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E203 (13.64%) (e203-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: E203 (13.64%) (e203-il)
Reynolds number: 1,000,000
Max Cl/Cd: 132.39 at α=5.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-e203-il-1000000.txt
Download as CSV file: xf-e203-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: E203  (13.64%)                                  
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -15.000  -0.6868   0.09262   0.09058  -0.0485   1.0000   0.0095
 -14.750  -0.7354   0.07861   0.07638  -0.0569   1.0000   0.0093
 -14.500  -0.7456   0.07279   0.07047  -0.0606   1.0000   0.0095
 -14.250  -0.7775   0.06393   0.06144  -0.0661   1.0000   0.0093
 -14.000  -0.7957   0.05785   0.05524  -0.0698   1.0000   0.0092
 -13.750  -0.8134   0.05221   0.04946  -0.0731   1.0000   0.0093
 -13.500  -0.8291   0.04719   0.04429  -0.0758   1.0000   0.0093
 -13.250  -0.8291   0.04447   0.04150  -0.0772   1.0000   0.0096
 -13.000  -0.8426   0.04036   0.03724  -0.0788   1.0000   0.0096
 -12.750  -0.8520   0.03715   0.03390  -0.0795   1.0000   0.0096
 -12.500  -0.8592   0.03465   0.03129  -0.0794   1.0000   0.0097
 -12.250  -0.8704   0.03242   0.02893  -0.0780   1.0000   0.0098
 -12.000  -0.8824   0.03111   0.02753  -0.0749   1.0000   0.0099
 -11.750  -0.9029   0.02993   0.02626  -0.0692   1.0000   0.0098
 -11.500  -0.8988   0.02905   0.02529  -0.0669   0.9997   0.0100
 -11.250  -0.8707   0.02770   0.02378  -0.0693   0.9976   0.0101
 -11.000  -0.8537   0.02388   0.01964  -0.0716   0.9947   0.0105
 -10.750  -0.8289   0.02217   0.01784  -0.0731   0.9921   0.0108
 -10.500  -0.8007   0.02110   0.01671  -0.0746   0.9892   0.0112
 -10.250  -0.7699   0.02015   0.01570  -0.0765   0.9869   0.0115
 -10.000  -0.7376   0.01919   0.01465  -0.0785   0.9851   0.0119
  -9.750  -0.7044   0.01822   0.01360  -0.0806   0.9837   0.0122
  -9.500  -0.6781   0.01744   0.01274  -0.0810   0.9793   0.0126
  -9.250  -0.6468   0.01674   0.01198  -0.0824   0.9760   0.0130
  -9.000  -0.6126   0.01611   0.01128  -0.0842   0.9737   0.0133
  -8.750  -0.5784   0.01541   0.01050  -0.0861   0.9714   0.0135
  -8.500  -0.5600   0.01395   0.00893  -0.0852   0.9619   0.0141
  -8.250  -0.5328   0.01309   0.00801  -0.0857   0.9543   0.0146
  -8.000  -0.5052   0.01249   0.00736  -0.0861   0.9438   0.0151
  -7.750  -0.4772   0.01196   0.00675  -0.0864   0.9295   0.0157
  -7.500  -0.4491   0.01154   0.00625  -0.0866   0.9111   0.0163
  -7.250  -0.4230   0.01121   0.00579  -0.0864   0.8888   0.0170
  -7.000  -0.3981   0.01092   0.00537  -0.0859   0.8672   0.0173
  -6.750  -0.3739   0.01059   0.00491  -0.0853   0.8466   0.0178
  -6.500  -0.3503   0.01018   0.00435  -0.0846   0.8273   0.0190
  -6.250  -0.3253   0.00992   0.00399  -0.0841   0.8103   0.0202
  -6.000  -0.2999   0.00971   0.00369  -0.0837   0.7947   0.0216
  -5.750  -0.2741   0.00950   0.00339  -0.0833   0.7802   0.0238
  -5.500  -0.2487   0.00919   0.00308  -0.0830   0.7667   0.0329
  -5.250  -0.2240   0.00874   0.00276  -0.0826   0.7546   0.0670
  -5.000  -0.1982   0.00846   0.00254  -0.0824   0.7432   0.0944
  -4.750  -0.1723   0.00821   0.00234  -0.0822   0.7324   0.1227
  -4.500  -0.1459   0.00794   0.00215  -0.0821   0.7223   0.1547
  -4.250  -0.1197   0.00765   0.00198  -0.0819   0.7133   0.1962
  -4.000  -0.0935   0.00737   0.00182  -0.0818   0.7041   0.2417
  -3.750  -0.0670   0.00707   0.00167  -0.0818   0.6960   0.2915
  -3.500  -0.0405   0.00684   0.00157  -0.0817   0.6881   0.3427
  -3.250  -0.0129   0.00672   0.00151  -0.0817   0.6807   0.3763
  -3.000   0.0147   0.00666   0.00147  -0.0816   0.6734   0.4056
  -2.750   0.0428   0.00661   0.00145  -0.0817   0.6668   0.4244
  -2.500   0.0709   0.00661   0.00142  -0.0817   0.6602   0.4378
  -2.250   0.0990   0.00661   0.00140  -0.0818   0.6540   0.4510
  -2.000   0.1272   0.00658   0.00138  -0.0818   0.6477   0.4603
  -1.750   0.1553   0.00661   0.00135  -0.0819   0.6419   0.4682
  -1.500   0.1837   0.00659   0.00134  -0.0820   0.6363   0.4768
  -1.250   0.2120   0.00660   0.00133  -0.0820   0.6305   0.4845
  -1.000   0.2400   0.00662   0.00132  -0.0821   0.6251   0.4926
  -0.750   0.2685   0.00661   0.00132  -0.0822   0.6198   0.5003
  -0.500   0.2966   0.00662   0.00132  -0.0822   0.6142   0.5084
  -0.250   0.3248   0.00664   0.00133  -0.0823   0.6092   0.5162
   0.000   0.3532   0.00663   0.00134  -0.0824   0.6040   0.5245
   0.250   0.3812   0.00665   0.00136  -0.0824   0.5988   0.5324
   0.500   0.4093   0.00667   0.00138  -0.0825   0.5939   0.5415
   0.750   0.4376   0.00666   0.00141  -0.0826   0.5887   0.5514
   1.000   0.4655   0.00668   0.00144  -0.0826   0.5835   0.5618
   1.250   0.4935   0.00670   0.00148  -0.0826   0.5785   0.5726
   1.500   0.5217   0.00669   0.00152  -0.0827   0.5731   0.5840
   1.750   0.5493   0.00673   0.00156  -0.0827   0.5674   0.5961
   2.000   0.5774   0.00673   0.00161  -0.0827   0.5613   0.6098
   2.250   0.6049   0.00674   0.00166  -0.0827   0.5543   0.6252
   2.500   0.6325   0.00676   0.00172  -0.0826   0.5480   0.6422
   2.750   0.6602   0.00676   0.00179  -0.0826   0.5413   0.6609
   3.000   0.6873   0.00679   0.00186  -0.0825   0.5346   0.6824
   3.250   0.7147   0.00678   0.00194  -0.0824   0.5272   0.7067
   3.500   0.7414   0.00680   0.00203  -0.0822   0.5195   0.7336
   3.750   0.7683   0.00679   0.00212  -0.0820   0.5116   0.7636
   4.000   0.7943   0.00681   0.00222  -0.0816   0.5037   0.7977
   4.250   0.8197   0.00679   0.00233  -0.0811   0.4949   0.8381
   4.500   0.8432   0.00677   0.00245  -0.0801   0.4858   0.8869
   4.750   0.8663   0.00677   0.00256  -0.0789   0.4754   0.9504
   5.000   0.9061   0.00689   0.00267  -0.0816   0.4614   1.0000
   5.250   0.9319   0.00705   0.00279  -0.0813   0.4475   1.0000
   5.500   0.9572   0.00723   0.00293  -0.0809   0.4305   1.0000
   5.750   0.9822   0.00744   0.00309  -0.0804   0.4109   1.0000
   6.000   1.0054   0.00776   0.00329  -0.0797   0.3812   1.0000
   6.250   1.0264   0.00824   0.00358  -0.0786   0.3393   1.0000
   6.500   1.0452   0.00886   0.00395  -0.0771   0.2894   1.0000
   6.750   1.0622   0.00960   0.00441  -0.0755   0.2373   1.0000
   7.000   1.0793   0.01031   0.00487  -0.0738   0.1914   1.0000
   7.250   1.0967   0.01097   0.00533  -0.0722   0.1548   1.0000
   7.500   1.1146   0.01157   0.00578  -0.0706   0.1254   1.0000
   7.750   1.1326   0.01214   0.00621  -0.0691   0.1024   1.0000
   8.000   1.1509   0.01266   0.00664  -0.0676   0.0837   1.0000
   8.250   1.1681   0.01321   0.00711  -0.0660   0.0676   1.0000
   8.500   1.1846   0.01376   0.00758  -0.0642   0.0541   1.0000
   8.750   1.1989   0.01430   0.00806  -0.0620   0.0424   1.0000
   9.000   1.2112   0.01487   0.00858  -0.0595   0.0322   1.0000
   9.250   1.2195   0.01563   0.00925  -0.0563   0.0200   1.0000
   9.500   1.2273   0.01645   0.01001  -0.0532   0.0124   1.0000
   9.750   1.2399   0.01707   0.01067  -0.0510   0.0106   1.0000
  10.000   1.2504   0.01782   0.01145  -0.0485   0.0093   1.0000
  10.250   1.2628   0.01849   0.01216  -0.0464   0.0088   1.0000
  10.500   1.2748   0.01921   0.01293  -0.0444   0.0084   1.0000
  10.750   1.2856   0.02001   0.01379  -0.0424   0.0080   1.0000
  11.000   1.2955   0.02091   0.01473  -0.0403   0.0076   1.0000
  11.250   1.3026   0.02202   0.01590  -0.0382   0.0072   1.0000
  11.500   1.3068   0.02340   0.01736  -0.0358   0.0069   1.0000
  11.750   1.3120   0.02480   0.01885  -0.0339   0.0067   1.0000
  12.000   1.3198   0.02608   0.02019  -0.0323   0.0066   1.0000
  12.250   1.3265   0.02751   0.02169  -0.0309   0.0065   1.0000
  12.500   1.3324   0.02908   0.02334  -0.0295   0.0064   1.0000
  12.750   1.3401   0.03055   0.02488  -0.0284   0.0062   1.0000
  13.000   1.3443   0.03239   0.02680  -0.0273   0.0060   1.0000
  13.250   1.3485   0.03430   0.02878  -0.0263   0.0060   1.0000
  13.500   1.3523   0.03630   0.03087  -0.0254   0.0059   1.0000
  13.750   1.3542   0.03856   0.03321  -0.0246   0.0058   1.0000
  14.000   1.3575   0.04076   0.03548  -0.0241   0.0055   1.0000
  14.250   1.3584   0.04325   0.03807  -0.0236   0.0057   1.0000
  14.500   1.3616   0.04559   0.04046  -0.0233   0.0054   1.0000
  14.750   1.3594   0.04859   0.04356  -0.0231   0.0053   1.0000
  15.000   1.3581   0.05159   0.04664  -0.0230   0.0052   1.0000
  15.250   1.3563   0.05474   0.04988  -0.0232   0.0051   1.0000
  15.500   1.3516   0.05837   0.05361  -0.0235   0.0051   1.0000
  15.750   1.3502   0.06169   0.05701  -0.0239   0.0051   1.0000
  16.000   1.3313   0.06736   0.06283  -0.0247   0.0049   1.0000
  16.250   1.3230   0.07185   0.06744  -0.0256   0.0048   1.0000
  16.500   1.3198   0.07579   0.07149  -0.0266   0.0048   1.0000
  16.750   1.3182   0.07964   0.07543  -0.0278   0.0048   1.0000
  17.000   1.3150   0.08382   0.07971  -0.0292   0.0048   1.0000
  17.250   1.3111   0.08817   0.08417  -0.0307   0.0048   1.0000
  17.500   1.3060   0.09284   0.08895  -0.0324   0.0047   1.0000
  17.750   1.3019   0.09750   0.09372  -0.0343   0.0047   1.0000
  18.000   1.2957   0.10257   0.09891  -0.0365   0.0047   1.0000
  18.250   1.2899   0.10766   0.10411  -0.0388   0.0047   1.0000
  18.500   1.2838   0.11294   0.10951  -0.0413   0.0047   1.0000
  18.750   1.2770   0.11840   0.11508  -0.0440   0.0047   1.0000
  19.000   1.2682   0.12437   0.12117  -0.0471   0.0047   1.0000
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