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E201 (11.88%) (e201-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: E201 (11.88%) (e201-il)
Reynolds number: 1,000,000
Max Cl/Cd: 122.49 at α=4.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-e201-il-1000000-n5.txt
Download as CSV file: xf-e201-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: E201  (11.88%)                                  
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -12.500  -0.7049   0.05820   0.05618  -0.0605   1.0000   0.0065
 -12.250  -0.7406   0.04689   0.04468  -0.0697   1.0000   0.0065
 -12.000  -0.7630   0.03973   0.03734  -0.0761   1.0000   0.0064
 -11.750  -0.7855   0.03556   0.03302  -0.0779   1.0000   0.0064
 -11.500  -0.7963   0.03259   0.02987  -0.0777   0.9972   0.0065
 -11.250  -0.7844   0.02964   0.02666  -0.0799   0.9918   0.0066
 -11.000  -0.7669   0.02729   0.02409  -0.0816   0.9872   0.0067
 -10.500  -0.7253   0.02342   0.01979  -0.0840   0.9775   0.0069
 -10.000  -0.6756   0.02090   0.01695  -0.0857   0.9632   0.0071
  -9.750  -0.6486   0.01984   0.01574  -0.0866   0.9521   0.0072
  -9.500  -0.6220   0.01872   0.01444  -0.0874   0.9334   0.0073
  -9.250  -0.5971   0.01796   0.01350  -0.0874   0.9059   0.0073
  -9.000  -0.5760   0.01728   0.01260  -0.0865   0.8766   0.0074
  -8.750  -0.5562   0.01643   0.01152  -0.0855   0.8517   0.0075
  -8.500  -0.5372   0.01536   0.01024  -0.0844   0.8301   0.0076
  -8.250  -0.5162   0.01456   0.00926  -0.0836   0.8110   0.0078
  -8.000  -0.4936   0.01394   0.00850  -0.0829   0.7941   0.0079
  -7.750  -0.4701   0.01343   0.00786  -0.0823   0.7786   0.0080
  -7.500  -0.4459   0.01298   0.00729  -0.0819   0.7645   0.0082
  -7.250  -0.4212   0.01258   0.00679  -0.0814   0.7513   0.0084
  -7.000  -0.3961   0.01219   0.00631  -0.0811   0.7393   0.0086
  -6.750  -0.3704   0.01187   0.00591  -0.0808   0.7286   0.0088
  -6.500  -0.3448   0.01154   0.00549  -0.0805   0.7184   0.0092
  -6.250  -0.3191   0.01120   0.00506  -0.0802   0.7084   0.0094
  -6.000  -0.2930   0.01088   0.00466  -0.0800   0.6996   0.0097
  -5.750  -0.2668   0.01059   0.00429  -0.0797   0.6913   0.0099
  -5.500  -0.2401   0.01034   0.00397  -0.0796   0.6829   0.0102
  -5.250  -0.2133   0.01012   0.00367  -0.0794   0.6755   0.0104
  -5.000  -0.1863   0.00991   0.00341  -0.0793   0.6683   0.0106
  -4.750  -0.1596   0.00965   0.00307  -0.0791   0.6614   0.0109
  -4.500  -0.1326   0.00940   0.00277  -0.0790   0.6545   0.0115
  -4.000  -0.0780   0.00906   0.00233  -0.0788   0.6423   0.0128
  -3.750  -0.0505   0.00893   0.00216  -0.0787   0.6359   0.0137
  -3.500  -0.0229   0.00881   0.00200  -0.0787   0.6304   0.0149
  -3.250   0.0047   0.00865   0.00184  -0.0786   0.6247   0.0192
  -2.750   0.0589   0.00818   0.00154  -0.0785   0.6141   0.0707
  -2.500   0.0863   0.00801   0.00143  -0.0785   0.6087   0.0967
  -2.250   0.1134   0.00782   0.00134  -0.0785   0.6037   0.1336
  -2.000   0.1409   0.00762   0.00125  -0.0785   0.5988   0.1719
  -1.750   0.1680   0.00740   0.00118  -0.0785   0.5937   0.2229
  -1.500   0.1952   0.00724   0.00112  -0.0785   0.5889   0.2665
  -1.250   0.2222   0.00694   0.00108  -0.0785   0.5843   0.3442
  -1.000   0.2495   0.00678   0.00106  -0.0785   0.5792   0.4002
  -0.500   0.3052   0.00668   0.00105  -0.0785   0.5699   0.4491
  -0.250   0.3332   0.00665   0.00105  -0.0785   0.5648   0.4715
   0.000   0.3609   0.00664   0.00106  -0.0785   0.5602   0.4909
   0.250   0.3890   0.00660   0.00108  -0.0786   0.5557   0.5102
   0.500   0.4169   0.00658   0.00109  -0.0786   0.5505   0.5308
   0.750   0.4446   0.00657   0.00112  -0.0786   0.5456   0.5530
   1.000   0.4725   0.00654   0.00115  -0.0786   0.5411   0.5762
   1.250   0.5002   0.00652   0.00119  -0.0786   0.5356   0.5998
   1.500   0.5276   0.00652   0.00124  -0.0785   0.5303   0.6261
   1.750   0.5552   0.00648   0.00129  -0.0785   0.5238   0.6564
   2.250   0.6090   0.00643   0.00142  -0.0781   0.5084   0.7298
   2.500   0.6354   0.00641   0.00149  -0.0778   0.5007   0.7678
   2.750   0.6617   0.00638   0.00157  -0.0775   0.4921   0.8075
   3.000   0.6868   0.00636   0.00166  -0.0769   0.4826   0.8519
   3.250   0.7103   0.00635   0.00176  -0.0758   0.4724   0.9027
   3.500   0.7390   0.00637   0.00185  -0.0759   0.4621   0.9555
   3.750   0.7753   0.00649   0.00195  -0.0778   0.4497   0.9831
   4.000   0.8101   0.00664   0.00205  -0.0795   0.4348   0.9997
   4.250   0.8354   0.00682   0.00217  -0.0791   0.4183   1.0000
   4.500   0.8602   0.00704   0.00231  -0.0786   0.3989   1.0000
   4.750   0.8837   0.00736   0.00250  -0.0779   0.3668   1.0000
   5.000   0.9041   0.00793   0.00280  -0.0767   0.3112   1.0000
   5.250   0.9239   0.00856   0.00316  -0.0755   0.2576   1.0000
   5.500   0.9443   0.00914   0.00352  -0.0743   0.2120   1.0000
   5.750   0.9636   0.00980   0.00393  -0.0730   0.1635   1.0000
   6.000   0.9835   0.01040   0.00433  -0.0718   0.1247   1.0000
   6.250   1.0046   0.01090   0.00468  -0.0708   0.0984   1.0000
   6.500   1.0259   0.01136   0.00505  -0.0699   0.0780   1.0000
   6.750   1.0470   0.01183   0.00542  -0.0689   0.0595   1.0000
   7.000   1.0663   0.01240   0.00587  -0.0676   0.0387   1.0000
   7.250   1.0864   0.01290   0.00630  -0.0664   0.0260   1.0000
   7.500   1.1035   0.01358   0.00687  -0.0648   0.0099   1.0000
   7.750   1.1241   0.01400   0.00729  -0.0636   0.0075   1.0000
   8.000   1.1446   0.01440   0.00772  -0.0625   0.0067   1.0000
   8.250   1.1643   0.01483   0.00817  -0.0613   0.0059   1.0000
   8.500   1.1840   0.01523   0.00861  -0.0601   0.0056   1.0000
   8.750   1.2026   0.01566   0.00907  -0.0587   0.0054   1.0000
   9.000   1.2189   0.01609   0.00954  -0.0568   0.0051   1.0000
   9.250   1.2337   0.01656   0.01005  -0.0548   0.0050   1.0000
   9.500   1.2476   0.01708   0.01062  -0.0526   0.0047   1.0000
   9.750   1.2613   0.01763   0.01121  -0.0505   0.0046   1.0000
  10.000   1.2738   0.01826   0.01189  -0.0483   0.0045   1.0000
  10.250   1.2860   0.01893   0.01261  -0.0462   0.0043   1.0000
  10.500   1.2968   0.01971   0.01344  -0.0441   0.0042   1.0000
  10.750   1.3056   0.02063   0.01442  -0.0418   0.0040   1.0000
  11.000   1.3100   0.02188   0.01576  -0.0391   0.0038   1.0000
  11.250   1.3206   0.02279   0.01674  -0.0374   0.0038   1.0000
  11.500   1.3298   0.02385   0.01787  -0.0357   0.0038   1.0000
  11.750   1.3388   0.02498   0.01906  -0.0341   0.0037   1.0000
  12.000   1.3485   0.02612   0.02026  -0.0327   0.0036   1.0000
  12.250   1.3529   0.02772   0.02195  -0.0311   0.0036   1.0000
  12.500   1.3635   0.02890   0.02318  -0.0301   0.0034   1.0000
  12.750   1.3694   0.03052   0.02488  -0.0289   0.0034   1.0000
  13.000   1.3767   0.03208   0.02651  -0.0279   0.0033   1.0000
  13.250   1.3812   0.03395   0.02847  -0.0270   0.0033   1.0000
  13.500   1.3854   0.03591   0.03052  -0.0261   0.0032   1.0000
  13.750   1.3891   0.03799   0.03267  -0.0254   0.0031   1.0000
  14.000   1.3910   0.04031   0.03509  -0.0248   0.0031   1.0000
  14.250   1.3940   0.04258   0.03744  -0.0244   0.0031   1.0000
  14.500   1.3947   0.04517   0.04012  -0.0241   0.0030   1.0000
  14.750   1.3962   0.04775   0.04279  -0.0239   0.0030   1.0000
  15.000   1.3955   0.05066   0.04579  -0.0238   0.0030   1.0000
  15.250   1.3952   0.05362   0.04885  -0.0240   0.0029   1.0000
  15.500   1.3923   0.05703   0.05236  -0.0243   0.0029   1.0000
  15.750   1.3913   0.06029   0.05572  -0.0248   0.0028   1.0000
  16.000   1.3900   0.06368   0.05920  -0.0254   0.0028   1.0000
  16.250   1.3870   0.06743   0.06306  -0.0262   0.0028   1.0000
  16.500   1.3851   0.07114   0.06686  -0.0272   0.0027   1.0000
  16.750   1.3805   0.07534   0.07117  -0.0284   0.0027   1.0000
  17.000   1.3746   0.07987   0.07581  -0.0299   0.0027   1.0000
  17.250   1.3693   0.08446   0.08050  -0.0315   0.0027   1.0000
  17.500   1.3632   0.08930   0.08545  -0.0334   0.0027   1.0000
  17.750   1.3524   0.09504   0.09132  -0.0358   0.0027   1.0000
  18.000   1.3461   0.10017   0.09655  -0.0380   0.0026   1.0000
  18.250   1.3368   0.10598   0.10247  -0.0407   0.0026   1.0000
  18.500   1.3244   0.11249   0.10912  -0.0438   0.0026   1.0000
  18.750   1.3162   0.11834   0.11507  -0.0468   0.0026   1.0000
  19.000   1.3051   0.12490   0.12175  -0.0502   0.0026   1.0000
  19.250   1.2953   0.13134   0.12830  -0.0538   0.0026   1.0000
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