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EPPLER 603 AIRFOIL (e603-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: EPPLER 603 AIRFOIL (e603-il)
Reynolds number: 1,000,000
Max Cl/Cd: 127.81 at α=6°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-e603-il-1000000-n5.txt
Download as CSV file: xf-e603-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: EPPLER 603 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
  ------ -------- --------- --------- -------- -------- --------
 -18.750  -0.6606   0.12181   0.11945  -0.0566   1.0000   0.0055
 -18.500  -0.7187   0.10671   0.10415  -0.0641   1.0000   0.0055
 -18.250  -0.7567   0.09576   0.09305  -0.0698   1.0000   0.0054
 -18.000  -0.7999   0.08365   0.08074  -0.0767   0.9998   0.0054
 -17.750  -0.8276   0.07529   0.07223  -0.0806   0.9914   0.0053
 -17.500  -0.8300   0.06584   0.06255  -0.0917   0.9623   0.0054
 -17.250  -0.7976   0.05686   0.05326  -0.1091   0.9326   0.0054
 -17.000  -0.7836   0.05159   0.04735  -0.1173   0.8255   0.0055
 -16.750  -0.7918   0.04835   0.04386  -0.1176   0.7920   0.0055
 -16.500  -0.7928   0.04584   0.04118  -0.1179   0.7713   0.0055
 -16.000  -0.7932   0.04110   0.03615  -0.1181   0.7437   0.0056
 -15.750  -0.7948   0.03877   0.03368  -0.1178   0.7337   0.0056
 -15.500  -0.7892   0.03714   0.03193  -0.1175   0.7241   0.0057
 -15.250  -0.7841   0.03551   0.03019  -0.1171   0.7165   0.0057
 -15.000  -0.7825   0.03367   0.02824  -0.1163   0.7091   0.0058
 -14.750  -0.7721   0.03258   0.02705  -0.1158   0.7024   0.0058
 -14.500  -0.7641   0.03133   0.02572  -0.1151   0.6966   0.0058
 -14.250  -0.7617   0.02973   0.02401  -0.1139   0.6903   0.0059
 -14.000  -0.7566   0.02838   0.02256  -0.1128   0.6849   0.0061
 -13.750  -0.7484   0.02723   0.02133  -0.1118   0.6803   0.0062
 -13.500  -0.7401   0.02612   0.02013  -0.1106   0.6751   0.0062
 -13.250  -0.7284   0.02526   0.01920  -0.1097   0.6707   0.0063
 -13.000  -0.7168   0.02437   0.01825  -0.1086   0.6671   0.0064
 -12.750  -0.7033   0.02361   0.01744  -0.1077   0.6637   0.0065
 -12.500  -0.6903   0.02282   0.01659  -0.1066   0.6600   0.0066
 -12.250  -0.6758   0.02215   0.01586  -0.1057   0.6566   0.0067
 -12.000  -0.6614   0.02149   0.01514  -0.1046   0.6532   0.0069
 -11.750  -0.6465   0.02083   0.01443  -0.1036   0.6506   0.0069
 -11.500  -0.6306   0.02023   0.01378  -0.1026   0.6480   0.0071
 -11.250  -0.6140   0.01969   0.01319  -0.1017   0.6454   0.0073
 -11.000  -0.5983   0.01909   0.01254  -0.1006   0.6427   0.0074
 -10.750  -0.5823   0.01853   0.01192  -0.0995   0.6399   0.0074
 -10.500  -0.5645   0.01809   0.01144  -0.0986   0.6371   0.0076
 -10.250  -0.5470   0.01763   0.01093  -0.0977   0.6347   0.0077
 -10.000  -0.5290   0.01717   0.01043  -0.0967   0.6327   0.0079
  -9.750  -0.5119   0.01666   0.00988  -0.0956   0.6307   0.0081
  -9.500  -0.4947   0.01617   0.00937  -0.0945   0.6287   0.0083
  -9.250  -0.4768   0.01574   0.00891  -0.0935   0.6267   0.0085
  -9.000  -0.4587   0.01533   0.00848  -0.0924   0.6247   0.0090
  -8.750  -0.4406   0.01494   0.00806  -0.0913   0.6227   0.0091
  -8.500  -0.4224   0.01458   0.00767  -0.0902   0.6208   0.0095
  -8.000  -0.3867   0.01392   0.00695  -0.0877   0.6174   0.0102
  -7.750  -0.3716   0.01360   0.00662  -0.0860   0.6161   0.0108
  -7.500  -0.3551   0.01331   0.00633  -0.0845   0.6144   0.0115
  -7.250  -0.3348   0.01302   0.00603  -0.0837   0.6127   0.0123
  -7.000  -0.3132   0.01276   0.00574  -0.0830   0.6109   0.0131
  -6.750  -0.2914   0.01249   0.00547  -0.0824   0.6093   0.0147
  -6.500  -0.2685   0.01226   0.00523  -0.0819   0.6078   0.0163
  -6.250  -0.2454   0.01202   0.00499  -0.0815   0.6062   0.0186
  -6.000  -0.2217   0.01180   0.00477  -0.0811   0.6047   0.0212
  -5.750  -0.1974   0.01161   0.00456  -0.0808   0.6031   0.0241
  -5.500  -0.1731   0.01139   0.00436  -0.0806   0.6015   0.0289
  -5.250  -0.1480   0.01116   0.00416  -0.0804   0.6004   0.0349
  -5.000  -0.1227   0.01092   0.00397  -0.0804   0.5991   0.0438
  -4.750  -0.0970   0.01070   0.00379  -0.0804   0.5978   0.0543
  -4.500  -0.0709   0.01048   0.00362  -0.0804   0.5965   0.0662
  -4.250  -0.0450   0.01023   0.00345  -0.0805   0.5951   0.0847
  -4.000  -0.0192   0.00994   0.00327  -0.0806   0.5936   0.1128
  -3.750   0.0068   0.00963   0.00309  -0.0808   0.5919   0.1494
  -3.500   0.0333   0.00930   0.00291  -0.0811   0.5904   0.1922
  -3.250   0.0601   0.00896   0.00274  -0.0815   0.5890   0.2435
  -3.000   0.0869   0.00844   0.00251  -0.0821   0.5874   0.3288
  -2.750   0.1146   0.00762   0.00217  -0.0833   0.5856   0.4677
  -2.500   0.1447   0.00700   0.00196  -0.0846   0.5844   0.5858
  -2.250   0.1748   0.00690   0.00197  -0.0853   0.5833   0.6274
  -2.000   0.2049   0.00691   0.00199  -0.0859   0.5820   0.6451
  -1.750   0.2349   0.00693   0.00203  -0.0865   0.5805   0.6592
  -1.500   0.2648   0.00698   0.00208  -0.0870   0.5790   0.6705
  -1.250   0.2947   0.00705   0.00213  -0.0875   0.5774   0.6806
  -1.000   0.3243   0.00716   0.00223  -0.0880   0.5758   0.6892
  -0.750   0.3542   0.00724   0.00228  -0.0885   0.5741   0.6947
  -0.500   0.3835   0.00728   0.00231  -0.0890   0.5725   0.6973
  -0.250   0.4129   0.00732   0.00232  -0.0895   0.5707   0.6983
   0.000   0.4423   0.00737   0.00233  -0.0900   0.5688   0.6993
   0.250   0.4721   0.00738   0.00235  -0.0906   0.5675   0.7004
   0.500   0.5018   0.00740   0.00237  -0.0911   0.5660   0.7016
   0.750   0.5315   0.00742   0.00239  -0.0917   0.5642   0.7026
   1.000   0.5611   0.00745   0.00240  -0.0923   0.5623   0.7036
   1.250   0.5905   0.00748   0.00242  -0.0928   0.5602   0.7046
   1.500   0.6198   0.00751   0.00245  -0.0933   0.5581   0.7057
   1.750   0.6489   0.00756   0.00247  -0.0938   0.5559   0.7068
   2.000   0.6778   0.00762   0.00250  -0.0942   0.5536   0.7078
   2.250   0.7072   0.00765   0.00254  -0.0948   0.5516   0.7087
   2.500   0.7367   0.00767   0.00258  -0.0954   0.5492   0.7094
   2.750   0.7659   0.00771   0.00262  -0.0959   0.5465   0.7101
   3.000   0.7949   0.00775   0.00266  -0.0963   0.5435   0.7108
   3.250   0.8233   0.00779   0.00270  -0.0967   0.5403   0.7120
   3.500   0.8514   0.00784   0.00275  -0.0970   0.5367   0.7131
   3.750   0.8803   0.00787   0.00282  -0.0975   0.5327   0.7140
   4.000   0.9086   0.00792   0.00287  -0.0978   0.5278   0.7149
   4.250   0.9360   0.00799   0.00294  -0.0980   0.5228   0.7157
   4.500   0.9643   0.00805   0.00302  -0.0984   0.5180   0.7165
   4.750   0.9920   0.00812   0.00310  -0.0986   0.5117   0.7174
   5.000   1.0188   0.00822   0.00319  -0.0987   0.5052   0.7183
   5.250   1.0460   0.00832   0.00329  -0.0989   0.4970   0.7193
   5.500   1.0719   0.00845   0.00341  -0.0988   0.4882   0.7204
   5.750   1.0971   0.00861   0.00354  -0.0987   0.4773   0.7214
   6.000   1.1222   0.00878   0.00369  -0.0984   0.4658   0.7223
   6.250   1.1461   0.00898   0.00387  -0.0980   0.4536   0.7232
   6.500   1.1685   0.00924   0.00408  -0.0974   0.4393   0.7241
   6.750   1.1896   0.00954   0.00432  -0.0965   0.4229   0.7250
   7.000   1.2091   0.00988   0.00459  -0.0953   0.4051   0.7258
   7.250   1.2262   0.01028   0.00492  -0.0937   0.3856   0.7266
   7.500   1.2409   0.01069   0.00525  -0.0917   0.3676   0.7274
   7.750   1.2517   0.01110   0.00560  -0.0889   0.3492   0.7285
   8.000   1.2624   0.01158   0.00602  -0.0861   0.3314   0.7299
   8.250   1.2708   0.01216   0.00654  -0.0831   0.3117   0.7311
   8.500   1.2781   0.01280   0.00712  -0.0801   0.2928   0.7322
   8.750   1.2837   0.01353   0.00778  -0.0769   0.2748   0.7334
   9.000   1.2880   0.01437   0.00855  -0.0737   0.2576   0.7345
   9.250   1.2910   0.01533   0.00945  -0.0706   0.2404   0.7357
   9.500   1.2937   0.01641   0.01049  -0.0677   0.2245   0.7368
   9.750   1.2997   0.01746   0.01152  -0.0654   0.2130   0.7379
  10.000   1.3024   0.01877   0.01279  -0.0630   0.1988   0.7391
  10.250   1.3081   0.02003   0.01403  -0.0611   0.1880   0.7402
  10.500   1.3094   0.02162   0.01557  -0.0590   0.1736   0.7414
  10.750   1.3091   0.02342   0.01731  -0.0569   0.1580   0.7426
  11.000   1.3141   0.02493   0.01881  -0.0554   0.1488   0.7436
  11.250   1.3154   0.02674   0.02057  -0.0537   0.1361   0.7445
  11.500   1.3175   0.02853   0.02232  -0.0521   0.1250   0.7454
  11.750   1.3218   0.03020   0.02398  -0.0508   0.1151   0.7466
  12.000   1.3261   0.03191   0.02568  -0.0496   0.1061   0.7478
  12.250   1.3287   0.03380   0.02755  -0.0484   0.0966   0.7489
  12.500   1.3324   0.03566   0.02939  -0.0473   0.0881   0.7500
  12.750   1.3385   0.03737   0.03111  -0.0465   0.0811   0.7511
  13.000   1.3433   0.03924   0.03297  -0.0457   0.0747   0.7522
  13.250   1.3501   0.04099   0.03473  -0.0450   0.0689   0.7533
  13.500   1.3558   0.04287   0.03661  -0.0444   0.0636   0.7544
  13.750   1.3627   0.04467   0.03844  -0.0439   0.0589   0.7555
  14.000   1.3689   0.04659   0.04036  -0.0434   0.0542   0.7566
  14.250   1.3731   0.04874   0.04250  -0.0429   0.0485   0.7577
  14.500   1.3814   0.05053   0.04432  -0.0426   0.0454   0.7588
  14.750   1.3850   0.05282   0.04661  -0.0423   0.0406   0.7597
  15.000   1.3923   0.05477   0.04858  -0.0421   0.0374   0.7608
  15.250   1.3972   0.05703   0.05085  -0.0419   0.0341   0.7618
  15.500   1.4034   0.05917   0.05303  -0.0418   0.0312   0.7631
  15.750   1.4081   0.06150   0.05538  -0.0418   0.0281   0.7645
  16.000   1.4130   0.06386   0.05779  -0.0418   0.0253   0.7658
  16.250   1.4177   0.06627   0.06022  -0.0419   0.0226   0.7670
  16.500   1.4209   0.06893   0.06292  -0.0420   0.0202   0.7683
  16.750   1.4252   0.07148   0.06551  -0.0422   0.0178   0.7696
  17.000   1.4273   0.07435   0.06842  -0.0425   0.0158   0.7708
  17.250   1.4314   0.07700   0.07112  -0.0429   0.0143   0.7721
  17.500   1.4336   0.07997   0.07413  -0.0434   0.0131   0.7734
  17.750   1.4380   0.08267   0.07689  -0.0439   0.0123   0.7747
  18.000   1.4401   0.08573   0.08000  -0.0445   0.0114   0.7759
  18.250   1.4425   0.08876   0.08308  -0.0451   0.0107   0.7771
  18.500   1.4447   0.09186   0.08625  -0.0459   0.0101   0.7782
  19.000   1.4490   0.09820   0.09274  -0.0477   0.0093   0.7810
  19.250   1.4505   0.10150   0.09612  -0.0487   0.0089   0.7825
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