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EPPLER 603 AIRFOIL (e603-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: EPPLER 603 AIRFOIL (e603-il)
Reynolds number: 1,000,000
Max Cl/Cd: 136.88 at α=7.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-e603-il-1000000.txt
Download as CSV file: xf-e603-il-1000000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -17.250  -0.6378   0.10032   0.09806  -0.0686   1.0000   0.0087
 -17.000  -0.6649   0.09053   0.08810  -0.0742   1.0000   0.0086
 -16.750  -0.6915   0.08143   0.07884  -0.0797   1.0000   0.0086
 -16.500  -0.7025   0.07558   0.07289  -0.0831   1.0000   0.0085
 -16.250  -0.7009   0.07210   0.06936  -0.0852   1.0000   0.0085
 -16.000  -0.7429   0.06232   0.05932  -0.0902   1.0000   0.0085
 -15.750  -0.7271   0.06140   0.05842  -0.0907   1.0000   0.0085
 -15.500  -0.7651   0.05211   0.04880  -0.0958   0.9985   0.0086
 -15.250  -0.7617   0.04810   0.04464  -0.0990   0.9792   0.0085
 -15.000  -0.7339   0.04092   0.03710  -0.1126   0.9416   0.0087
 -14.750  -0.6959   0.03704   0.03260  -0.1227   0.8418   0.0089
 -14.500  -0.6986   0.03537   0.03066  -0.1210   0.8005   0.0089
 -14.250  -0.6973   0.03385   0.02896  -0.1197   0.7776   0.0090
 -14.000  -0.6932   0.03250   0.02749  -0.1186   0.7612   0.0091
 -13.750  -0.6856   0.03141   0.02630  -0.1177   0.7485   0.0093
 -13.500  -0.6795   0.03017   0.02493  -0.1166   0.7378   0.0095
 -13.250  -0.6703   0.02917   0.02383  -0.1156   0.7286   0.0096
 -13.000  -0.6625   0.02798   0.02252  -0.1144   0.7208   0.0096
 -12.750  -0.6531   0.02692   0.02136  -0.1133   0.7139   0.0099
 -12.500  -0.6419   0.02605   0.02039  -0.1122   0.7071   0.0100
 -12.250  -0.6313   0.02500   0.01925  -0.1110   0.7020   0.0101
 -12.000  -0.6191   0.02413   0.01829  -0.1098   0.6968   0.0103
 -11.750  -0.6063   0.02331   0.01737  -0.1087   0.6919   0.0104
 -11.500  -0.5926   0.02255   0.01652  -0.1075   0.6874   0.0105
 -11.250  -0.5769   0.02192   0.01582  -0.1066   0.6835   0.0108
 -11.000  -0.5614   0.02128   0.01511  -0.1056   0.6797   0.0108
 -10.750  -0.5511   0.02025   0.01399  -0.1039   0.6761   0.0111
 -10.500  -0.5403   0.01936   0.01303  -0.1023   0.6723   0.0114
 -10.250  -0.5249   0.01872   0.01236  -0.1011   0.6699   0.0116
 -10.000  -0.5085   0.01816   0.01177  -0.1001   0.6672   0.0119
  -9.750  -0.4929   0.01757   0.01114  -0.0988   0.6644   0.0120
  -9.500  -0.4760   0.01708   0.01061  -0.0977   0.6617   0.0124
  -9.250  -0.4586   0.01663   0.01011  -0.0966   0.6590   0.0127
  -9.000  -0.4411   0.01622   0.00964  -0.0955   0.6558   0.0132
  -8.750  -0.4228   0.01580   0.00918  -0.0945   0.6539   0.0135
  -8.500  -0.4068   0.01528   0.00863  -0.0931   0.6518   0.0138
  -8.250  -0.3935   0.01464   0.00798  -0.0913   0.6496   0.0145
  -8.000  -0.3762   0.01426   0.00758  -0.0900   0.6476   0.0150
  -7.750  -0.3596   0.01394   0.00723  -0.0886   0.6455   0.0158
  -7.500  -0.3439   0.01369   0.00695  -0.0869   0.6434   0.0165
  -7.250  -0.3289   0.01329   0.00651  -0.0852   0.6413   0.0176
  -7.000  -0.3089   0.01301   0.00620  -0.0844   0.6388   0.0188
  -6.750  -0.2868   0.01274   0.00591  -0.0838   0.6375   0.0203
  -6.500  -0.2662   0.01237   0.00556  -0.0829   0.6360   0.0229
  -6.250  -0.2438   0.01207   0.00526  -0.0824   0.6343   0.0261
  -6.000  -0.2208   0.01178   0.00498  -0.0819   0.6325   0.0307
  -5.750  -0.1975   0.01149   0.00473  -0.0815   0.6308   0.0377
  -5.500  -0.1737   0.01121   0.00450  -0.0812   0.6292   0.0487
  -5.250  -0.1499   0.01090   0.00427  -0.0810   0.6276   0.0658
  -5.000  -0.1254   0.01062   0.00406  -0.0808   0.6259   0.0857
  -4.750  -0.1004   0.01036   0.00388  -0.0808   0.6239   0.1099
  -4.500  -0.0754   0.01005   0.00370  -0.0808   0.6218   0.1447
  -4.250  -0.0506   0.00959   0.00346  -0.0809   0.6207   0.1998
  -4.000  -0.0257   0.00900   0.00320  -0.0813   0.6195   0.2809
  -3.750  -0.0004   0.00815   0.00283  -0.0820   0.6180   0.4079
  -3.500   0.0275   0.00708   0.00244  -0.0834   0.6165   0.5944
  -3.250   0.0574   0.00702   0.00250  -0.0839   0.6148   0.6426
  -3.000   0.0876   0.00709   0.00254  -0.0845   0.6133   0.6621
  -2.750   0.1175   0.00719   0.00263  -0.0850   0.6118   0.6748
  -2.500   0.1476   0.00726   0.00265  -0.0855   0.6102   0.6815
  -2.250   0.1773   0.00737   0.00273  -0.0860   0.6084   0.6866
  -2.000   0.2074   0.00752   0.00282  -0.0865   0.6063   0.6918
  -1.750   0.2374   0.00762   0.00289  -0.0871   0.6049   0.6968
  -1.500   0.2666   0.00773   0.00302  -0.0873   0.6037   0.7017
  -1.250   0.2960   0.00789   0.00319  -0.0877   0.6023   0.7077
  -1.000   0.3256   0.00804   0.00332  -0.0880   0.6008   0.7136
  -0.750   0.3539   0.00820   0.00352  -0.0881   0.5992   0.7180
  -0.500   0.3831   0.00831   0.00362  -0.0884   0.5975   0.7211
  -0.250   0.4129   0.00833   0.00361  -0.0890   0.5959   0.7226
   0.000   0.4426   0.00834   0.00360  -0.0896   0.5942   0.7238
   0.250   0.4725   0.00838   0.00360  -0.0902   0.5924   0.7252
   0.500   0.5024   0.00846   0.00363  -0.0909   0.5902   0.7264
   0.750   0.5323   0.00851   0.00366  -0.0916   0.5886   0.7273
   1.000   0.5619   0.00851   0.00366  -0.0921   0.5871   0.7281
   1.250   0.5914   0.00848   0.00363  -0.0927   0.5854   0.7292
   1.500   0.6206   0.00843   0.00360  -0.0932   0.5835   0.7306
   1.750   0.6498   0.00843   0.00360  -0.0937   0.5815   0.7316
   2.000   0.6790   0.00843   0.00360  -0.0942   0.5795   0.7325
   2.250   0.7081   0.00845   0.00361  -0.0947   0.5774   0.7333
   2.500   0.7373   0.00850   0.00365  -0.0952   0.5750   0.7342
   2.750   0.7665   0.00858   0.00373  -0.0958   0.5726   0.7352
   3.000   0.7952   0.00858   0.00376  -0.0962   0.5706   0.7363
   3.250   0.8239   0.00858   0.00378  -0.0966   0.5682   0.7374
   3.500   0.8527   0.00857   0.00380  -0.0970   0.5653   0.7384
   3.750   0.8813   0.00858   0.00380  -0.0975   0.5623   0.7394
   4.000   0.9098   0.00863   0.00383  -0.0979   0.5589   0.7404
   4.250   0.9384   0.00867   0.00388  -0.0983   0.5558   0.7414
   4.500   0.9667   0.00866   0.00392  -0.0987   0.5526   0.7424
   4.750   0.9950   0.00867   0.00395  -0.0990   0.5490   0.7434
   5.000   1.0230   0.00871   0.00398  -0.0993   0.5452   0.7443
   5.250   1.0506   0.00879   0.00405  -0.0996   0.5411   0.7450
   5.500   1.0787   0.00879   0.00410  -0.0999   0.5369   0.7457
   5.750   1.1063   0.00877   0.00411  -0.1002   0.5320   0.7469
   6.000   1.1327   0.00882   0.00416  -0.1002   0.5269   0.7480
   6.250   1.1601   0.00885   0.00424  -0.1005   0.5214   0.7489
   6.500   1.1865   0.00891   0.00432  -0.1005   0.5148   0.7499
   6.750   1.2122   0.00900   0.00443  -0.1004   0.5077   0.7509
   7.000   1.2372   0.00910   0.00454  -0.1002   0.4985   0.7520
   7.250   1.2620   0.00922   0.00468  -0.0999   0.4888   0.7531
   7.500   1.2849   0.00940   0.00484  -0.0993   0.4777   0.7542
   7.750   1.3063   0.00962   0.00503  -0.0984   0.4642   0.7553
   8.000   1.3262   0.00989   0.00526  -0.0973   0.4496   0.7564
   8.250   1.3443   0.01020   0.00553  -0.0959   0.4330   0.7575
   8.500   1.3586   0.01056   0.00583  -0.0938   0.4148   0.7586
   8.750   1.3687   0.01096   0.00617  -0.0908   0.3961   0.7597
   9.000   1.3768   0.01150   0.00663  -0.0876   0.3759   0.7608
   9.250   1.3841   0.01211   0.00717  -0.0845   0.3573   0.7618
   9.500   1.3904   0.01276   0.00775  -0.0813   0.3387   0.7633
   9.750   1.3944   0.01351   0.00844  -0.0779   0.3188   0.7649
  10.000   1.3945   0.01448   0.00934  -0.0741   0.2979   0.7663
  10.500   1.3887   0.01707   0.01179  -0.0668   0.2576   0.7690
  10.750   1.3876   0.01854   0.01320  -0.0639   0.2409   0.7704
  11.000   1.3868   0.02014   0.01476  -0.0614   0.2252   0.7718
  11.250   1.3858   0.02187   0.01644  -0.0590   0.2099   0.7732
  11.500   1.3848   0.02371   0.01823  -0.0569   0.1950   0.7746
  11.750   1.3845   0.02557   0.02004  -0.0550   0.1811   0.7758
  12.000   1.3843   0.02749   0.02192  -0.0532   0.1680   0.7771
  12.250   1.3853   0.02938   0.02378  -0.0517   0.1568   0.7781
  12.500   1.3875   0.03121   0.02559  -0.0503   0.1462   0.7795
  12.750   1.3899   0.03308   0.02745  -0.0490   0.1357   0.7811
  13.000   1.3925   0.03498   0.02934  -0.0479   0.1264   0.7826
  13.250   1.3941   0.03701   0.03134  -0.0468   0.1165   0.7840
  13.500   1.3982   0.03892   0.03325  -0.0459   0.1080   0.7853
  13.750   1.4021   0.04089   0.03520  -0.0451   0.0996   0.7866
  14.000   1.4036   0.04312   0.03741  -0.0442   0.0907   0.7880
  14.250   1.4092   0.04503   0.03932  -0.0437   0.0840   0.7894
  14.500   1.4128   0.04719   0.04148  -0.0431   0.0772   0.7907
  14.750   1.4169   0.04934   0.04362  -0.0427   0.0706   0.7921
  15.000   1.4218   0.05146   0.04576  -0.0423   0.0653   0.7933
  15.250   1.4250   0.05378   0.04805  -0.0420   0.0591   0.7944
  15.500   1.4300   0.05600   0.05030  -0.0418   0.0544   0.7958
  15.750   1.4333   0.05839   0.05270  -0.0416   0.0493   0.7976
  16.000   1.4371   0.06080   0.05513  -0.0415   0.0448   0.7993
  16.250   1.4407   0.06326   0.05761  -0.0415   0.0407   0.8010
  16.500   1.4431   0.06590   0.06028  -0.0415   0.0365   0.8028
  16.750   1.4463   0.06853   0.06293  -0.0416   0.0327   0.8046
  17.000   1.4472   0.07147   0.06589  -0.0418   0.0289   0.8063
  17.250   1.4486   0.07441   0.06884  -0.0421   0.0253   0.8079
  17.500   1.4500   0.07739   0.07186  -0.0425   0.0224   0.8095
  17.750   1.4498   0.08065   0.07515  -0.0430   0.0198   0.8109
  18.000   1.4514   0.08375   0.07830  -0.0435   0.0181   0.8128
  18.250   1.4508   0.08715   0.08175  -0.0442   0.0165   0.8148
  18.500   1.4521   0.09036   0.08504  -0.0450   0.0154   0.8168
  18.750   1.4527   0.09368   0.08842  -0.0458   0.0144   0.8188
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