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E195 (11.82%) (e195-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: E195 (11.82%) (e195-il)
Reynolds number: 1,000,000
Max Cl/Cd: 124.2 at α=4.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-e195-il-1000000-n5.txt
Download as CSV file: xf-e195-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: E195  (11.82%)                                  
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -12.250  -0.5766   0.08187   0.08014  -0.0433   1.0000   0.0071
 -12.000  -0.7165   0.04725   0.04518  -0.0672   1.0000   0.0066
 -11.750  -0.7441   0.03866   0.03637  -0.0761   1.0000   0.0066
 -11.500  -0.7692   0.03515   0.03271  -0.0756   1.0000   0.0066
 -11.250  -0.7728   0.03219   0.02954  -0.0755   0.9911   0.0067
 -11.000  -0.7570   0.02897   0.02602  -0.0784   0.9825   0.0068
 -10.750  -0.7346   0.02687   0.02370  -0.0804   0.9702   0.0069
 -10.500  -0.7109   0.02488   0.02146  -0.0821   0.9481   0.0070
 -10.250  -0.6922   0.02327   0.01955  -0.0821   0.9095   0.0070
 -10.000  -0.6759   0.02238   0.01840  -0.0808   0.8745   0.0071
  -9.750  -0.6604   0.02123   0.01699  -0.0795   0.8478   0.0072
  -9.500  -0.6418   0.02040   0.01595  -0.0785   0.8254   0.0072
  -9.250  -0.6219   0.01958   0.01493  -0.0776   0.8062   0.0073
  -9.000  -0.6009   0.01884   0.01400  -0.0769   0.7895   0.0073
  -8.750  -0.5815   0.01767   0.01262  -0.0760   0.7753   0.0074
  -8.500  -0.5630   0.01630   0.01102  -0.0750   0.7619   0.0076
  -8.250  -0.5412   0.01544   0.01001  -0.0743   0.7494   0.0077
  -8.000  -0.5183   0.01473   0.00916  -0.0737   0.7378   0.0078
  -7.750  -0.4942   0.01417   0.00850  -0.0732   0.7278   0.0080
  -7.500  -0.4697   0.01368   0.00790  -0.0728   0.7180   0.0081
  -7.250  -0.4446   0.01327   0.00741  -0.0725   0.7087   0.0083
  -7.000  -0.4192   0.01286   0.00692  -0.0722   0.7004   0.0086
  -6.500  -0.3682   0.01205   0.00594  -0.0716   0.6849   0.0090
  -6.000  -0.3163   0.01131   0.00503  -0.0710   0.6713   0.0095
  -5.750  -0.2901   0.01100   0.00464  -0.0708   0.6646   0.0098
  -5.500  -0.2635   0.01071   0.00429  -0.0706   0.6588   0.0100
  -5.250  -0.2368   0.01045   0.00396  -0.0704   0.6527   0.0103
  -5.000  -0.2099   0.01022   0.00367  -0.0702   0.6473   0.0104
  -4.750  -0.1827   0.01000   0.00341  -0.0701   0.6419   0.0106
  -4.500  -0.1561   0.00970   0.00303  -0.0699   0.6363   0.0110
  -4.250  -0.1290   0.00946   0.00274  -0.0698   0.6316   0.0115
  -4.000  -0.1016   0.00926   0.00250  -0.0697   0.6267   0.0121
  -3.750  -0.0743   0.00910   0.00230  -0.0696   0.6215   0.0128
  -3.500  -0.0467   0.00896   0.00212  -0.0696   0.6171   0.0138
  -3.250  -0.0189   0.00884   0.00196  -0.0695   0.6126   0.0147
  -3.000   0.0087   0.00870   0.00181  -0.0695   0.6078   0.0175
  -2.750   0.0356   0.00845   0.00164  -0.0694   0.6034   0.0412
  -2.500   0.0632   0.00827   0.00152  -0.0693   0.5994   0.0605
  -2.250   0.0906   0.00809   0.00142  -0.0693   0.5949   0.0867
  -2.000   0.1178   0.00791   0.00133  -0.0693   0.5904   0.1191
  -1.500   0.1722   0.00747   0.00118  -0.0693   0.5824   0.2138
  -1.250   0.1996   0.00733   0.00113  -0.0692   0.5779   0.2523
  -1.000   0.2265   0.00710   0.00109  -0.0692   0.5739   0.3166
  -0.750   0.2533   0.00684   0.00107  -0.0691   0.5699   0.3939
  -0.500   0.2808   0.00673   0.00106  -0.0691   0.5655   0.4370
  -0.250   0.3085   0.00669   0.00106  -0.0691   0.5611   0.4633
   0.000   0.3364   0.00662   0.00106  -0.0691   0.5573   0.4932
   0.250   0.3642   0.00656   0.00107  -0.0691   0.5529   0.5221
   0.500   0.3918   0.00651   0.00108  -0.0691   0.5483   0.5513
   1.000   0.4469   0.00639   0.00114  -0.0691   0.5398   0.6164
   1.250   0.4741   0.00633   0.00117  -0.0689   0.5349   0.6543
   1.500   0.5010   0.00627   0.00122  -0.0688   0.5304   0.6951
   1.750   0.5279   0.00619   0.00127  -0.0686   0.5253   0.7389
   2.000   0.5538   0.00611   0.00133  -0.0681   0.5192   0.7903
   2.250   0.5786   0.00600   0.00140  -0.0674   0.5131   0.8514
   2.500   0.6028   0.00592   0.00149  -0.0664   0.5057   0.9194
   2.750   0.6369   0.00597   0.00156  -0.0677   0.4972   0.9610
   3.000   0.6717   0.00607   0.00164  -0.0693   0.4877   0.9772
   3.250   0.7058   0.00616   0.00170  -0.0707   0.4783   0.9861
   3.500   0.7400   0.00627   0.00178  -0.0722   0.4677   0.9923
   3.750   0.7735   0.00639   0.00186  -0.0736   0.4557   0.9974
   4.000   0.8036   0.00653   0.00197  -0.0742   0.4433   1.0000
   4.250   0.8279   0.00669   0.00208  -0.0735   0.4295   1.0000
   4.500   0.8520   0.00686   0.00220  -0.0729   0.4137   1.0000
   4.750   0.8751   0.00712   0.00236  -0.0720   0.3889   1.0000
   5.000   0.8966   0.00750   0.00258  -0.0710   0.3512   1.0000
   5.250   0.9172   0.00799   0.00286  -0.0698   0.3082   1.0000
   5.500   0.9340   0.00876   0.00330  -0.0681   0.2433   1.0000
   5.750   0.9513   0.00951   0.00374  -0.0664   0.1861   1.0000
   6.000   0.9712   0.01006   0.00412  -0.0652   0.1498   1.0000
   6.250   0.9912   0.01060   0.00450  -0.0640   0.1184   1.0000
   6.500   1.0117   0.01109   0.00487  -0.0629   0.0947   1.0000
   6.750   1.0325   0.01155   0.00523  -0.0619   0.0746   1.0000
   7.000   1.0525   0.01205   0.00564  -0.0607   0.0558   1.0000
   7.250   1.0711   0.01262   0.00610  -0.0593   0.0365   1.0000
   7.500   1.0888   0.01323   0.00661  -0.0578   0.0199   1.0000
   7.750   1.1056   0.01388   0.00718  -0.0561   0.0081   1.0000
   8.000   1.1254   0.01430   0.00761  -0.0549   0.0066   1.0000
   8.250   1.1453   0.01469   0.00804  -0.0538   0.0060   1.0000
   8.500   1.1646   0.01509   0.00847  -0.0525   0.0057   1.0000
   8.750   1.1829   0.01551   0.00892  -0.0511   0.0054   1.0000
   9.000   1.1982   0.01596   0.00941  -0.0491   0.0051   1.0000
   9.250   1.2121   0.01644   0.00992  -0.0469   0.0050   1.0000
   9.500   1.2254   0.01696   0.01048  -0.0447   0.0047   1.0000
   9.750   1.2377   0.01756   0.01113  -0.0425   0.0045   1.0000
  10.000   1.2488   0.01825   0.01188  -0.0402   0.0044   1.0000
  10.250   1.2581   0.01908   0.01277  -0.0378   0.0042   1.0000
  10.500   1.2678   0.01993   0.01369  -0.0357   0.0040   1.0000
  10.750   1.2784   0.02078   0.01459  -0.0338   0.0039   1.0000
  11.000   1.2895   0.02164   0.01551  -0.0322   0.0039   1.0000
  11.250   1.2990   0.02266   0.01659  -0.0305   0.0038   1.0000
  11.500   1.3087   0.02372   0.01772  -0.0290   0.0037   1.0000
  11.750   1.3187   0.02481   0.01887  -0.0276   0.0036   1.0000
  12.000   1.3265   0.02613   0.02025  -0.0263   0.0035   1.0000
  12.250   1.3345   0.02749   0.02168  -0.0250   0.0034   1.0000
  12.500   1.3396   0.02915   0.02342  -0.0238   0.0033   1.0000
  12.750   1.3470   0.03068   0.02502  -0.0228   0.0033   1.0000
  13.000   1.3536   0.03232   0.02673  -0.0219   0.0032   1.0000
  13.250   1.3579   0.03422   0.02871  -0.0210   0.0032   1.0000
  13.500   1.3615   0.03625   0.03082  -0.0202   0.0031   1.0000
  13.750   1.3645   0.03839   0.03304  -0.0196   0.0031   1.0000
  14.000   1.3684   0.04050   0.03524  -0.0191   0.0030   1.0000
  14.250   1.3707   0.04280   0.03762  -0.0186   0.0030   1.0000
  14.500   1.3730   0.04519   0.04009  -0.0183   0.0030   1.0000
  14.750   1.3741   0.04778   0.04276  -0.0181   0.0029   1.0000
  15.000   1.3746   0.05052   0.04559  -0.0181   0.0029   1.0000
  15.250   1.3753   0.05332   0.04847  -0.0182   0.0028   1.0000
  15.500   1.3739   0.05647   0.05171  -0.0184   0.0028   1.0000
  15.750   1.3730   0.05965   0.05498  -0.0188   0.0028   1.0000
  16.000   1.3706   0.06312   0.05855  -0.0194   0.0027   1.0000
  16.250   1.3687   0.06664   0.06216  -0.0201   0.0027   1.0000
  16.500   1.3634   0.07074   0.06636  -0.0211   0.0027   1.0000
  16.750   1.3584   0.07494   0.07067  -0.0223   0.0027   1.0000
  17.000   1.3511   0.07957   0.07541  -0.0238   0.0026   1.0000
  17.250   1.3462   0.08401   0.07995  -0.0253   0.0026   1.0000
  17.500   1.3352   0.08955   0.08563  -0.0273   0.0026   1.0000
  17.750   1.3283   0.09454   0.09073  -0.0293   0.0026   1.0000
  18.000   1.3174   0.10036   0.09667  -0.0318   0.0025   1.0000
  18.250   1.3076   0.10617   0.10259  -0.0344   0.0025   1.0000
  18.500   1.2989   0.11189   0.10843  -0.0371   0.0025   1.0000
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