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EPPLER 603 AIRFOIL (e603-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: EPPLER 603 AIRFOIL (e603-il)
Reynolds number: 500,000
Max Cl/Cd: 103.6 at α=8.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-e603-il-500000.txt
Download as CSV file: xf-e603-il-500000.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 =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.500  -0.3276   0.07616   0.07297  -0.0992   0.7946   0.0165
 -14.250  -0.4257   0.08208   0.07954  -0.0926   0.9397   0.0164
 -14.000  -0.4455   0.06735   0.06451  -0.1095   0.9184   0.0160
 -13.750  -0.4648   0.05633   0.05288  -0.1225   0.8638   0.0159
 -13.500  -0.4937   0.05132   0.04742  -0.1231   0.8198   0.0156
 -13.250  -0.5127   0.04783   0.04363  -0.1225   0.7973   0.0156
 -13.000  -0.5358   0.04390   0.03938  -0.1214   0.7825   0.0153
 -12.750  -0.5559   0.04039   0.03554  -0.1196   0.7711   0.0152
 -12.500  -0.5669   0.03769   0.03256  -0.1177   0.7611   0.0152
 -12.250  -0.5748   0.03504   0.02960  -0.1157   0.7532   0.0151
 -12.000  -0.5753   0.03301   0.02733  -0.1139   0.7457   0.0151
 -11.750  -0.5721   0.03124   0.02531  -0.1121   0.7396   0.0153
 -11.500  -0.5644   0.02968   0.02357  -0.1107   0.7339   0.0154
 -11.250  -0.5547   0.02835   0.02205  -0.1092   0.7284   0.0157
 -11.000  -0.5417   0.02710   0.02059  -0.1080   0.7235   0.0159
 -10.750  -0.5271   0.02602   0.01936  -0.1069   0.7190   0.0162
 -10.500  -0.5113   0.02504   0.01822  -0.1058   0.7146   0.0165
 -10.250  -0.4939   0.02420   0.01723  -0.1049   0.7106   0.0167
 -10.000  -0.4718   0.02305   0.01596  -0.1044   0.7071   0.0171
  -9.750  -0.4519   0.02219   0.01507  -0.1037   0.7040   0.0174
  -9.500  -0.4336   0.02148   0.01435  -0.1029   0.7007   0.0179
  -9.250  -0.4153   0.02088   0.01371  -0.1020   0.6975   0.0184
  -9.000  -0.3969   0.02032   0.01309  -0.1011   0.6945   0.0192
  -8.750  -0.3781   0.01981   0.01248  -0.1001   0.6917   0.0200
  -8.500  -0.3604   0.01920   0.01179  -0.0991   0.6888   0.0207
  -8.250  -0.3450   0.01847   0.01110  -0.0978   0.6863   0.0216
  -8.000  -0.3278   0.01795   0.01056  -0.0966   0.6835   0.0225
  -7.750  -0.3105   0.01744   0.01002  -0.0954   0.6810   0.0236
  -7.500  -0.2943   0.01692   0.00944  -0.0940   0.6786   0.0246
  -7.250  -0.2815   0.01629   0.00881  -0.0922   0.6764   0.0263
  -7.000  -0.2659   0.01592   0.00839  -0.0906   0.6741   0.0281
  -6.750  -0.2544   0.01549   0.00793  -0.0884   0.6719   0.0306
  -6.500  -0.2376   0.01515   0.00759  -0.0870   0.6701   0.0341
  -6.250  -0.2208   0.01469   0.00717  -0.0857   0.6680   0.0394
  -6.000  -0.2023   0.01428   0.00679  -0.0846   0.6658   0.0473
  -5.750  -0.1834   0.01385   0.00643  -0.0836   0.6635   0.0608
  -5.500  -0.1635   0.01344   0.00611  -0.0828   0.6616   0.0823
  -5.250  -0.1430   0.01303   0.00583  -0.0821   0.6598   0.1113
  -5.000  -0.1222   0.01259   0.00555  -0.0816   0.6580   0.1531
  -4.750  -0.1021   0.01205   0.00527  -0.0811   0.6561   0.2177
  -4.250  -0.0641   0.00993   0.00431  -0.0809   0.6525   0.4896
  -4.000  -0.0388   0.00955   0.00449  -0.0808   0.6506   0.6315
  -3.750  -0.0093   0.00974   0.00467  -0.0811   0.6488   0.6610
  -3.500   0.0205   0.00997   0.00484  -0.0814   0.6470   0.6782
  -3.250   0.0495   0.01033   0.00517  -0.0814   0.6451   0.6899
  -3.000   0.0789   0.01057   0.00535  -0.0816   0.6433   0.6982
  -2.750   0.1077   0.01087   0.00561  -0.0816   0.6416   0.7037
  -2.500   0.1377   0.01110   0.00574  -0.0821   0.6399   0.7105
  -2.250   0.1659   0.01141   0.00604  -0.0820   0.6382   0.7150
  -2.000   0.1930   0.01177   0.00644  -0.0815   0.6365   0.7200
  -1.750   0.2220   0.01207   0.00669  -0.0817   0.6347   0.7281
  -1.500   0.2478   0.01243   0.00711  -0.0807   0.6329   0.7322
  -1.250   0.2741   0.01285   0.00755  -0.0799   0.6310   0.7362
  -1.000   0.3020   0.01308   0.00775  -0.0798   0.6291   0.7410
  -0.750   0.3336   0.01304   0.00762  -0.0812   0.6272   0.7455
  -0.500   0.3617   0.01300   0.00755  -0.0814   0.6256   0.7468
  -0.250   0.3904   0.01304   0.00755  -0.0817   0.6238   0.7480
   0.000   0.4191   0.01316   0.00763  -0.0821   0.6218   0.7491
   0.250   0.4467   0.01315   0.00765  -0.0823   0.6202   0.7505
   0.500   0.4745   0.01315   0.00765  -0.0825   0.6182   0.7518
   0.750   0.5030   0.01313   0.00763  -0.0830   0.6161   0.7532
   1.000   0.5318   0.01312   0.00761  -0.0835   0.6139   0.7548
   1.250   0.5613   0.01310   0.00757  -0.0842   0.6119   0.7567
   1.500   0.5916   0.01305   0.00749  -0.0851   0.6099   0.7584
   1.750   0.6226   0.01303   0.00741  -0.0862   0.6080   0.7601
   2.000   0.6541   0.01313   0.00745  -0.0874   0.6058   0.7618
   2.250   0.6814   0.01306   0.00743  -0.0877   0.6037   0.7631
   2.500   0.7084   0.01303   0.00744  -0.0878   0.6013   0.7641
   2.750   0.7362   0.01300   0.00744  -0.0881   0.5987   0.7650
   3.000   0.7645   0.01298   0.00744  -0.0885   0.5962   0.7660
   3.250   0.7936   0.01297   0.00742  -0.0890   0.5938   0.7670
   3.500   0.8231   0.01298   0.00740  -0.0896   0.5915   0.7681
   3.750   0.8523   0.01309   0.00750  -0.0902   0.5888   0.7694
   4.000   0.8785   0.01306   0.00755  -0.0902   0.5859   0.7709
   4.250   0.9060   0.01302   0.00755  -0.0905   0.5826   0.7722
   4.500   0.9347   0.01295   0.00749  -0.0910   0.5792   0.7734
   4.750   0.9645   0.01289   0.00742  -0.0918   0.5760   0.7747
   5.000   0.9943   0.01293   0.00743  -0.0925   0.5727   0.7759
   5.250   1.0203   0.01288   0.00747  -0.0926   0.5687   0.7773
   5.500   1.0482   0.01285   0.00746  -0.0930   0.5646   0.7786
   5.750   1.0757   0.01275   0.00738  -0.0932   0.5608   0.7797
   6.000   1.1042   0.01274   0.00735  -0.0936   0.5570   0.7807
   6.250   1.1276   0.01269   0.00743  -0.0931   0.5522   0.7817
   6.500   1.1530   0.01264   0.00742  -0.0929   0.5472   0.7827
   6.750   1.1799   0.01262   0.00740  -0.0930   0.5427   0.7837
   7.000   1.2035   0.01262   0.00750  -0.0926   0.5369   0.7849
   7.250   1.2276   0.01261   0.00754  -0.0922   0.5307   0.7861
   7.500   1.2520   0.01263   0.00758  -0.0918   0.5244   0.7876
   7.750   1.2743   0.01265   0.00768  -0.0911   0.5163   0.7892
   8.000   1.2968   0.01271   0.00775  -0.0905   0.5083   0.7905
   8.250   1.3177   0.01278   0.00787  -0.0896   0.4984   0.7919
   8.500   1.3375   0.01291   0.00802  -0.0885   0.4877   0.7932
   8.750   1.3543   0.01308   0.00819  -0.0868   0.4761   0.7944
   9.000   1.3655   0.01329   0.00838  -0.0841   0.4629   0.7957
   9.250   1.3749   0.01362   0.00870  -0.0812   0.4486   0.7971
   9.500   1.3825   0.01409   0.00915  -0.0781   0.4324   0.7986
   9.750   1.3882   0.01468   0.00972  -0.0749   0.4152   0.8003
  10.000   1.3923   0.01541   0.01042  -0.0716   0.3980   0.8020
  10.250   1.3935   0.01632   0.01129  -0.0681   0.3799   0.8037
  10.500   1.3923   0.01746   0.01239  -0.0647   0.3617   0.8055
  10.750   1.3892   0.01886   0.01375  -0.0614   0.3436   0.8073
  11.000   1.3851   0.02051   0.01534  -0.0584   0.3260   0.8090
  11.250   1.3800   0.02241   0.01717  -0.0557   0.3076   0.8105
  11.500   1.3758   0.02438   0.01910  -0.0533   0.2895   0.8120
  11.750   1.3700   0.02654   0.02121  -0.0510   0.2711   0.8136
  12.000   1.3644   0.02879   0.02341  -0.0488   0.2535   0.8154
  12.250   1.3585   0.03115   0.02573  -0.0469   0.2363   0.8172
  12.500   1.3549   0.03345   0.02798  -0.0452   0.2206   0.8190
  12.750   1.3527   0.03573   0.03022  -0.0438   0.2056   0.8206
  13.000   1.3520   0.03797   0.03242  -0.0426   0.1915   0.8223
  13.250   1.3527   0.04018   0.03461  -0.0417   0.1791   0.8239
  13.500   1.3540   0.04243   0.03683  -0.0409   0.1672   0.8255
  13.750   1.3548   0.04477   0.03913  -0.0402   0.1552   0.8270
  14.000   1.3557   0.04715   0.04148  -0.0395   0.1441   0.8285
  14.250   1.3592   0.04930   0.04364  -0.0390   0.1333   0.8302
  14.500   1.3616   0.05164   0.04599  -0.0385   0.1235   0.8319
  14.750   1.3637   0.05405   0.04839  -0.0382   0.1144   0.8336
  15.000   1.3655   0.05658   0.05091  -0.0379   0.1052   0.8354
  15.250   1.3700   0.05888   0.05323  -0.0378   0.0974   0.8373
  15.500   1.3712   0.06160   0.05594  -0.0377   0.0897   0.8393
  15.750   1.3742   0.06415   0.05849  -0.0377   0.0822   0.8414
  16.000   1.3774   0.06679   0.06116  -0.0378   0.0761   0.8434
  16.250   1.3784   0.06964   0.06402  -0.0379   0.0696   0.8455
  16.500   1.3817   0.07228   0.06673  -0.0381   0.0642   0.8477
  16.750   1.3815   0.07542   0.06987  -0.0384   0.0585   0.8498
  17.000   1.3845   0.07822   0.07273  -0.0388   0.0537   0.8521
  17.250   1.3845   0.08146   0.07599  -0.0394   0.0487   0.8545
  17.500   1.3845   0.08479   0.07935  -0.0400   0.0440   0.8569
  17.750   1.3846   0.08817   0.08277  -0.0407   0.0395   0.8592
  18.000   1.3808   0.09204   0.08667  -0.0416   0.0355   0.8615
  18.250   1.3803   0.09554   0.09026  -0.0424   0.0320   0.8642
  18.500   1.3754   0.09974   0.09450  -0.0435   0.0290   0.8668
  18.750   1.3744   0.10346   0.09831  -0.0447   0.0266   0.8700
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