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EPPLER 604 AIRFOIL (e604-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: EPPLER 604 AIRFOIL (e604-il)
Reynolds number: 500,000
Max Cl/Cd: 101.85 at α=6°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-e604-il-500000-n5.txt
Download as CSV file: xf-e604-il-500000-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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -17.000  -0.5444   0.11443   0.11157  -0.0697   1.0000   0.0050
 -16.750  -0.6074   0.09754   0.09439  -0.0776   1.0000   0.0049
 -16.500  -0.6398   0.08757   0.08421  -0.0825   1.0000   0.0047
 -16.250  -0.6655   0.07938   0.07586  -0.0865   1.0000   0.0047
 -16.000  -0.6844   0.07170   0.06802  -0.0914   0.9995   0.0048
 -15.750  -0.6902   0.06520   0.06135  -0.0969   0.9977   0.0048
 -15.250  -0.6939   0.05523   0.05106  -0.1048   0.9895   0.0048
 -15.000  -0.6926   0.05117   0.04686  -0.1081   0.9835   0.0048
 -14.500  -0.6873   0.04450   0.03995  -0.1124   0.9592   0.0050
 -14.250  -0.6726   0.04138   0.03667  -0.1165   0.9478   0.0050
 -14.000  -0.6485   0.03854   0.03367  -0.1218   0.9392   0.0050
 -13.750  -0.6186   0.03581   0.03078  -0.1280   0.9306   0.0052
 -13.500  -0.5872   0.03334   0.02811  -0.1340   0.9186   0.0053
 -13.250  -0.5577   0.03146   0.02605  -0.1386   0.9017   0.0054
 -13.000  -0.5393   0.02998   0.02436  -0.1403   0.8824   0.0054
 -12.750  -0.5287   0.02869   0.02290  -0.1401   0.8652   0.0057
 -12.500  -0.5196   0.02756   0.02162  -0.1393   0.8510   0.0058
 -12.250  -0.5096   0.02658   0.02050  -0.1384   0.8393   0.0061
 -12.000  -0.4999   0.02562   0.01941  -0.1373   0.8291   0.0061
 -11.750  -0.4897   0.02471   0.01840  -0.1361   0.8197   0.0061
 -11.500  -0.4783   0.02389   0.01746  -0.1350   0.8115   0.0062
 -11.250  -0.4668   0.02308   0.01656  -0.1338   0.8033   0.0063
 -11.000  -0.4563   0.02224   0.01563  -0.1325   0.7959   0.0066
 -10.750  -0.4437   0.02151   0.01484  -0.1313   0.7886   0.0071
 -10.500  -0.4304   0.02085   0.01410  -0.1301   0.7817   0.0072
 -10.250  -0.4165   0.02023   0.01341  -0.1289   0.7755   0.0074
 -10.000  -0.4027   0.01959   0.01270  -0.1276   0.7694   0.0078
  -9.750  -0.3885   0.01903   0.01205  -0.1264   0.7640   0.0082
  -9.500  -0.3735   0.01847   0.01144  -0.1252   0.7589   0.0085
  -9.250  -0.3596   0.01789   0.01082  -0.1238   0.7535   0.0091
  -9.000  -0.3453   0.01737   0.01024  -0.1224   0.7484   0.0097
  -8.750  -0.3303   0.01688   0.00970  -0.1211   0.7436   0.0106
  -8.500  -0.3162   0.01637   0.00916  -0.1195   0.7387   0.0115
  -8.250  -0.3025   0.01592   0.00866  -0.1179   0.7341   0.0129
  -8.000  -0.2905   0.01552   0.00822  -0.1159   0.7302   0.0147
  -7.750  -0.2780   0.01516   0.00784  -0.1139   0.7261   0.0166
  -7.500  -0.2617   0.01476   0.00743  -0.1127   0.7219   0.0189
  -7.250  -0.2437   0.01442   0.00705  -0.1116   0.7179   0.0220
  -7.000  -0.2245   0.01410   0.00670  -0.1107   0.7142   0.0258
  -6.750  -0.2042   0.01377   0.00638  -0.1099   0.7107   0.0305
  -6.500  -0.1831   0.01345   0.00607  -0.1092   0.7073   0.0363
  -6.250  -0.1615   0.01314   0.00577  -0.1087   0.7039   0.0437
  -6.000  -0.1396   0.01283   0.00548  -0.1081   0.7007   0.0549
  -5.750  -0.1169   0.01253   0.00520  -0.1077   0.6976   0.0691
  -5.500  -0.0939   0.01218   0.00493  -0.1074   0.6943   0.0871
  -5.250  -0.0702   0.01185   0.00468  -0.1073   0.6911   0.1085
  -4.750  -0.0225   0.01108   0.00414  -0.1071   0.6852   0.1780
  -4.500   0.0017   0.01062   0.00384  -0.1072   0.6824   0.2341
  -4.250   0.0256   0.00992   0.00348  -0.1075   0.6795   0.3227
  -4.000   0.0500   0.00894   0.00305  -0.1082   0.6767   0.4630
  -3.750   0.0778   0.00868   0.00303  -0.1087   0.6737   0.5424
  -3.500   0.1065   0.00868   0.00303  -0.1090   0.6708   0.5668
  -3.250   0.1354   0.00870   0.00301  -0.1093   0.6681   0.5808
  -2.750   0.1934   0.00878   0.00301  -0.1101   0.6631   0.6023
  -2.500   0.2222   0.00884   0.00306  -0.1104   0.6602   0.6137
  -2.250   0.2513   0.00893   0.00311  -0.1108   0.6573   0.6258
  -2.000   0.2796   0.00903   0.00322  -0.1109   0.6546   0.6340
  -1.750   0.3087   0.00910   0.00321  -0.1113   0.6519   0.6395
  -1.500   0.3378   0.00914   0.00317  -0.1118   0.6495   0.6416
  -1.250   0.3663   0.00913   0.00317  -0.1121   0.6468   0.6433
  -1.000   0.3949   0.00914   0.00317  -0.1125   0.6440   0.6448
  -0.750   0.4234   0.00916   0.00317  -0.1128   0.6411   0.6464
  -0.500   0.4520   0.00919   0.00317  -0.1131   0.6383   0.6481
  -0.250   0.4806   0.00923   0.00318  -0.1135   0.6356   0.6501
   0.000   0.5093   0.00928   0.00318  -0.1139   0.6330   0.6520
   0.250   0.5378   0.00930   0.00320  -0.1142   0.6301   0.6538
   0.500   0.5662   0.00933   0.00322  -0.1146   0.6271   0.6556
   0.750   0.5945   0.00936   0.00323  -0.1149   0.6238   0.6572
   1.000   0.6226   0.00940   0.00326  -0.1152   0.6208   0.6588
   1.250   0.6506   0.00946   0.00330  -0.1154   0.6179   0.6605
   1.500   0.6784   0.00950   0.00336  -0.1157   0.6149   0.6622
   1.750   0.7061   0.00954   0.00343  -0.1159   0.6114   0.6639
   2.000   0.7337   0.00959   0.00349  -0.1160   0.6079   0.6656
   2.250   0.7612   0.00965   0.00354  -0.1162   0.6044   0.6674
   2.500   0.7888   0.00972   0.00359  -0.1164   0.6011   0.6692
   2.750   0.8159   0.00976   0.00367  -0.1165   0.5971   0.6711
   3.000   0.8428   0.00982   0.00374  -0.1166   0.5925   0.6730
   3.250   0.8692   0.00989   0.00380  -0.1165   0.5878   0.6749
   3.500   0.8953   0.00996   0.00389  -0.1164   0.5832   0.6766
   3.750   0.9211   0.01001   0.00400  -0.1163   0.5778   0.6784
   4.000   0.9462   0.01010   0.00409  -0.1160   0.5722   0.6802
   4.250   0.9714   0.01018   0.00420  -0.1157   0.5664   0.6820
   4.500   0.9959   0.01026   0.00431  -0.1153   0.5596   0.6840
   4.750   1.0197   0.01038   0.00441  -0.1148   0.5533   0.6861
   5.000   1.0438   0.01047   0.00454  -0.1143   0.5459   0.6881
   5.250   1.0658   0.01062   0.00466  -0.1134   0.5383   0.6902
   5.500   1.0883   0.01073   0.00481  -0.1126   0.5296   0.6921
   5.750   1.1069   0.01087   0.00497  -0.1111   0.5203   0.6942
   6.000   1.1244   0.01104   0.00515  -0.1093   0.5098   0.6964
   6.250   1.1422   0.01123   0.00536  -0.1076   0.4992   0.6986
   6.500   1.1585   0.01150   0.00561  -0.1057   0.4877   0.7010
   6.750   1.1730   0.01182   0.00591  -0.1035   0.4744   0.7033
   7.250   1.1995   0.01262   0.00663  -0.0989   0.4447   0.7080
   7.500   1.2097   0.01311   0.00710  -0.0962   0.4274   0.7101
   7.750   1.2200   0.01364   0.00761  -0.0936   0.4112   0.7124
   8.000   1.2284   0.01428   0.00821  -0.0907   0.3931   0.7149
   8.250   1.2356   0.01501   0.00890  -0.0879   0.3748   0.7178
   8.500   1.2422   0.01583   0.00967  -0.0851   0.3567   0.7208
   8.750   1.2466   0.01681   0.01058  -0.0821   0.3371   0.7236
   9.000   1.2517   0.01781   0.01154  -0.0794   0.3196   0.7261
   9.250   1.2559   0.01892   0.01261  -0.0767   0.3020   0.7285
   9.500   1.2605   0.02009   0.01374  -0.0742   0.2843   0.7312
   9.750   1.2646   0.02136   0.01496  -0.0718   0.2665   0.7341
  10.000   1.2694   0.02266   0.01623  -0.0696   0.2503   0.7370
  10.250   1.2742   0.02402   0.01754  -0.0676   0.2346   0.7399
  10.500   1.2792   0.02541   0.01891  -0.0657   0.2198   0.7426
  10.750   1.2840   0.02686   0.02033  -0.0639   0.2055   0.7455
  11.000   1.2887   0.02837   0.02182  -0.0621   0.1910   0.7488
  11.250   1.2934   0.02994   0.02337  -0.0605   0.1773   0.7522
  11.500   1.2984   0.03155   0.02495  -0.0590   0.1648   0.7555
  11.750   1.3050   0.03310   0.02649  -0.0578   0.1531   0.7585
  12.000   1.3115   0.03467   0.02807  -0.0566   0.1425   0.7616
  12.250   1.3172   0.03636   0.02976  -0.0554   0.1323   0.7649
  12.500   1.3224   0.03815   0.03153  -0.0543   0.1221   0.7685
  12.750   1.3283   0.03992   0.03330  -0.0533   0.1121   0.7720
  13.000   1.3346   0.04170   0.03509  -0.0525   0.1033   0.7755
  13.250   1.3398   0.04360   0.03701  -0.0516   0.0951   0.7794
  13.500   1.3460   0.04548   0.03891  -0.0509   0.0875   0.7838
  13.750   1.3523   0.04739   0.04084  -0.0503   0.0807   0.7883
  14.000   1.3579   0.04941   0.04288  -0.0497   0.0748   0.7925
  14.250   1.3645   0.05134   0.04488  -0.0492   0.0693   0.7972
  14.500   1.3689   0.05357   0.04712  -0.0487   0.0636   0.8021
  15.000   1.3792   0.05795   0.05159  -0.0479   0.0539   0.8123
  15.250   1.3851   0.06012   0.05382  -0.0477   0.0497   0.8184
  15.500   1.3884   0.06262   0.05637  -0.0475   0.0456   0.8247
  15.750   1.3933   0.06495   0.05877  -0.0473   0.0418   0.8325
  16.000   1.3957   0.06763   0.06151  -0.0472   0.0383   0.8407
  16.250   1.3999   0.07009   0.06406  -0.0472   0.0353   0.8511
  16.500   1.4017   0.07284   0.06689  -0.0471   0.0324   0.8634
  16.750   1.4043   0.07554   0.06970  -0.0472   0.0299   0.8803
  17.000   1.4053   0.07817   0.07247  -0.0469   0.0277   0.9226
  17.500   1.4085   0.08412   0.07856  -0.0478   0.0237   1.0000
  17.750   1.4084   0.08754   0.08202  -0.0484   0.0218   1.0000
  18.000   1.4105   0.09070   0.08527  -0.0492   0.0204   1.0000
  18.250   1.4112   0.09410   0.08872  -0.0500   0.0188   1.0000
  18.500   1.4104   0.09776   0.09244  -0.0510   0.0175   1.0000
  18.750   1.4112   0.10121   0.09598  -0.0520   0.0162   1.0000
  19.000   1.4105   0.10491   0.09974  -0.0532   0.0151   1.0000
  19.250   1.4089   0.10878   0.10369  -0.0545   0.0142   1.0000
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