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EPPLER 604 AIRFOIL (e604-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: EPPLER 604 AIRFOIL (e604-il)
Reynolds number: 1,000,000
Max Cl/Cd: 123.77 at α=5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-e604-il-1000000-n5.txt
Download as CSV file: xf-e604-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: EPPLER 604 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  -0.5762   0.13523   0.13297  -0.0600   1.0000   0.0033
 -18.500  -0.6222   0.12191   0.11949  -0.0660   1.0000   0.0032
 -18.250  -0.6515   0.11248   0.10994  -0.0702   1.0000   0.0031
 -18.000  -0.6939   0.10075   0.09805  -0.0757   1.0000   0.0031
 -17.750  -0.7265   0.09107   0.08823  -0.0803   1.0000   0.0031
 -17.500  -0.7593   0.08014   0.07709  -0.0872   0.9996   0.0031
 -17.250  -0.7699   0.07302   0.06984  -0.0927   0.9989   0.0030
 -17.000  -0.7818   0.06600   0.06266  -0.0980   0.9979   0.0030
 -16.750  -0.7901   0.05995   0.05646  -0.1027   0.9961   0.0030
 -16.500  -0.7893   0.05611   0.05253  -0.1052   0.9925   0.0030
 -16.250  -0.7978   0.05120   0.04748  -0.1082   0.9884   0.0030
 -16.000  -0.8086   0.04621   0.04231  -0.1111   0.9828   0.0031
 -15.500  -0.7907   0.04065   0.03655  -0.1159   0.9575   0.0031
 -15.250  -0.7621   0.03776   0.03352  -0.1222   0.9461   0.0031
 -15.000  -0.7279   0.03465   0.03025  -0.1301   0.9371   0.0032
 -14.750  -0.6882   0.03177   0.02718  -0.1388   0.9220   0.0033
 -14.500  -0.6592   0.03001   0.02519  -0.1433   0.8947   0.0034
 -14.250  -0.6499   0.02877   0.02376  -0.1431   0.8693   0.0034
 -14.000  -0.6413   0.02777   0.02262  -0.1421   0.8512   0.0034
 -13.750  -0.6349   0.02664   0.02137  -0.1410   0.8371   0.0035
 -13.500  -0.6267   0.02565   0.02025  -0.1398   0.8252   0.0034
 -13.250  -0.6164   0.02478   0.01930  -0.1388   0.8148   0.0035
 -13.000  -0.6054   0.02394   0.01838  -0.1378   0.8061   0.0035
 -12.750  -0.5957   0.02306   0.01740  -0.1366   0.7973   0.0036
 -12.500  -0.5837   0.02227   0.01654  -0.1355   0.7898   0.0037
 -12.250  -0.5710   0.02158   0.01578  -0.1344   0.7821   0.0039
 -12.000  -0.5586   0.02085   0.01497  -0.1333   0.7749   0.0039
 -11.750  -0.5454   0.02019   0.01425  -0.1322   0.7678   0.0038
 -11.500  -0.5319   0.01956   0.01355  -0.1310   0.7614   0.0039
 -11.250  -0.5176   0.01895   0.01287  -0.1299   0.7555   0.0040
 -11.000  -0.5033   0.01837   0.01224  -0.1288   0.7497   0.0042
 -10.750  -0.4881   0.01784   0.01165  -0.1277   0.7448   0.0045
 -10.500  -0.4727   0.01731   0.01107  -0.1266   0.7398   0.0045
 -10.250  -0.4572   0.01682   0.01053  -0.1254   0.7346   0.0045
 -10.000  -0.4439   0.01624   0.00989  -0.1239   0.7297   0.0048
  -9.750  -0.4286   0.01572   0.00935  -0.1227   0.7251   0.0051
  -9.500  -0.4132   0.01526   0.00885  -0.1214   0.7202   0.0052
  -9.250  -0.3983   0.01483   0.00837  -0.1200   0.7158   0.0057
  -9.000  -0.3835   0.01439   0.00790  -0.1185   0.7121   0.0058
  -8.750  -0.3694   0.01398   0.00746  -0.1168   0.7082   0.0063
  -8.500  -0.3590   0.01363   0.00707  -0.1144   0.7040   0.0066
  -8.250  -0.3436   0.01327   0.00668  -0.1130   0.6999   0.0073
  -8.000  -0.3246   0.01296   0.00634  -0.1120   0.6964   0.0083
  -7.750  -0.3043   0.01265   0.00602  -0.1112   0.6930   0.0093
  -7.500  -0.2829   0.01238   0.00573  -0.1106   0.6896   0.0105
  -7.250  -0.2612   0.01211   0.00545  -0.1099   0.6863   0.0124
  -7.000  -0.2387   0.01187   0.00519  -0.1094   0.6830   0.0144
  -6.750  -0.2152   0.01163   0.00494  -0.1091   0.6801   0.0169
  -6.500  -0.1911   0.01139   0.00470  -0.1088   0.6771   0.0197
  -6.250  -0.1667   0.01116   0.00447  -0.1086   0.6739   0.0229
  -6.000  -0.1421   0.01093   0.00425  -0.1084   0.6710   0.0281
  -5.750  -0.1177   0.01069   0.00403  -0.1082   0.6681   0.0362
  -5.500  -0.0929   0.01045   0.00382  -0.1081   0.6652   0.0472
  -5.250  -0.0674   0.01016   0.00362  -0.1082   0.6628   0.0629
  -5.000  -0.0416   0.00988   0.00342  -0.1083   0.6600   0.0819
  -4.750  -0.0155   0.00962   0.00323  -0.1084   0.6572   0.1034
  -4.500   0.0107   0.00935   0.00304  -0.1086   0.6544   0.1292
  -4.250   0.0369   0.00907   0.00286  -0.1088   0.6515   0.1640
  -4.000   0.0635   0.00876   0.00267  -0.1091   0.6490   0.2054
  -3.750   0.0905   0.00826   0.00244  -0.1097   0.6467   0.2784
  -3.500   0.1178   0.00764   0.00216  -0.1105   0.6442   0.3760
  -3.250   0.1459   0.00699   0.00190  -0.1115   0.6415   0.4908
  -3.000   0.1750   0.00683   0.00186  -0.1121   0.6388   0.5400
  -2.750   0.2040   0.00682   0.00184  -0.1125   0.6361   0.5575
  -2.250   0.2624   0.00682   0.00184  -0.1134   0.6313   0.5823
  -2.000   0.2919   0.00683   0.00184  -0.1139   0.6289   0.5946
  -1.750   0.3212   0.00685   0.00187  -0.1144   0.6262   0.6057
  -1.500   0.3502   0.00688   0.00190  -0.1148   0.6235   0.6140
  -1.250   0.3791   0.00693   0.00193  -0.1151   0.6209   0.6200
  -1.000   0.4078   0.00698   0.00193  -0.1155   0.6181   0.6226
  -0.750   0.4370   0.00701   0.00192  -0.1159   0.6157   0.6241
  -0.500   0.4663   0.00702   0.00193  -0.1164   0.6131   0.6255
  -0.250   0.4952   0.00703   0.00194  -0.1168   0.6102   0.6272
   0.000   0.5238   0.00706   0.00196  -0.1172   0.6073   0.6290
   0.250   0.5522   0.00710   0.00198  -0.1175   0.6042   0.6307
   0.500   0.5803   0.00715   0.00201  -0.1177   0.6012   0.6324
   0.750   0.6094   0.00717   0.00204  -0.1182   0.5986   0.6340
   1.000   0.6381   0.00720   0.00207  -0.1186   0.5954   0.6356
   1.250   0.6665   0.00724   0.00210  -0.1189   0.5920   0.6372
   1.500   0.6944   0.00730   0.00214  -0.1191   0.5884   0.6389
   1.750   0.7221   0.00737   0.00218  -0.1193   0.5849   0.6405
   2.000   0.7506   0.00740   0.00223  -0.1197   0.5812   0.6421
   2.250   0.7783   0.00744   0.00228  -0.1199   0.5763   0.6438
   2.500   0.8051   0.00751   0.00234  -0.1199   0.5712   0.6454
   2.750   0.8326   0.00756   0.00241  -0.1200   0.5664   0.6471
   3.000   0.8598   0.00762   0.00247  -0.1202   0.5606   0.6488
   3.250   0.8855   0.00772   0.00255  -0.1200   0.5543   0.6506
   3.500   0.9126   0.00779   0.00263  -0.1200   0.5478   0.6524
   3.750   0.9379   0.00790   0.00272  -0.1198   0.5402   0.6543
   4.000   0.9639   0.00799   0.00281  -0.1197   0.5331   0.6561
   4.250   0.9882   0.00812   0.00291  -0.1192   0.5244   0.6577
   4.500   1.0130   0.00823   0.00303  -0.1189   0.5157   0.6596
   4.750   1.0358   0.00839   0.00316  -0.1181   0.5057   0.6614
   5.000   1.0582   0.00855   0.00331  -0.1173   0.4940   0.6633
   5.250   1.0788   0.00872   0.00346  -0.1161   0.4823   0.6652
   5.500   1.0975   0.00892   0.00363  -0.1146   0.4702   0.6672
   5.750   1.1149   0.00916   0.00384  -0.1128   0.4565   0.6692
   6.000   1.1315   0.00946   0.00408  -0.1109   0.4406   0.6712
   6.250   1.1478   0.00979   0.00436  -0.1090   0.4252   0.6731
   6.500   1.1621   0.01018   0.00468  -0.1068   0.4063   0.6750
   6.750   1.1756   0.01059   0.00505  -0.1045   0.3876   0.6774
   7.000   1.1877   0.01107   0.00546  -0.1020   0.3682   0.6797
   7.250   1.1986   0.01160   0.00592  -0.0994   0.3495   0.6819
   7.500   1.2098   0.01214   0.00640  -0.0969   0.3310   0.6842
   7.750   1.2199   0.01275   0.00694  -0.0943   0.3125   0.6865
   8.000   1.2291   0.01341   0.00754  -0.0917   0.2944   0.6887
   8.250   1.2378   0.01415   0.00820  -0.0890   0.2769   0.6906
   8.500   1.2460   0.01493   0.00893  -0.0865   0.2602   0.6928
   8.750   1.2549   0.01573   0.00970  -0.0841   0.2451   0.6952
   9.000   1.2612   0.01669   0.01060  -0.0815   0.2277   0.6977
   9.250   1.2695   0.01762   0.01149  -0.0793   0.2134   0.7005
   9.500   1.2779   0.01859   0.01242  -0.0772   0.1998   0.7032
   9.750   1.2852   0.01965   0.01344  -0.0751   0.1857   0.7057
  10.000   1.2917   0.02082   0.01455  -0.0730   0.1713   0.7079
  10.250   1.3000   0.02192   0.01563  -0.0713   0.1602   0.7103
  10.500   1.3065   0.02316   0.01685  -0.0694   0.1477   0.7129
  10.750   1.3138   0.02441   0.01807  -0.0677   0.1371   0.7155
  11.000   1.3226   0.02561   0.01926  -0.0662   0.1272   0.7182
  11.250   1.3302   0.02691   0.02055  -0.0647   0.1176   0.7208
  11.500   1.3359   0.02839   0.02200  -0.0631   0.1069   0.7233
  11.750   1.3429   0.02983   0.02341  -0.0617   0.0979   0.7258
  12.000   1.3509   0.03124   0.02482  -0.0605   0.0898   0.7287
  12.250   1.3585   0.03271   0.02630  -0.0593   0.0831   0.7319
  12.500   1.3669   0.03415   0.02775  -0.0583   0.0767   0.7351
  12.750   1.3742   0.03573   0.02934  -0.0572   0.0704   0.7381
  13.000   1.3820   0.03731   0.03091  -0.0563   0.0648   0.7408
  13.250   1.3902   0.03888   0.03251  -0.0554   0.0601   0.7436
  13.500   1.3959   0.04069   0.03432  -0.0545   0.0540   0.7467
  13.750   1.4040   0.04235   0.03601  -0.0538   0.0496   0.7500
  14.000   1.4100   0.04424   0.03791  -0.0531   0.0450   0.7533
  14.250   1.4161   0.04615   0.03983  -0.0524   0.0400   0.7564
  14.500   1.4228   0.04804   0.04175  -0.0518   0.0367   0.7598
  14.750   1.4278   0.05013   0.04386  -0.0513   0.0325   0.7636
  15.000   1.4330   0.05226   0.04602  -0.0508   0.0285   0.7677
  15.250   1.4385   0.05440   0.04819  -0.0504   0.0260   0.7718
  15.500   1.4430   0.05669   0.05051  -0.0501   0.0225   0.7754
  15.750   1.4483   0.05892   0.05278  -0.0498   0.0204   0.7796
  16.000   1.4532   0.06125   0.05516  -0.0496   0.0184   0.7840
  16.250   1.4580   0.06363   0.05759  -0.0496   0.0165   0.7885
  16.500   1.4629   0.06605   0.06007  -0.0495   0.0152   0.7930
  16.750   1.4674   0.06855   0.06263  -0.0496   0.0141   0.7982
  17.000   1.4721   0.07106   0.06522  -0.0497   0.0131   0.8042
  17.250   1.4750   0.07383   0.06805  -0.0499   0.0117   0.8101
  17.500   1.4787   0.07654   0.07085  -0.0502   0.0109   0.8175
  17.750   1.4830   0.07922   0.07361  -0.0506   0.0103   0.8250
  18.000   1.4847   0.08228   0.07676  -0.0510   0.0096   0.8336
  18.250   1.4873   0.08524   0.07980  -0.0515   0.0089   0.8433
  18.750   1.4901   0.09150   0.08628  -0.0527   0.0078   0.8708
  19.000   1.4888   0.09480   0.08971  -0.0531   0.0072   0.9008
  19.250   1.4878   0.09787   0.09296  -0.0536   0.0069   1.0000
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