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E186 (10.27%) (e186-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: E186 (10.27%) (e186-il)
Reynolds number: 1,000,000
Max Cl/Cd: 73.38 at α=4.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-e186-il-1000000-n5.txt
Download as CSV file: xf-e186-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: E186  (10.27%)                                  
  
 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  -1.0779   0.04747   0.04560  -0.0025   1.0000   0.0044
 -12.250  -1.1008   0.04339   0.04134  -0.0013   1.0000   0.0045
 -12.000  -1.1335   0.03907   0.03674   0.0030   1.0000   0.0045
 -11.750  -1.1390   0.03702   0.03453   0.0064   1.0000   0.0045
 -11.500  -1.1363   0.03494   0.03227   0.0086   1.0000   0.0047
 -11.250  -1.1302   0.03293   0.03008   0.0106   1.0000   0.0048
 -11.000  -1.1222   0.03089   0.02784   0.0126   1.0000   0.0050
 -10.750  -1.1110   0.02908   0.02581   0.0143   1.0000   0.0051
 -10.500  -1.0968   0.02748   0.02401   0.0157   0.9703   0.0053
 -10.250  -1.0869   0.02650   0.02271   0.0187   0.8764   0.0055
 -10.000  -1.0687   0.02586   0.02184   0.0201   0.8369   0.0057
  -9.750  -1.0506   0.02484   0.02059   0.0214   0.8072   0.0058
  -9.500  -1.0294   0.02422   0.01979   0.0222   0.7830   0.0059
  -9.250  -1.0083   0.02347   0.01886   0.0231   0.7618   0.0059
  -9.000  -0.9931   0.02150   0.01657   0.0248   0.7444   0.0062
  -8.750  -0.9741   0.02019   0.01506   0.0260   0.7280   0.0064
  -8.500  -0.9514   0.01952   0.01426   0.0267   0.7135   0.0066
  -8.250  -0.9280   0.01896   0.01357   0.0273   0.6998   0.0068
  -8.000  -0.9041   0.01844   0.01294   0.0279   0.6874   0.0070
  -7.500  -0.8556   0.01739   0.01168   0.0290   0.6659   0.0075
  -7.250  -0.8309   0.01690   0.01109   0.0295   0.6563   0.0078
  -7.000  -0.8063   0.01637   0.01044   0.0301   0.6472   0.0082
  -6.750  -0.7820   0.01570   0.00965   0.0307   0.6390   0.0084
  -6.500  -0.7575   0.01508   0.00892   0.0313   0.6314   0.0086
  -6.250  -0.7328   0.01449   0.00822   0.0319   0.6237   0.0088
  -6.000  -0.7079   0.01394   0.00756   0.0325   0.6170   0.0090
  -5.750  -0.6826   0.01345   0.00700   0.0330   0.6104   0.0092
  -5.500  -0.6573   0.01299   0.00645   0.0336   0.6041   0.0094
  -5.250  -0.6318   0.01257   0.00593   0.0340   0.5979   0.0095
  -5.000  -0.6056   0.01225   0.00555   0.0344   0.5921   0.0097
  -4.750  -0.5791   0.01199   0.00524   0.0347   0.5866   0.0098
  -4.500  -0.5541   0.01145   0.00462   0.0353   0.5810   0.0101
  -4.250  -0.5293   0.01089   0.00394   0.0360   0.5759   0.0107
  -4.000  -0.5033   0.01052   0.00352   0.0365   0.5710   0.0113
  -3.750  -0.4766   0.01026   0.00320   0.0368   0.5656   0.0118
  -3.500  -0.4498   0.01004   0.00293   0.0371   0.5608   0.0124
  -3.250  -0.4228   0.00983   0.00269   0.0373   0.5561   0.0128
  -3.000  -0.3957   0.00966   0.00247   0.0375   0.5512   0.0132
  -2.750  -0.3684   0.00950   0.00227   0.0377   0.5466   0.0137
  -2.500  -0.3410   0.00936   0.00208   0.0379   0.5418   0.0141
  -2.250  -0.3136   0.00923   0.00192   0.0380   0.5370   0.0147
  -2.000  -0.2861   0.00912   0.00178   0.0382   0.5325   0.0157
  -1.750  -0.2587   0.00897   0.00165   0.0384   0.5278   0.0216
  -1.500  -0.2326   0.00865   0.00147   0.0387   0.5232   0.0639
  -1.250  -0.2063   0.00838   0.00135   0.0390   0.5189   0.1083
  -1.000  -0.1803   0.00806   0.00124   0.0393   0.5143   0.1660
  -0.750  -0.1543   0.00777   0.00114   0.0396   0.5096   0.2254
  -0.500  -0.1284   0.00749   0.00106   0.0399   0.5053   0.2900
  -0.250  -0.1029   0.00717   0.00099   0.0403   0.5007   0.3641
   0.000  -0.0798   0.00665   0.00091   0.0411   0.4960   0.4916
   0.250  -0.0604   0.00599   0.00083   0.0428   0.4919   0.6575
   0.500  -0.0406   0.00554   0.00078   0.0446   0.4877   0.7685
   0.750  -0.0173   0.00518   0.00077   0.0459   0.4828   0.8632
   1.000   0.0475   0.00517   0.00092   0.0378   0.4770   0.9255
   1.500   0.1307   0.00545   0.00115   0.0319   0.4653   0.9491
   2.000   0.1897   0.00566   0.00131   0.0314   0.4515   0.9646
   2.500   0.2520   0.00588   0.00148   0.0301   0.4352   0.9734
   2.750   0.2865   0.00599   0.00156   0.0287   0.4257   0.9766
   3.000   0.3175   0.00611   0.00166   0.0280   0.4158   0.9804
   3.250   0.3486   0.00625   0.00176   0.0273   0.4053   0.9833
   3.500   0.3851   0.00634   0.00183   0.0253   0.3928   0.9846
   3.750   0.4200   0.00646   0.00190   0.0237   0.3775   0.9860
   4.000   0.4534   0.00658   0.00198   0.0224   0.3609   0.9874
   4.250   0.4857   0.00673   0.00209   0.0213   0.3418   0.9889
   4.500   0.5166   0.00704   0.00224   0.0203   0.2994   0.9902
   4.750   0.5457   0.00780   0.00257   0.0193   0.2061   0.9913
   5.000   0.5750   0.00826   0.00284   0.0186   0.1616   0.9925
   5.250   0.6037   0.00874   0.00314   0.0179   0.1202   0.9935
   5.500   0.6331   0.00921   0.00345   0.0171   0.0838   0.9943
   5.750   0.6637   0.00967   0.00377   0.0161   0.0525   0.9949
   6.000   0.6937   0.01012   0.00410   0.0151   0.0300   0.9956
   6.250   0.7232   0.01065   0.00451   0.0142   0.0103   0.9963
   6.500   0.7530   0.01098   0.00484   0.0135   0.0067   0.9970
   6.750   0.7825   0.01128   0.00519   0.0128   0.0058   0.9978
   7.000   0.8119   0.01163   0.00557   0.0121   0.0050   0.9985
   7.250   0.8408   0.01205   0.00603   0.0115   0.0044   0.9991
   7.500   0.8693   0.01256   0.00662   0.0109   0.0040   0.9997
   7.750   0.8963   0.01295   0.00705   0.0106   0.0039   1.0000
   8.000   0.9198   0.01341   0.00756   0.0111   0.0038   1.0000
   8.250   0.9430   0.01388   0.00810   0.0116   0.0036   1.0000
   8.500   0.9657   0.01439   0.00866   0.0121   0.0034   1.0000
   8.750   0.9878   0.01496   0.00930   0.0127   0.0033   1.0000
   9.000   1.0091   0.01560   0.01000   0.0133   0.0032   1.0000
   9.250   1.0297   0.01626   0.01073   0.0141   0.0030   1.0000
   9.500   1.0495   0.01697   0.01151   0.0149   0.0029   1.0000
   9.750   1.0683   0.01773   0.01235   0.0158   0.0028   1.0000
  10.000   1.0861   0.01853   0.01323   0.0168   0.0027   1.0000
  10.250   1.1025   0.01940   0.01418   0.0179   0.0026   1.0000
  10.500   1.1175   0.02032   0.01518   0.0191   0.0026   1.0000
  10.750   1.1300   0.02136   0.01631   0.0206   0.0025   1.0000
  11.000   1.1400   0.02249   0.01752   0.0223   0.0024   1.0000
  11.250   1.1475   0.02369   0.01882   0.0242   0.0024   1.0000
  11.500   1.1442   0.02502   0.02023   0.0271   0.0023   1.0000
  11.750   1.1380   0.02679   0.02210   0.0295   0.0023   1.0000
  12.000   1.1369   0.02873   0.02414   0.0306   0.0023   1.0000
  12.250   1.1323   0.03128   0.02681   0.0314   0.0022   1.0000
  12.500   1.1224   0.03458   0.03026   0.0319   0.0021   1.0000
  12.750   1.1173   0.03755   0.03335   0.0321   0.0021   1.0000
  13.000   1.1120   0.04066   0.03658   0.0320   0.0021   1.0000
  13.250   1.1156   0.04290   0.03890   0.0317   0.0021   1.0000
  13.500   1.1089   0.04637   0.04251   0.0312   0.0021   1.0000
  13.750   1.1075   0.04933   0.04558   0.0306   0.0021   1.0000
  14.000   1.1029   0.05276   0.04911   0.0297   0.0021   1.0000
  14.250   1.0918   0.05714   0.05363   0.0285   0.0021   1.0000
  14.500   1.0839   0.06130   0.05791   0.0271   0.0020   1.0000
  14.750   1.0778   0.06546   0.06217   0.0254   0.0020   1.0000
  15.000   1.0689   0.07025   0.06708   0.0234   0.0020   1.0000
  15.250   1.0527   0.07640   0.07337   0.0208   0.0020   1.0000
  15.500   1.0411   0.08206   0.07914   0.0182   0.0020   1.0000
  15.750   1.0263   0.08851   0.08571   0.0152   0.0021   1.0000
  16.000   1.0182   0.09404   0.09134   0.0125   0.0020   1.0000
  16.250   0.9986   0.10181   0.09923   0.0088   0.0020   1.0000
  16.500   0.9810   0.10952   0.10706   0.0052   0.0021   1.0000
  16.750   0.9669   0.11677   0.11441   0.0017   0.0021   1.0000
  17.000   0.9431   0.12638   0.12414  -0.0029   0.0021   1.0000
  17.250   0.9172   0.13694   0.13482  -0.0078   0.0021   1.0000
  17.500   0.9088   0.14356   0.14150  -0.0109   0.0021   1.0000
  17.750   0.8779   0.15638   0.15442  -0.0168   0.0021   1.0000
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