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NLF(1)-0115 (nlf0115-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: NLF(1)-0115 (nlf0115-il)
Reynolds number: 1,000,000
Max Cl/Cd: 76.26 at α=7.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-nlf0115-il-1000000-n5.txt
Download as CSV file: xf-nlf0115-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NLF(1)-0115                                     
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -15.000  -0.7768   0.06319   0.06072  -0.0751   1.0000   0.0076
 -14.750  -0.7986   0.05732   0.05468  -0.0773   1.0000   0.0074
 -14.500  -0.8355   0.05080   0.04794  -0.0785   1.0000   0.0075
 -14.250  -0.8575   0.04668   0.04366  -0.0779   1.0000   0.0075
 -14.000  -0.8720   0.04369   0.04054  -0.0766   1.0000   0.0076
 -13.750  -0.8756   0.04037   0.03705  -0.0775   0.9991   0.0076
 -13.500  -0.8740   0.03747   0.03401  -0.0786   0.9975   0.0077
 -13.250  -0.8717   0.03467   0.03101  -0.0792   0.9952   0.0076
 -13.000  -0.8628   0.03280   0.02904  -0.0796   0.9928   0.0077
 -12.750  -0.8544   0.03075   0.02684  -0.0799   0.9901   0.0078
 -12.500  -0.8404   0.02920   0.02518  -0.0805   0.9879   0.0078
 -12.250  -0.8227   0.02789   0.02378  -0.0813   0.9861   0.0079
 -12.000  -0.8035   0.02639   0.02215  -0.0823   0.9845   0.0080
 -11.750  -0.7860   0.02505   0.02070  -0.0827   0.9816   0.0080
 -11.500  -0.7677   0.02377   0.01930  -0.0829   0.9781   0.0081
 -11.250  -0.7457   0.02253   0.01793  -0.0836   0.9750   0.0081
 -11.000  -0.7202   0.02154   0.01685  -0.0848   0.9724   0.0082
 -10.750  -0.7042   0.02072   0.01595  -0.0837   0.9661   0.0083
 -10.500  -0.6818   0.01993   0.01508  -0.0838   0.9609   0.0084
 -10.250  -0.6647   0.01903   0.01407  -0.0827   0.9535   0.0085
 -10.000  -0.6446   0.01831   0.01327  -0.0821   0.9445   0.0086
  -9.500  -0.6079   0.01712   0.01188  -0.0796   0.9037   0.0089
  -9.250  -0.5922   0.01663   0.01117  -0.0777   0.8646   0.0090
  -9.000  -0.5780   0.01623   0.01059  -0.0754   0.8349   0.0091
  -8.750  -0.5616   0.01583   0.01005  -0.0736   0.8132   0.0093
  -8.500  -0.5437   0.01541   0.00950  -0.0721   0.7958   0.0095
  -8.250  -0.5249   0.01501   0.00900  -0.0707   0.7816   0.0096
  -8.000  -0.5057   0.01459   0.00849  -0.0694   0.7701   0.0097
  -7.750  -0.4861   0.01421   0.00802  -0.0682   0.7597   0.0098
  -7.500  -0.4653   0.01385   0.00760  -0.0671   0.7505   0.0099
  -7.250  -0.4449   0.01349   0.00716  -0.0660   0.7424   0.0099
  -7.000  -0.4236   0.01314   0.00675  -0.0650   0.7347   0.0101
  -6.750  -0.4052   0.01261   0.00616  -0.0636   0.7278   0.0104
  -6.500  -0.3838   0.01225   0.00576  -0.0626   0.7215   0.0106
  -6.250  -0.3617   0.01195   0.00542  -0.0617   0.7151   0.0109
  -6.000  -0.3389   0.01168   0.00511  -0.0610   0.7095   0.0110
  -5.750  -0.3156   0.01141   0.00482  -0.0603   0.7039   0.0113
  -5.500  -0.2921   0.01118   0.00455  -0.0596   0.6987   0.0116
  -5.250  -0.2683   0.01094   0.00428  -0.0590   0.6945   0.0119
  -5.000  -0.2439   0.01071   0.00402  -0.0585   0.6903   0.0122
  -4.750  -0.2193   0.01051   0.00379  -0.0580   0.6861   0.0125
  -4.500  -0.1946   0.01032   0.00357  -0.0576   0.6822   0.0129
  -4.250  -0.1692   0.01017   0.00339  -0.0572   0.6789   0.0132
  -4.000  -0.1444   0.00992   0.00314  -0.0568   0.6755   0.0141
  -3.750  -0.1189   0.00975   0.00296  -0.0564   0.6719   0.0149
  -3.500  -0.0932   0.00961   0.00279  -0.0561   0.6684   0.0155
  -3.000  -0.0409   0.00935   0.00251  -0.0557   0.6625   0.0178
  -2.750  -0.0146   0.00920   0.00237  -0.0555   0.6598   0.0215
  -2.500   0.0107   0.00897   0.00224  -0.0552   0.6571   0.0427
  -2.250   0.0359   0.00874   0.00212  -0.0548   0.6545   0.0738
  -2.000   0.0588   0.00832   0.00196  -0.0542   0.6519   0.1546
  -1.500   0.0904   0.00628   0.00145  -0.0507   0.6469   0.6158
  -1.250   0.1187   0.00631   0.00149  -0.0508   0.6445   0.6336
  -1.000   0.1471   0.00636   0.00154  -0.0509   0.6423   0.6461
  -0.750   0.1755   0.00644   0.00160  -0.0510   0.6400   0.6548
  -0.500   0.2037   0.00648   0.00163  -0.0511   0.6370   0.6610
  -0.250   0.2315   0.00650   0.00161  -0.0512   0.6309   0.6622
   0.000   0.2595   0.00652   0.00159  -0.0512   0.6223   0.6630
   0.250   0.2871   0.00655   0.00158  -0.0512   0.6142   0.6639
   0.500   0.3146   0.00658   0.00156  -0.0512   0.6044   0.6648
   0.750   0.3424   0.00661   0.00156  -0.0512   0.5956   0.6656
   1.000   0.3697   0.00666   0.00156  -0.0512   0.5866   0.6663
   1.250   0.3979   0.00669   0.00158  -0.0513   0.5799   0.6671
   1.500   0.4253   0.00674   0.00159  -0.0513   0.5715   0.6679
   1.750   0.4529   0.00678   0.00161  -0.0513   0.5612   0.6687
   2.000   0.4800   0.00684   0.00164  -0.0512   0.5495   0.6694
   2.250   0.5057   0.00696   0.00167  -0.0509   0.5270   0.6702
   2.500   0.5280   0.00724   0.00176  -0.0499   0.4815   0.6710
   2.750   0.5478   0.00768   0.00194  -0.0485   0.4238   0.6718
   3.000   0.5672   0.00816   0.00217  -0.0471   0.3688   0.6725
   3.250   0.5874   0.00858   0.00238  -0.0458   0.3214   0.6731
   3.500   0.6095   0.00888   0.00254  -0.0449   0.2905   0.6741
   3.750   0.6321   0.00914   0.00270  -0.0441   0.2655   0.6752
   4.000   0.6547   0.00939   0.00287  -0.0432   0.2443   0.6764
   4.250   0.6773   0.00963   0.00304  -0.0424   0.2246   0.6775
   4.500   0.7000   0.00986   0.00320  -0.0416   0.2087   0.6786
   4.750   0.7229   0.01007   0.00337  -0.0408   0.1963   0.6796
   5.000   0.7453   0.01029   0.00354  -0.0399   0.1835   0.6806
   5.250   0.7674   0.01052   0.00371  -0.0390   0.1721   0.6817
   5.500   0.7902   0.01070   0.00388  -0.0382   0.1640   0.6829
   5.750   0.8118   0.01092   0.00407  -0.0372   0.1557   0.6840
   6.000   0.8332   0.01110   0.00424  -0.0361   0.1489   0.6851
   6.250   0.8524   0.01132   0.00442  -0.0346   0.1410   0.6863
   6.500   0.8726   0.01150   0.00461  -0.0333   0.1355   0.6874
   6.750   0.8918   0.01175   0.00483  -0.0319   0.1295   0.6884
   7.000   0.9119   0.01197   0.00505  -0.0306   0.1246   0.6894
   7.250   0.9311   0.01223   0.00530  -0.0292   0.1188   0.6909
   7.500   0.9499   0.01250   0.00557  -0.0277   0.1137   0.6924
   7.750   0.9700   0.01272   0.00582  -0.0265   0.1108   0.6939
   8.000   0.9889   0.01300   0.00610  -0.0252   0.1059   0.6954
   8.250   1.0068   0.01332   0.00642  -0.0237   0.1009   0.6972
   8.500   1.0263   0.01359   0.00671  -0.0224   0.0983   0.6990
   8.750   1.0450   0.01389   0.00703  -0.0211   0.0945   0.7009
   9.000   1.0625   0.01424   0.00738  -0.0196   0.0909   0.7029
   9.250   1.0802   0.01459   0.00774  -0.0182   0.0870   0.7047
   9.500   1.0981   0.01493   0.00811  -0.0169   0.0837   0.7065
   9.750   1.1149   0.01532   0.00851  -0.0154   0.0803   0.7088
  10.000   1.1307   0.01576   0.00896  -0.0138   0.0760   0.7112
  10.250   1.1475   0.01617   0.00939  -0.0124   0.0725   0.7137
  10.500   1.1641   0.01660   0.00986  -0.0110   0.0702   0.7163
  10.750   1.1780   0.01717   0.01041  -0.0093   0.0651   0.7190
  11.000   1.1940   0.01766   0.01093  -0.0080   0.0622   0.7216
  11.250   1.2095   0.01816   0.01148  -0.0066   0.0601   0.7248
  11.500   1.2230   0.01879   0.01212  -0.0051   0.0568   0.7284
  11.750   1.2374   0.01939   0.01276  -0.0037   0.0537   0.7323
  12.000   1.2514   0.02005   0.01344  -0.0023   0.0507   0.7362
  12.250   1.2642   0.02077   0.01420  -0.0009   0.0479   0.7407
  12.500   1.2772   0.02150   0.01496   0.0005   0.0452   0.7460
  12.750   1.2905   0.02225   0.01575   0.0018   0.0428   0.7518
  13.000   1.3021   0.02310   0.01665   0.0031   0.0402   0.7582
  13.250   1.3133   0.02399   0.01759   0.0044   0.0373   0.7666
  13.500   1.3255   0.02484   0.01850   0.0056   0.0355   0.7759
  13.750   1.3352   0.02585   0.01957   0.0070   0.0327   0.7892
  14.000   1.3451   0.02684   0.02064   0.0083   0.0305   0.8068
  14.250   1.3543   0.02779   0.02173   0.0097   0.0286   0.8371
  14.500   1.3814   0.02898   0.02325   0.0069   0.0257   0.9557
  14.750   1.3941   0.03019   0.02450   0.0072   0.0240   1.0000
  15.000   1.4020   0.03159   0.02592   0.0082   0.0217   1.0000
  15.250   1.4109   0.03295   0.02732   0.0090   0.0204   1.0000
  15.500   1.4176   0.03451   0.02892   0.0098   0.0178   1.0000
  15.750   1.4223   0.03628   0.03071   0.0107   0.0152   1.0000
  16.000   1.4235   0.03840   0.03284   0.0116   0.0116   1.0000
  16.250   1.4263   0.04045   0.03493   0.0123   0.0098   1.0000
  16.750   1.4293   0.04496   0.03955   0.0133   0.0070   1.0000
  17.000   1.4298   0.04741   0.04206   0.0137   0.0062   1.0000
  17.250   1.4325   0.04971   0.04445   0.0138   0.0059   1.0000
  17.500   1.4333   0.05229   0.04710   0.0139   0.0056   1.0000
  17.750   1.4328   0.05507   0.04997   0.0138   0.0052   1.0000
  18.000   1.4336   0.05779   0.05277   0.0136   0.0052   1.0000
  18.250   1.4293   0.06118   0.05625   0.0132   0.0049   1.0000
  18.500   1.4259   0.06460   0.05976   0.0125   0.0047   1.0000
  19.000   1.4143   0.07240   0.06777   0.0106   0.0044   1.0000
  19.250   1.4072   0.07669   0.07217   0.0092   0.0044   1.0000
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