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NASA/LANGLEY NLF(1)-0416 AIRFOIL (nlf416-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: NASA/LANGLEY NLF(1)-0416 AIRFOIL (nlf416-il)
Reynolds number: 1,000,000
Max Cl/Cd: 115.75 at α=6.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-nlf416-il-1000000.txt
Download as CSV file: xf-nlf416-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NASA/LANGLEY NLF(1)-0416 AIRFOIL                
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.000  -0.7474   0.09418   0.09175  -0.0473   1.0000   0.0083
 -15.750  -0.7758   0.08464   0.08204  -0.0529   1.0000   0.0083
 -15.500  -0.8102   0.07464   0.07181  -0.0587   1.0000   0.0082
 -15.250  -0.8031   0.07219   0.06939  -0.0601   1.0000   0.0085
 -15.000  -0.8322   0.06395   0.06092  -0.0646   1.0000   0.0084
 -14.750  -0.8522   0.05782   0.05459  -0.0675   1.0000   0.0083
 -14.500  -0.8621   0.05353   0.05019  -0.0692   1.0000   0.0083
 -14.250  -0.8621   0.05082   0.04743  -0.0702   1.0000   0.0085
 -14.000  -0.8778   0.04651   0.04293  -0.0708   1.0000   0.0083
 -13.750  -0.8792   0.04415   0.04049  -0.0710   1.0000   0.0085
 -13.500  -0.8801   0.04197   0.03826  -0.0707   1.0000   0.0086
 -13.250  -0.8839   0.03961   0.03579  -0.0701   1.0000   0.0087
 -13.000  -0.8888   0.03723   0.03330  -0.0691   1.0000   0.0087
 -12.750  -0.8909   0.03524   0.03121  -0.0679   1.0000   0.0087
 -12.500  -0.8911   0.03358   0.02947  -0.0665   1.0000   0.0088
 -12.250  -0.8933   0.03180   0.02759  -0.0646   1.0000   0.0088
 -12.000  -0.8928   0.03048   0.02620  -0.0627   1.0000   0.0089
 -11.750  -0.8938   0.02916   0.02480  -0.0603   1.0000   0.0090
 -11.500  -0.8976   0.02786   0.02343  -0.0573   1.0000   0.0089
 -11.250  -0.8944   0.02683   0.02233  -0.0554   0.9995   0.0091
 -11.000  -0.8700   0.02545   0.02086  -0.0575   0.9969   0.0092
 -10.750  -0.8425   0.02402   0.01933  -0.0599   0.9945   0.0093
 -10.500  -0.8135   0.02281   0.01804  -0.0622   0.9921   0.0094
 -10.250  -0.7855   0.02155   0.01671  -0.0642   0.9889   0.0095
 -10.000  -0.7538   0.02042   0.01551  -0.0667   0.9864   0.0097
  -9.750  -0.7194   0.01941   0.01443  -0.0695   0.9846   0.0098
  -9.500  -0.6834   0.01855   0.01351  -0.0724   0.9832   0.0099
  -9.250  -0.6633   0.01709   0.01198  -0.0726   0.9767   0.0102
  -9.000  -0.6311   0.01598   0.01082  -0.0749   0.9735   0.0105
  -8.750  -0.5955   0.01519   0.01000  -0.0774   0.9715   0.0108
  -8.500  -0.5736   0.01459   0.00938  -0.0768   0.9628   0.0112
  -8.250  -0.5393   0.01397   0.00874  -0.0787   0.9589   0.0117
  -7.750  -0.4814   0.01285   0.00756  -0.0800   0.9373   0.0125
  -7.500  -0.4324   0.01200   0.00664  -0.0851   0.9283   0.0132
  -7.250  -0.3737   0.01136   0.00595  -0.0921   0.9118   0.0143
  -7.000  -0.3298   0.01100   0.00543  -0.0957   0.8743   0.0152
  -6.750  -0.3036   0.01080   0.00502  -0.0956   0.8304   0.0163
  -6.500  -0.2805   0.01062   0.00470  -0.0948   0.7920   0.0181
  -6.250  -0.2571   0.01044   0.00438  -0.0941   0.7581   0.0210
  -6.000  -0.2333   0.01017   0.00404  -0.0937   0.7282   0.0304
  -5.750  -0.2087   0.00974   0.00367  -0.0935   0.7016   0.0603
  -5.250  -0.1564   0.00910   0.00315  -0.0937   0.6585   0.1242
  -5.000  -0.1290   0.00882   0.00293  -0.0940   0.6407   0.1591
  -4.750  -0.1011   0.00852   0.00273  -0.0944   0.6245   0.1993
  -4.250  -0.0437   0.00793   0.00236  -0.0956   0.5965   0.2930
  -4.000  -0.0143   0.00758   0.00218  -0.0963   0.5845   0.3550
  -3.750   0.0156   0.00718   0.00199  -0.0972   0.5736   0.4302
  -3.500   0.0458   0.00687   0.00184  -0.0980   0.5641   0.4954
  -3.250   0.0754   0.00669   0.00179  -0.0986   0.5555   0.5476
  -3.000   0.1048   0.00668   0.00183  -0.0988   0.5473   0.5856
  -2.750   0.1338   0.00678   0.00190  -0.0989   0.5398   0.6051
  -2.500   0.1632   0.00686   0.00193  -0.0991   0.5334   0.6173
  -2.250   0.1920   0.00698   0.00201  -0.0992   0.5268   0.6254
  -2.000   0.2214   0.00709   0.00203  -0.0994   0.5211   0.6323
  -1.750   0.2503   0.00718   0.00211  -0.0995   0.5157   0.6373
  -1.500   0.2791   0.00730   0.00219  -0.0995   0.5102   0.6423
  -1.250   0.3082   0.00743   0.00225  -0.0997   0.5053   0.6470
  -1.000   0.3374   0.00749   0.00229  -0.0998   0.5008   0.6508
  -0.750   0.3660   0.00759   0.00238  -0.0998   0.4961   0.6541
  -0.500   0.3944   0.00772   0.00246  -0.0998   0.4911   0.6573
  -0.250   0.4235   0.00780   0.00253  -0.1000   0.4874   0.6604
   0.000   0.4528   0.00789   0.00258  -0.1002   0.4833   0.6634
   0.250   0.4817   0.00795   0.00261  -0.1003   0.4791   0.6660
   0.500   0.5098   0.00805   0.00268  -0.1003   0.4744   0.6685
   0.750   0.5385   0.00812   0.00276  -0.1004   0.4708   0.6706
   1.000   0.5674   0.00818   0.00282  -0.1005   0.4670   0.6728
   1.250   0.5961   0.00826   0.00289  -0.1006   0.4629   0.6751
   1.500   0.6244   0.00837   0.00296  -0.1007   0.4584   0.6773
   1.750   0.6532   0.00847   0.00304  -0.1008   0.4546   0.6794
   2.000   0.6823   0.00854   0.00310  -0.1010   0.4509   0.6810
   2.250   0.7110   0.00854   0.00311  -0.1012   0.4467   0.6830
   2.500   0.7391   0.00861   0.00316  -0.1012   0.4423   0.6845
   2.750   0.7673   0.00868   0.00324  -0.1013   0.4381   0.6858
   3.000   0.7961   0.00872   0.00330  -0.1014   0.4341   0.6872
   3.250   0.8244   0.00879   0.00337  -0.1015   0.4293   0.6885
   3.500   0.8521   0.00891   0.00345  -0.1015   0.4239   0.6900
   3.750   0.8808   0.00896   0.00353  -0.1016   0.4194   0.6916
   4.000   0.9091   0.00903   0.00360  -0.1017   0.4140   0.6930
   4.250   0.9369   0.00914   0.00369  -0.1017   0.4082   0.6944
   4.500   0.9653   0.00921   0.00377  -0.1018   0.4028   0.6955
   4.750   0.9934   0.00929   0.00385  -0.1019   0.3964   0.6964
   5.000   1.0209   0.00941   0.00394  -0.1019   0.3895   0.6971
   5.250   1.0490   0.00949   0.00403  -0.1020   0.3821   0.6976
   5.500   1.0762   0.00960   0.00412  -0.1020   0.3736   0.6986
   5.750   1.1037   0.00968   0.00420  -0.1020   0.3639   0.6998
   6.000   1.1305   0.00982   0.00432  -0.1019   0.3533   0.7007
   6.250   1.1568   0.01000   0.00447  -0.1017   0.3410   0.7015
   6.500   1.1826   0.01022   0.00464  -0.1014   0.3278   0.7023
   6.750   1.2084   0.01044   0.00483  -0.1011   0.3147   0.7031
   7.000   1.2338   0.01068   0.00504  -0.1008   0.3011   0.7039
   7.250   1.2588   0.01095   0.00527  -0.1004   0.2875   0.7047
   7.500   1.2835   0.01124   0.00551  -0.1000   0.2743   0.7055
   7.750   1.3077   0.01155   0.00578  -0.0995   0.2612   0.7065
   8.000   1.3315   0.01188   0.00607  -0.0989   0.2481   0.7075
   8.250   1.3549   0.01224   0.00638  -0.0983   0.2348   0.7086
   8.500   1.3781   0.01259   0.00668  -0.0976   0.2219   0.7095
   8.750   1.4012   0.01293   0.00699  -0.0970   0.2102   0.7103
   9.000   1.4237   0.01329   0.00733  -0.0962   0.1989   0.7112
   9.250   1.4453   0.01370   0.00770  -0.0953   0.1875   0.7120
   9.750   1.4871   0.01455   0.00847  -0.0933   0.1656   0.7135
  10.000   1.5065   0.01501   0.00890  -0.0921   0.1541   0.7141
  10.250   1.5246   0.01551   0.00935  -0.0907   0.1426   0.7152
  10.500   1.5408   0.01604   0.00984  -0.0890   0.1317   0.7164
  10.750   1.5547   0.01653   0.01031  -0.0868   0.1226   0.7175
  11.000   1.5688   0.01702   0.01080  -0.0847   0.1149   0.7186
  11.250   1.5807   0.01764   0.01141  -0.0823   0.1069   0.7197
  11.500   1.5939   0.01821   0.01198  -0.0801   0.1002   0.7208
  11.750   1.6048   0.01889   0.01266  -0.0778   0.0935   0.7220
  12.000   1.6157   0.01958   0.01336  -0.0755   0.0875   0.7233
  12.250   1.6249   0.02038   0.01417  -0.0731   0.0818   0.7247
  12.500   1.6332   0.02126   0.01505  -0.0707   0.0763   0.7260
  12.750   1.6401   0.02225   0.01606  -0.0683   0.0713   0.7272
  13.000   1.6466   0.02332   0.01715  -0.0661   0.0667   0.7284
  13.250   1.6505   0.02462   0.01846  -0.0638   0.0623   0.7294
  13.500   1.6566   0.02588   0.01976  -0.0620   0.0589   0.7304
  13.750   1.6583   0.02753   0.02144  -0.0601   0.0551   0.7319
  14.000   1.6621   0.02916   0.02314  -0.0586   0.0520   0.7335
  14.250   1.6637   0.03110   0.02513  -0.0573   0.0488   0.7350
  14.500   1.6625   0.03344   0.02751  -0.0561   0.0456   0.7365
  14.750   1.6646   0.03563   0.02977  -0.0554   0.0430   0.7380
  15.000   1.6622   0.03838   0.03258  -0.0548   0.0403   0.7395
  15.250   1.6604   0.04123   0.03549  -0.0545   0.0378   0.7410
  15.500   1.6588   0.04417   0.03849  -0.0544   0.0356   0.7425
  15.750   1.6530   0.04770   0.04208  -0.0545   0.0333   0.7439
  16.000   1.6500   0.05101   0.04546  -0.0547   0.0314   0.7453
  16.250   1.6449   0.05465   0.04917  -0.0551   0.0294   0.7465
  16.500   1.6366   0.05882   0.05340  -0.0558   0.0275   0.7482
  16.750   1.6325   0.06257   0.05724  -0.0566   0.0259   0.7500
  17.000   1.6254   0.06679   0.06155  -0.0575   0.0242   0.7517
  17.250   1.6165   0.07140   0.06623  -0.0587   0.0225   0.7533
  17.500   1.6110   0.07565   0.07057  -0.0599   0.0212   0.7552
  17.750   1.6025   0.08042   0.07542  -0.0614   0.0199   0.7569
  18.000   1.5930   0.08547   0.08055  -0.0631   0.0187   0.7587
  18.250   1.5871   0.09009   0.08526  -0.0647   0.0177   0.7606
  18.500   1.5791   0.09509   0.09034  -0.0666   0.0167   0.7623
  18.750   1.5691   0.10052   0.09585  -0.0687   0.0159   0.7642
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