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E203 (13.64%) (e203-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: E203 (13.64%) (e203-il)
Reynolds number: 1,000,000
Max Cl/Cd: 108.55 at α=4.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-e203-il-1000000-n5.txt
Download as CSV file: xf-e203-il-1000000-n5.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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -17.750  -0.5262   0.18798   0.18614  -0.0083   1.0000   0.0043
 -17.250  -0.7326   0.12117   0.11910  -0.0342   1.0000   0.0067
 -17.000  -0.7829   0.10679   0.10454  -0.0414   1.0000   0.0067
 -16.750  -0.8166   0.09636   0.09399  -0.0469   1.0000   0.0067
 -16.500  -0.8504   0.08634   0.08383  -0.0523   1.0000   0.0066
 -16.250  -0.8751   0.07820   0.07557  -0.0568   1.0000   0.0066
 -16.000  -0.8955   0.07105   0.06830  -0.0608   1.0000   0.0066
 -15.750  -0.9073   0.06560   0.06275  -0.0639   1.0000   0.0067
 -15.500  -0.9258   0.05952   0.05655  -0.0672   1.0000   0.0067
 -15.250  -0.9415   0.05413   0.05105  -0.0701   1.0000   0.0067
 -15.000  -0.9486   0.05007   0.04690  -0.0722   1.0000   0.0068
 -14.750  -0.9575   0.04594   0.04267  -0.0742   1.0000   0.0068
 -14.500  -0.9665   0.04197   0.03859  -0.0760   1.0000   0.0069
 -14.250  -0.9686   0.03894   0.03548  -0.0773   1.0000   0.0070
 -14.000  -0.9711   0.03603   0.03246  -0.0783   1.0000   0.0070
 -13.750  -0.9745   0.03323   0.02957  -0.0790   1.0000   0.0071
 -13.500  -0.9763   0.03091   0.02715  -0.0791   1.0000   0.0072
 -13.250  -0.9751   0.02919   0.02537  -0.0786   1.0000   0.0074
 -13.000  -0.9783   0.02761   0.02372  -0.0772   1.0000   0.0075
 -12.750  -0.9786   0.02587   0.02187  -0.0765   0.9988   0.0075
 -12.500  -0.9592   0.02464   0.02054  -0.0777   0.9958   0.0077
 -12.250  -0.9367   0.02346   0.01926  -0.0789   0.9930   0.0078
 -12.000  -0.9159   0.02233   0.01802  -0.0796   0.9898   0.0079
 -11.750  -0.8903   0.02149   0.01710  -0.0806   0.9871   0.0081
 -11.500  -0.8634   0.02055   0.01606  -0.0820   0.9848   0.0082
 -11.250  -0.8341   0.01975   0.01518  -0.0835   0.9832   0.0083
 -11.000  -0.8146   0.01881   0.01415  -0.0832   0.9780   0.0084
 -10.750  -0.7907   0.01761   0.01285  -0.0840   0.9735   0.0088
 -10.250  -0.7402   0.01618   0.01131  -0.0847   0.9619   0.0092
 -10.000  -0.7115   0.01555   0.01062  -0.0857   0.9551   0.0094
  -9.750  -0.6837   0.01498   0.00997  -0.0863   0.9434   0.0097
  -9.500  -0.6543   0.01440   0.00932  -0.0871   0.9267   0.0099
  -9.250  -0.6275   0.01392   0.00870  -0.0873   0.9022   0.0102
  -9.000  -0.6042   0.01353   0.00816  -0.0868   0.8750   0.0105
  -8.750  -0.5817   0.01318   0.00766  -0.0860   0.8515   0.0107
  -8.500  -0.5585   0.01288   0.00723  -0.0853   0.8303   0.0110
  -8.250  -0.5350   0.01261   0.00684  -0.0847   0.8113   0.0113
  -8.000  -0.5107   0.01237   0.00649  -0.0842   0.7943   0.0115
  -7.750  -0.4863   0.01209   0.00611  -0.0838   0.7791   0.0116
  -7.500  -0.4619   0.01178   0.00571  -0.0833   0.7653   0.0119
  -7.250  -0.4377   0.01139   0.00520  -0.0828   0.7521   0.0123
  -7.000  -0.4126   0.01107   0.00480  -0.0825   0.7400   0.0127
  -6.750  -0.3870   0.01081   0.00447  -0.0822   0.7291   0.0132
  -6.500  -0.3611   0.01058   0.00417  -0.0820   0.7189   0.0137
  -6.250  -0.3349   0.01037   0.00390  -0.0818   0.7088   0.0142
  -6.000  -0.3084   0.01018   0.00364  -0.0816   0.6996   0.0149
  -5.750  -0.2818   0.01001   0.00341  -0.0814   0.6911   0.0154
  -5.500  -0.2548   0.00984   0.00319  -0.0814   0.6828   0.0164
  -5.250  -0.2281   0.00965   0.00297  -0.0812   0.6751   0.0188
  -5.000  -0.2011   0.00946   0.00275  -0.0811   0.6677   0.0231
  -4.750  -0.1749   0.00916   0.00252  -0.0810   0.6609   0.0420
  -4.500  -0.1479   0.00895   0.00234  -0.0810   0.6539   0.0573
  -4.000  -0.0940   0.00850   0.00200  -0.0809   0.6415   0.1005
  -3.750  -0.0669   0.00832   0.00187  -0.0809   0.6351   0.1233
  -3.500  -0.0399   0.00809   0.00173  -0.0809   0.6296   0.1546
  -3.250  -0.0130   0.00780   0.00159  -0.0809   0.6240   0.1992
  -3.000   0.0140   0.00759   0.00147  -0.0809   0.6185   0.2368
  -2.750   0.0416   0.00741   0.00138  -0.0809   0.6134   0.2687
  -2.500   0.0686   0.00716   0.00129  -0.0810   0.6080   0.3193
  -2.000   0.1238   0.00689   0.00122  -0.0810   0.5982   0.3999
  -1.750   0.1520   0.00687   0.00120  -0.0811   0.5929   0.4119
  -1.250   0.2086   0.00685   0.00117  -0.0813   0.5835   0.4327
  -1.000   0.2369   0.00684   0.00116  -0.0814   0.5784   0.4421
  -0.500   0.2934   0.00685   0.00116  -0.0815   0.5692   0.4585
  -0.250   0.3217   0.00685   0.00117  -0.0816   0.5642   0.4662
   0.000   0.3498   0.00688   0.00118  -0.0817   0.5593   0.4736
   0.250   0.3781   0.00688   0.00120  -0.0818   0.5549   0.4805
   0.500   0.4064   0.00689   0.00122  -0.0819   0.5498   0.4882
   0.750   0.4343   0.00691   0.00124  -0.0819   0.5449   0.4966
   1.000   0.4626   0.00693   0.00127  -0.0820   0.5403   0.5053
   1.250   0.4907   0.00694   0.00131  -0.0820   0.5350   0.5126
   1.500   0.5185   0.00699   0.00135  -0.0821   0.5297   0.5201
   1.750   0.5467   0.00700   0.00139  -0.0821   0.5239   0.5272
   2.000   0.5743   0.00706   0.00145  -0.0821   0.5162   0.5353
   2.250   0.6021   0.00709   0.00150  -0.0821   0.5082   0.5434
   2.750   0.6572   0.00720   0.00163  -0.0821   0.4922   0.5616
   3.000   0.6844   0.00726   0.00171  -0.0820   0.4833   0.5721
   3.250   0.7117   0.00733   0.00179  -0.0819   0.4732   0.5832
   3.500   0.7388   0.00740   0.00188  -0.0818   0.4625   0.5952
   3.750   0.7656   0.00749   0.00199  -0.0817   0.4514   0.6085
   4.000   0.7921   0.00759   0.00210  -0.0815   0.4386   0.6237
   4.250   0.8184   0.00770   0.00222  -0.0812   0.4249   0.6405
   4.500   0.8443   0.00784   0.00237  -0.0809   0.4081   0.6584
   4.750   0.8695   0.00801   0.00253  -0.0805   0.3878   0.6775
   5.000   0.8937   0.00824   0.00273  -0.0800   0.3617   0.6990
   5.250   0.9165   0.00855   0.00297  -0.0792   0.3288   0.7249
   5.500   0.9361   0.00906   0.00334  -0.0779   0.2795   0.7545
   5.750   0.9533   0.00971   0.00379  -0.0761   0.2226   0.7876
   6.000   0.9731   0.01009   0.00413  -0.0748   0.1909   0.8255
   6.250   0.9917   0.01040   0.00446  -0.0731   0.1657   0.8742
   6.500   1.0106   0.01080   0.00486  -0.0715   0.1314   0.9644
   6.750   1.0340   0.01138   0.00529  -0.0711   0.1018   1.0000
   7.000   1.0543   0.01184   0.00565  -0.0700   0.0827   1.0000
   7.250   1.0740   0.01232   0.00603  -0.0687   0.0661   1.0000
   7.750   1.1123   0.01326   0.00683  -0.0660   0.0410   1.0000
   8.000   1.1307   0.01374   0.00726  -0.0646   0.0313   1.0000
   8.250   1.1484   0.01421   0.00770  -0.0630   0.0243   1.0000
   8.500   1.1633   0.01469   0.00815  -0.0609   0.0176   1.0000
   8.750   1.1752   0.01528   0.00869  -0.0583   0.0105   1.0000
   9.000   1.1887   0.01581   0.00922  -0.0560   0.0075   1.0000
   9.250   1.2040   0.01629   0.00972  -0.0541   0.0066   1.0000
   9.500   1.2181   0.01682   0.01029  -0.0520   0.0058   1.0000
   9.750   1.2319   0.01739   0.01088  -0.0500   0.0054   1.0000
  10.000   1.2456   0.01797   0.01151  -0.0481   0.0051   1.0000
  10.250   1.2594   0.01857   0.01215  -0.0462   0.0049   1.0000
  10.500   1.2725   0.01922   0.01284  -0.0444   0.0047   1.0000
  10.750   1.2847   0.01995   0.01362  -0.0425   0.0045   1.0000
  11.000   1.2967   0.02072   0.01444  -0.0408   0.0044   1.0000
  11.250   1.3076   0.02159   0.01536  -0.0390   0.0043   1.0000
  11.500   1.3177   0.02255   0.01638  -0.0372   0.0042   1.0000
  11.750   1.3275   0.02358   0.01746  -0.0356   0.0040   1.0000
  12.000   1.3372   0.02467   0.01860  -0.0341   0.0039   1.0000
  12.250   1.3457   0.02589   0.01989  -0.0326   0.0039   1.0000
  12.500   1.3523   0.02732   0.02138  -0.0311   0.0037   1.0000
  12.750   1.3588   0.02883   0.02295  -0.0298   0.0035   1.0000
  13.000   1.3640   0.03050   0.02470  -0.0286   0.0035   1.0000
  13.250   1.3649   0.03262   0.02691  -0.0273   0.0033   1.0000
  13.500   1.3714   0.03432   0.02869  -0.0264   0.0033   1.0000
  13.750   1.3758   0.03626   0.03071  -0.0256   0.0032   1.0000
  14.000   1.3830   0.03798   0.03250  -0.0250   0.0032   1.0000
  14.250   1.3898   0.03979   0.03437  -0.0245   0.0031   1.0000
  14.500   1.3916   0.04216   0.03682  -0.0239   0.0031   1.0000
  14.750   1.3960   0.04433   0.03907  -0.0236   0.0030   1.0000
  15.000   1.3972   0.04690   0.04173  -0.0233   0.0030   1.0000
  15.250   1.4013   0.04923   0.04413  -0.0232   0.0029   1.0000
  15.500   1.4016   0.05206   0.04705  -0.0232   0.0029   1.0000
  15.750   1.4012   0.05506   0.05014  -0.0234   0.0029   1.0000
  16.000   1.4019   0.05803   0.05320  -0.0237   0.0028   1.0000
  16.250   1.3999   0.06142   0.05669  -0.0242   0.0028   1.0000
  16.500   1.4000   0.06463   0.06000  -0.0248   0.0027   1.0000
  16.750   1.3976   0.06828   0.06375  -0.0256   0.0027   1.0000
  17.000   1.3925   0.07244   0.06801  -0.0267   0.0026   1.0000
  17.250   1.3896   0.07636   0.07203  -0.0278   0.0027   1.0000
  17.500   1.3846   0.08071   0.07648  -0.0292   0.0026   1.0000
  17.750   1.3791   0.08526   0.08114  -0.0308   0.0026   1.0000
  18.000   1.3720   0.09022   0.08621  -0.0327   0.0026   1.0000
  18.250   1.3652   0.09521   0.09131  -0.0347   0.0026   1.0000
  18.500   1.3557   0.10081   0.09702  -0.0371   0.0025   1.0000
  18.750   1.3479   0.10623   0.10255  -0.0396   0.0025   1.0000
  19.000   1.3368   0.11238   0.10883  -0.0426   0.0025   1.0000
  19.250   1.3270   0.11841   0.11497  -0.0456   0.0025   1.0000
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