-1000000-n5.txt
Download as CSV file: xf-e583-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: EPPLER 583 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
  ------ -------- --------- --------- -------- -------- --------
 -12.500  -0.3921   0.04281   0.03947  -0.1376   0.7233   0.0027
 -12.250  -0.4489   0.03531   0.03161  -0.1377   0.7174   0.0027
 -12.000  -0.4679   0.03217   0.02825  -0.1357   0.7124   0.0027
 -11.750  -0.4751   0.03012   0.02604  -0.1336   0.7073   0.0027
 -11.500  -0.4827   0.02814   0.02388  -0.1308   0.7022   0.0027
 -11.250  -0.4991   0.02557   0.02100  -0.1265   0.6977   0.0028
 -11.000  -0.4997   0.02421   0.01949  -0.1234   0.6935   0.0028
 -10.750  -0.4981   0.02316   0.01829  -0.1200   0.6891   0.0028
 -10.500  -0.4920   0.02199   0.01693  -0.1173   0.6848   0.0028
 -10.250  -0.4815   0.02088   0.01565  -0.1153   0.6812   0.0028
 -10.000  -0.4677   0.01988   0.01450  -0.1136   0.6781   0.0029
  -9.750  -0.4521   0.01898   0.01346  -0.1121   0.6748   0.0029
  -9.500  -0.4353   0.01813   0.01246  -0.1108   0.6716   0.0029
  -9.250  -0.4162   0.01749   0.01170  -0.1097   0.6684   0.0029
  -9.000  -0.3965   0.01685   0.01094  -0.1087   0.6656   0.0030
  -8.750  -0.3755   0.01626   0.01027  -0.1079   0.6632   0.0030
  -8.500  -0.3542   0.01567   0.00958  -0.1071   0.6604   0.0030
  -8.250  -0.3338   0.01495   0.00875  -0.1061   0.6575   0.0032
  -8.000  -0.3123   0.01438   0.00808  -0.1053   0.6545   0.0032
  -7.750  -0.2904   0.01385   0.00747  -0.1046   0.6518   0.0034
  -7.500  -0.2667   0.01349   0.00706  -0.1041   0.6494   0.0035
  -7.250  -0.2425   0.01311   0.00664  -0.1036   0.6475   0.0037
  -7.000  -0.2178   0.01280   0.00629  -0.1033   0.6454   0.0039
  -6.750  -0.1933   0.01245   0.00590  -0.1029   0.6431   0.0039
  -6.500  -0.1682   0.01219   0.00560  -0.1026   0.6406   0.0042
  -6.250  -0.1433   0.01191   0.00527  -0.1023   0.6382   0.0044
  -6.000  -0.1184   0.01164   0.00495  -0.1019   0.6358   0.0045
  -5.500  -0.0672   0.01116   0.00441  -0.1014   0.6319   0.0048
  -5.250  -0.0413   0.01091   0.00412  -0.1012   0.6299   0.0049
  -5.000  -0.0155   0.01066   0.00385  -0.1010   0.6277   0.0053
  -4.750   0.0107   0.01045   0.00363  -0.1009   0.6255   0.0057
  -4.500   0.0370   0.01028   0.00343  -0.1008   0.6232   0.0061
  -4.250   0.0634   0.01012   0.00324  -0.1007   0.6210   0.0067
  -4.000   0.0897   0.00996   0.00307  -0.1005   0.6187   0.0081
  -3.750   0.1164   0.00980   0.00291  -0.1005   0.6168   0.0104
  -3.500   0.1433   0.00961   0.00275  -0.1005   0.6150   0.0158
  -3.250   0.1702   0.00944   0.00261  -0.1005   0.6130   0.0248
  -3.000   0.1972   0.00928   0.00249  -0.1006   0.6109   0.0364
  -2.750   0.2240   0.00910   0.00238  -0.1006   0.6087   0.0537
  -2.500   0.2503   0.00887   0.00228  -0.1006   0.6066   0.0889
  -2.250   0.2767   0.00865   0.00218  -0.1006   0.6044   0.1311
  -2.000   0.3024   0.00835   0.00209  -0.1006   0.6021   0.2008
  -1.750   0.3290   0.00804   0.00201  -0.1008   0.6003   0.2747
  -1.500   0.3558   0.00769   0.00192  -0.1010   0.5983   0.3607
  -1.250   0.3821   0.00719   0.00182  -0.1013   0.5961   0.4919
  -1.000   0.4081   0.00659   0.00175  -0.1016   0.5937   0.6624
  -0.750   0.4360   0.00654   0.00181  -0.1017   0.5913   0.7140
  -0.500   0.4643   0.00658   0.00184  -0.1019   0.5887   0.7303
  -0.250   0.4926   0.00664   0.00186  -0.1021   0.5863   0.7413
   0.000   0.5212   0.00668   0.00192  -0.1024   0.5842   0.7562
   0.250   0.5496   0.00676   0.00202  -0.1025   0.5818   0.7725
   0.500   0.5775   0.00683   0.00211  -0.1026   0.5791   0.7821
   0.750   0.6060   0.00688   0.00214  -0.1029   0.5764   0.7850
   1.000   0.6343   0.00692   0.00215  -0.1032   0.5735   0.7866
   1.250   0.6623   0.00698   0.00217  -0.1034   0.5707   0.7881
   1.500   0.6911   0.00702   0.00219  -0.1038   0.5681   0.7892
   1.750   0.7197   0.00705   0.00222  -0.1042   0.5648   0.7903
   2.000   0.7477   0.00708   0.00225  -0.1044   0.5613   0.7918
   2.250   0.7750   0.00714   0.00229  -0.1045   0.5571   0.7932
   2.500   0.8025   0.00720   0.00234  -0.1047   0.5533   0.7945
   2.750   0.8306   0.00724   0.00239  -0.1049   0.5490   0.7957
   3.000   0.8579   0.00730   0.00244  -0.1051   0.5439   0.7970
   3.250   0.8845   0.00739   0.00250  -0.1051   0.5389   0.7983
   3.500   0.9121   0.00745   0.00257  -0.1053   0.5337   0.7996
   3.750   0.9387   0.00753   0.00264  -0.1053   0.5274   0.8010
   4.000   0.9651   0.00763   0.00272  -0.1052   0.5215   0.8026
   4.250   0.9915   0.00772   0.00281  -0.1052   0.5142   0.8041
   4.500   1.0167   0.00784   0.00291  -0.1050   0.5064   0.8055
   4.750   1.0421   0.00797   0.00301  -0.1048   0.4976   0.8066
   5.000   1.0665   0.00810   0.00313  -0.1044   0.4888   0.8080
   5.500   1.1130   0.00843   0.00343  -0.1032   0.4678   0.8109
   5.750   1.1354   0.00862   0.00360  -0.1024   0.4574   0.8124
   6.000   1.1564   0.00885   0.00380  -0.1014   0.4461   0.8141
   6.250   1.1765   0.00908   0.00400  -0.1003   0.4337   0.8158
   6.500   1.1942   0.00932   0.00420  -0.0986   0.4203   0.8179
   6.750   1.2113   0.00957   0.00443  -0.0968   0.4079   0.8199
   7.000   1.2275   0.00988   0.00470  -0.0949   0.3951   0.8217
   7.500   1.2569   0.01059   0.00533  -0.0907   0.3677   0.8254
   7.750   1.2702   0.01099   0.00571  -0.0884   0.3534   0.8274
   8.000   1.2820   0.01145   0.00613  -0.0859   0.3379   0.8296
   8.250   1.2916   0.01199   0.00662  -0.0831   0.3203   0.8320
   8.500   1.3001   0.01260   0.00717  -0.0802   0.3033   0.8346
   8.750   1.3086   0.01325   0.00777  -0.0775   0.2881   0.8371
   9.250   1.3241   0.01470   0.00916  -0.0721   0.2610   0.8425
   9.500   1.3296   0.01559   0.01002  -0.0693   0.2463   0.8454
   9.750   1.3346   0.01658   0.01098  -0.0667   0.2318   0.8485
  10.000   1.3410   0.01759   0.01196  -0.0643   0.2191   0.8516
  10.250   1.3468   0.01869   0.01304  -0.0621   0.2061   0.8545
  10.500   1.3509   0.01993   0.01425  -0.0598   0.1922   0.8575
  10.750   1.3536   0.02130   0.01559  -0.0574   0.1778   0.8611
  11.000   1.3565   0.02274   0.01700  -0.0553   0.1639   0.8649
  11.250   1.3582   0.02432   0.01853  -0.0531   0.1496   0.8688
  11.500   1.3592   0.02600   0.02016  -0.0511   0.1350   0.8728
  11.750   1.3635   0.02749   0.02166  -0.0494   0.1247   0.8776
  12.000   1.3647   0.02926   0.02339  -0.0475   0.1118   0.8828
  12.500   1.3711   0.03264   0.02677  -0.0445   0.0918   0.8939
  12.750   1.3687   0.03484   0.02891  -0.0428   0.0768   0.9011
  13.000   1.3743   0.03642   0.03054  -0.0416   0.0722   0.9100
  13.250   1.3761   0.03829   0.03243  -0.0401   0.0631   0.9239
  13.500   1.3796   0.04051   0.03469  -0.0397   0.0529   0.9583
  14.000   1.3832   0.04515   0.03926  -0.0384   0.0345   1.0000
  14.250   1.3847   0.04754   0.04163  -0.0377   0.0278   1.0000
  14.500   1.3916   0.04944   0.04355  -0.0373   0.0255   1.0000
  14.750   1.3949   0.05173   0.04586  -0.0369   0.0217   1.0000
  15.250   1.4031   0.05633   0.05050  -0.0363   0.0155   1.0000
  15.500   1.4087   0.05852   0.05273  -0.0362   0.0139   1.0000
  15.750   1.4119   0.06101   0.05525  -0.0361   0.0120   1.0000
  16.000   1.4172   0.06332   0.05761  -0.0360   0.0107   1.0000
  16.250   1.4207   0.06588   0.06021  -0.0361   0.0095   1.0000
  16.500   1.4245   0.06844   0.06282  -0.0362   0.0082   1.0000
  16.750   1.4274   0.07116   0.06559  -0.0364   0.0072   1.0000
  17.000   1.4312   0.07380   0.06829  -0.0367   0.0065   1.0000
  17.250   1.4333   0.07669   0.07123  -0.0371   0.0056   1.0000
  17.500   1.4349   0.07972   0.07432  -0.0375   0.0047   1.0000
  17.750   1.4372   0.08268   0.07734  -0.0380   0.0043   1.0000
  18.000   1.4391   0.08577   0.08050  -0.0387   0.0039   1.0000
  18.250   1.4392   0.08910   0.08389  -0.0394   0.0032   1.0000
  18.500   1.4397   0.09244   0.08730  -0.0402   0.0028   1.0000
  18.750   1.4398   0.09588   0.09081  -0.0411   0.0026   1.0000
  19.000   1.4394   0.09943   0.09443  -0.0421   0.0022   1.0000
  19.250   1.4385   0.10310   0.09818  -0.0433   0.0020   1.0000
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