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E195 (11.82%) (e195-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: E195 (11.82%) (e195-il)
Reynolds number: 500,000
Max Cl/Cd: 105.19 at α=5.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-e195-il-500000-n5.txt
Download as CSV file: xf-e195-il-500000-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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -10.250  -0.5850   0.04683   0.04441  -0.0685   1.0000   0.0091
 -10.000  -0.6163   0.04161   0.03902  -0.0708   0.9942   0.0092
  -9.750  -0.6182   0.03487   0.03176  -0.0764   0.9764   0.0092
  -9.500  -0.6051   0.03069   0.02713  -0.0790   0.9584   0.0093
  -9.250  -0.5860   0.02752   0.02354  -0.0807   0.9358   0.0095
  -9.000  -0.5651   0.02529   0.02093  -0.0814   0.9094   0.0097
  -8.750  -0.5481   0.02347   0.01875  -0.0807   0.8822   0.0098
  -8.500  -0.5302   0.02216   0.01712  -0.0796   0.8579   0.0100
  -8.250  -0.5114   0.02094   0.01561  -0.0785   0.8373   0.0101
  -8.000  -0.4911   0.01989   0.01430  -0.0776   0.8192   0.0102
  -7.750  -0.4688   0.01919   0.01336  -0.0769   0.8034   0.0104
  -7.500  -0.4460   0.01853   0.01250  -0.0763   0.7890   0.0106
  -7.250  -0.4262   0.01700   0.01073  -0.0753   0.7758   0.0109
  -7.000  -0.4038   0.01608   0.00965  -0.0746   0.7640   0.0111
  -6.750  -0.3805   0.01532   0.00875  -0.0740   0.7529   0.0114
  -6.500  -0.3566   0.01467   0.00798  -0.0735   0.7425   0.0116
  -6.250  -0.3323   0.01411   0.00731  -0.0730   0.7329   0.0119
  -6.000  -0.3076   0.01360   0.00670  -0.0725   0.7238   0.0122
  -5.750  -0.2824   0.01313   0.00614  -0.0721   0.7155   0.0126
  -5.250  -0.2313   0.01233   0.00513  -0.0714   0.6998   0.0134
  -4.750  -0.1790   0.01168   0.00430  -0.0708   0.6859   0.0142
  -4.500  -0.1525   0.01143   0.00397  -0.0706   0.6793   0.0147
  -4.250  -0.1261   0.01108   0.00355  -0.0704   0.6732   0.0160
  -4.000  -0.0994   0.01084   0.00324  -0.0702   0.6671   0.0173
  -3.750  -0.0724   0.01064   0.00297  -0.0700   0.6615   0.0187
  -3.500  -0.0453   0.01043   0.00273  -0.0698   0.6557   0.0220
  -3.250  -0.0188   0.01014   0.00250  -0.0696   0.6503   0.0420
  -3.000   0.0080   0.00989   0.00232  -0.0695   0.6454   0.0670
  -2.750   0.0347   0.00962   0.00216  -0.0694   0.6399   0.1016
  -2.500   0.0613   0.00939   0.00203  -0.0693   0.6350   0.1403
  -2.250   0.0878   0.00910   0.00191  -0.0692   0.6303   0.1952
  -2.000   0.1146   0.00886   0.00182  -0.0691   0.6253   0.2440
  -1.750   0.1414   0.00867   0.00174  -0.0690   0.6206   0.2888
  -1.500   0.1676   0.00837   0.00169  -0.0689   0.6163   0.3722
  -1.250   0.1941   0.00814   0.00167  -0.0688   0.6114   0.4400
  -1.000   0.2211   0.00804   0.00164  -0.0686   0.6068   0.4797
  -0.750   0.2484   0.00797   0.00162  -0.0685   0.6027   0.5106
  -0.500   0.2757   0.00787   0.00162  -0.0684   0.5981   0.5440
  -0.250   0.3028   0.00780   0.00162  -0.0683   0.5935   0.5785
   0.000   0.3295   0.00773   0.00162  -0.0680   0.5893   0.6147
   0.250   0.3565   0.00763   0.00164  -0.0678   0.5849   0.6536
   0.500   0.3829   0.00754   0.00167  -0.0675   0.5803   0.6968
   0.750   0.4087   0.00745   0.00171  -0.0670   0.5760   0.7443
   1.000   0.4341   0.00733   0.00176  -0.0664   0.5718   0.7959
   1.250   0.4588   0.00722   0.00183  -0.0655   0.5672   0.8552
   1.500   0.4885   0.00718   0.00191  -0.0655   0.5626   0.9173
   1.750   0.5281   0.00723   0.00196  -0.0680   0.5580   0.9574
   2.000   0.5660   0.00728   0.00201  -0.0702   0.5527   0.9766
   2.250   0.6026   0.00735   0.00206  -0.0722   0.5476   0.9877
   2.500   0.6389   0.00741   0.00211  -0.0741   0.5420   0.9958
   2.750   0.6709   0.00748   0.00216  -0.0751   0.5354   1.0000
   3.000   0.6957   0.00757   0.00224  -0.0745   0.5290   1.0000
   3.250   0.7206   0.00766   0.00231  -0.0739   0.5211   1.0000
   3.500   0.7454   0.00776   0.00239  -0.0733   0.5133   1.0000
   3.750   0.7701   0.00786   0.00248  -0.0727   0.5047   1.0000
   4.000   0.7952   0.00797   0.00260  -0.0722   0.4959   1.0000
   4.250   0.8199   0.00810   0.00270  -0.0716   0.4862   1.0000
   4.500   0.8446   0.00823   0.00282  -0.0711   0.4751   1.0000
   4.750   0.8695   0.00837   0.00297  -0.0705   0.4633   1.0000
   5.000   0.8941   0.00854   0.00311  -0.0700   0.4496   1.0000
   5.250   0.9183   0.00873   0.00328  -0.0693   0.4342   1.0000
   5.500   0.9419   0.00897   0.00346  -0.0686   0.4154   1.0000
   5.750   0.9636   0.00933   0.00371  -0.0676   0.3812   1.0000
   6.000   0.9811   0.01000   0.00409  -0.0660   0.3234   1.0000
   6.250   0.9978   0.01076   0.00457  -0.0643   0.2679   1.0000
   6.500   1.0141   0.01155   0.00509  -0.0626   0.2179   1.0000
   6.750   1.0299   0.01236   0.00565  -0.0609   0.1699   1.0000
   7.000   1.0459   0.01314   0.00622  -0.0592   0.1305   1.0000
   7.250   1.0633   0.01378   0.00674  -0.0577   0.1037   1.0000
   7.500   1.0806   0.01441   0.00725  -0.0562   0.0824   1.0000
   7.750   1.0964   0.01508   0.00782  -0.0545   0.0607   1.0000
   8.000   1.1116   0.01577   0.00841  -0.0526   0.0432   1.0000
   8.250   1.1245   0.01653   0.00908  -0.0505   0.0269   1.0000
   8.500   1.1345   0.01730   0.00979  -0.0478   0.0145   1.0000
   8.750   1.1446   0.01800   0.01049  -0.0451   0.0102   1.0000
   9.000   1.1562   0.01868   0.01120  -0.0427   0.0086   1.0000
   9.250   1.1690   0.01932   0.01189  -0.0407   0.0080   1.0000
   9.500   1.1809   0.02003   0.01267  -0.0387   0.0076   1.0000
   9.750   1.1920   0.02083   0.01353  -0.0367   0.0072   1.0000
  10.000   1.2016   0.02176   0.01454  -0.0347   0.0068   1.0000
  10.250   1.2102   0.02282   0.01567  -0.0327   0.0065   1.0000
  10.500   1.2169   0.02407   0.01701  -0.0307   0.0062   1.0000
  10.750   1.2260   0.02522   0.01824  -0.0292   0.0060   1.0000
  11.000   1.2340   0.02651   0.01962  -0.0277   0.0060   1.0000
  11.250   1.2413   0.02793   0.02112  -0.0264   0.0059   1.0000
  11.500   1.2482   0.02944   0.02272  -0.0251   0.0057   1.0000
  11.750   1.2541   0.03111   0.02447  -0.0240   0.0057   1.0000
  12.000   1.2594   0.03287   0.02633  -0.0230   0.0055   1.0000
  12.250   1.2638   0.03479   0.02835  -0.0220   0.0054   1.0000
  12.500   1.2666   0.03691   0.03057  -0.0212   0.0053   1.0000
  12.750   1.2706   0.03897   0.03271  -0.0205   0.0052   1.0000
  13.000   1.2750   0.04104   0.03487  -0.0200   0.0051   1.0000
  13.250   1.2763   0.04348   0.03741  -0.0194   0.0050   1.0000
  13.500   1.2772   0.04602   0.04003  -0.0190   0.0048   1.0000
  13.750   1.2784   0.04860   0.04272  -0.0187   0.0049   1.0000
  14.000   1.2807   0.05113   0.04533  -0.0187   0.0047   1.0000
  14.250   1.2798   0.05410   0.04839  -0.0186   0.0046   1.0000
  14.500   1.2808   0.05696   0.05134  -0.0188   0.0045   1.0000
  14.750   1.2792   0.06021   0.05469  -0.0191   0.0044   1.0000
  15.000   1.2776   0.06355   0.05814  -0.0196   0.0044   1.0000
  15.250   1.2706   0.06771   0.06241  -0.0202   0.0042   1.0000
  15.500   1.2675   0.07147   0.06629  -0.0210   0.0042   1.0000
  15.750   1.2647   0.07529   0.07021  -0.0219   0.0042   1.0000
  16.000   1.2603   0.07943   0.07447  -0.0230   0.0041   1.0000
  16.250   1.2550   0.08384   0.07900  -0.0242   0.0041   1.0000
  16.500   1.2488   0.08846   0.08376  -0.0256   0.0041   1.0000
  16.750   1.2450   0.09293   0.08835  -0.0273   0.0040   1.0000
  17.000   1.2405   0.09763   0.09318  -0.0291   0.0040   1.0000
  17.250   1.2349   0.10258   0.09826  -0.0312   0.0040   1.0000
  17.500   1.2290   0.10777   0.10358  -0.0335   0.0040   1.0000
  17.750   1.2224   0.11314   0.10908  -0.0360   0.0040   1.0000
  18.000   1.2159   0.11869   0.11477  -0.0388   0.0040   1.0000
  18.250   1.2081   0.12460   0.12082  -0.0419   0.0039   1.0000
  18.500   1.2005   0.13056   0.12691  -0.0451   0.0039   1.0000
  18.750   1.1920   0.13690   0.13339  -0.0486   0.0039   1.0000
  19.000   1.1828   0.14344   0.14006  -0.0524   0.0039   1.0000
  19.250   1.1734   0.15020   0.14696  -0.0564   0.0039   1.0000
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