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NASA/LANGLEY NLF(1)-0416 AIRFOIL (nlf416-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: NASA/LANGLEY NLF(1)-0416 AIRFOIL (nlf416-il)
Reynolds number: 1,000,000
Max Cl/Cd: 108.37 at α=5.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-nlf416-il-1000000-n5.txt
Download as CSV file: xf-nlf416-il-1000000-n5.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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -18.500  -0.7425   0.13733   0.13491  -0.0255   1.0000   0.0054
 -18.250  -0.7673   0.12784   0.12530  -0.0302   1.0000   0.0054
 -18.000  -0.7966   0.11786   0.11521  -0.0352   1.0000   0.0055
 -17.750  -0.8168   0.10992   0.10716  -0.0391   1.0000   0.0055
 -17.500  -0.8366   0.10226   0.09939  -0.0430   1.0000   0.0055
 -17.250  -0.8570   0.09467   0.09169  -0.0468   1.0000   0.0054
 -17.000  -0.8742   0.08782   0.08473  -0.0503   1.0000   0.0054
 -16.750  -0.8924   0.08094   0.07774  -0.0539   1.0000   0.0054
 -16.500  -0.9087   0.07457   0.07125  -0.0572   1.0000   0.0054
 -16.250  -0.9240   0.06855   0.06511  -0.0603   1.0000   0.0054
 -16.000  -0.9330   0.06367   0.06012  -0.0627   1.0000   0.0054
 -15.750  -0.9447   0.05863   0.05496  -0.0651   1.0000   0.0054
 -15.500  -0.9558   0.05393   0.05014  -0.0671   1.0000   0.0054
 -15.250  -0.9695   0.04922   0.04530  -0.0688   1.0000   0.0056
 -15.000  -0.9740   0.04592   0.04191  -0.0696   1.0000   0.0055
 -14.750  -0.9761   0.04315   0.03904  -0.0700   1.0000   0.0055
 -14.500  -0.9837   0.04008   0.03588  -0.0701   1.0000   0.0056
 -14.250  -0.9844   0.03787   0.03360  -0.0697   1.0000   0.0057
 -14.000  -0.9867   0.03568   0.03132  -0.0690   1.0000   0.0056
 -13.750  -0.9859   0.03387   0.02945  -0.0681   1.0000   0.0057
 -13.500  -0.9854   0.03215   0.02767  -0.0670   1.0000   0.0058
 -13.250  -0.9833   0.03065   0.02610  -0.0656   1.0000   0.0058
 -13.000  -0.9826   0.02915   0.02454  -0.0640   1.0000   0.0058
 -12.750  -0.9685   0.02771   0.02304  -0.0647   0.9992   0.0059
 -12.500  -0.9434   0.02629   0.02155  -0.0672   0.9972   0.0060
 -12.250  -0.9187   0.02491   0.02011  -0.0695   0.9950   0.0061
 -12.000  -0.8952   0.02379   0.01893  -0.0712   0.9930   0.0062
 -11.750  -0.8779   0.02272   0.01781  -0.0715   0.9903   0.0062
 -11.500  -0.8583   0.02166   0.01670  -0.0722   0.9873   0.0063
 -11.250  -0.8344   0.02075   0.01574  -0.0735   0.9847   0.0064
 -11.000  -0.8162   0.01982   0.01476  -0.0736   0.9807   0.0065
 -10.750  -0.7964   0.01886   0.01376  -0.0739   0.9750   0.0066
 -10.500  -0.7699   0.01801   0.01285  -0.0753   0.9707   0.0068
 -10.000  -0.7310   0.01655   0.01130  -0.0746   0.9524   0.0070
  -9.750  -0.6997   0.01586   0.01057  -0.0763   0.9438   0.0072
  -9.500  -0.6567   0.01520   0.00986  -0.0801   0.9336   0.0074
  -9.250  -0.5877   0.01429   0.00886  -0.0895   0.9189   0.0078
  -9.000  -0.5352   0.01363   0.00804  -0.0954   0.8784   0.0082
  -8.750  -0.5123   0.01339   0.00757  -0.0950   0.8295   0.0083
  -8.500  -0.4925   0.01317   0.00718  -0.0939   0.7903   0.0086
  -8.250  -0.4717   0.01295   0.00681  -0.0929   0.7564   0.0089
  -8.000  -0.4498   0.01274   0.00646  -0.0921   0.7263   0.0091
  -7.750  -0.4266   0.01253   0.00612  -0.0916   0.6994   0.0094
  -7.500  -0.4026   0.01233   0.00581  -0.0912   0.6769   0.0098
  -7.250  -0.3777   0.01209   0.00548  -0.0909   0.6574   0.0102
  -7.000  -0.3524   0.01185   0.00517  -0.0907   0.6405   0.0108
  -6.750  -0.3264   0.01164   0.00489  -0.0906   0.6251   0.0115
  -6.500  -0.2999   0.01146   0.00464  -0.0906   0.6109   0.0124
  -6.250  -0.2731   0.01125   0.00439  -0.0906   0.5980   0.0139
  -6.000  -0.2461   0.01105   0.00415  -0.0907   0.5861   0.0165
  -5.750  -0.2191   0.01084   0.00392  -0.0908   0.5743   0.0214
  -5.500  -0.1915   0.01061   0.00368  -0.0910   0.5638   0.0294
  -5.250  -0.1638   0.01035   0.00345  -0.0912   0.5551   0.0428
  -5.000  -0.1358   0.01008   0.00323  -0.0916   0.5468   0.0604
  -4.750  -0.1076   0.00984   0.00304  -0.0919   0.5395   0.0800
  -4.500  -0.0789   0.00959   0.00285  -0.0924   0.5327   0.1030
  -4.250  -0.0502   0.00931   0.00267  -0.0929   0.5256   0.1351
  -4.000  -0.0210   0.00897   0.00248  -0.0936   0.5194   0.1793
  -3.750   0.0086   0.00857   0.00229  -0.0944   0.5132   0.2402
  -3.250   0.0684   0.00799   0.00200  -0.0959   0.5030   0.3410
  -3.000   0.0983   0.00779   0.00189  -0.0965   0.4977   0.3770
  -2.750   0.1283   0.00760   0.00179  -0.0972   0.4925   0.4199
  -2.500   0.1584   0.00742   0.00170  -0.0978   0.4882   0.4601
  -2.250   0.1886   0.00725   0.00163  -0.0984   0.4839   0.4988
  -2.000   0.2185   0.00712   0.00160  -0.0990   0.4792   0.5381
  -1.750   0.2480   0.00709   0.00164  -0.0993   0.4748   0.5752
  -1.500   0.2774   0.00713   0.00169  -0.0996   0.4710   0.5953
  -1.250   0.3068   0.00717   0.00173  -0.0998   0.4672   0.6067
  -1.000   0.3360   0.00724   0.00175  -0.1000   0.4629   0.6155
  -0.750   0.3649   0.00731   0.00180  -0.1001   0.4587   0.6210
  -0.500   0.3940   0.00738   0.00184  -0.1003   0.4550   0.6262
  -0.250   0.4233   0.00744   0.00186  -0.1005   0.4515   0.6305
   0.000   0.4524   0.00750   0.00190  -0.1007   0.4475   0.6340
   0.250   0.4812   0.00757   0.00196  -0.1008   0.4435   0.6373
   0.500   0.5099   0.00767   0.00202  -0.1009   0.4393   0.6405
   0.750   0.5391   0.00772   0.00207  -0.1011   0.4360   0.6433
   1.000   0.5681   0.00779   0.00211  -0.1013   0.4317   0.6459
   1.250   0.5970   0.00788   0.00216  -0.1014   0.4273   0.6480
   1.500   0.6254   0.00796   0.00222  -0.1015   0.4229   0.6503
   1.750   0.6542   0.00801   0.00229  -0.1017   0.4191   0.6524
   2.000   0.6829   0.00808   0.00236  -0.1018   0.4146   0.6545
   2.250   0.7113   0.00818   0.00243  -0.1019   0.4096   0.6562
   2.500   0.7398   0.00826   0.00250  -0.1020   0.4052   0.6578
   2.750   0.7685   0.00833   0.00257  -0.1021   0.4002   0.6593
   3.000   0.7968   0.00843   0.00265  -0.1022   0.3942   0.6609
   3.250   0.8250   0.00854   0.00273  -0.1022   0.3884   0.6627
   3.500   0.8533   0.00864   0.00282  -0.1023   0.3814   0.6642
   3.750   0.8810   0.00876   0.00291  -0.1023   0.3735   0.6653
   4.000   0.9090   0.00885   0.00299  -0.1024   0.3652   0.6663
   4.250   0.9365   0.00898   0.00310  -0.1023   0.3565   0.6673
   4.500   0.9638   0.00913   0.00322  -0.1023   0.3457   0.6682
   4.750   0.9911   0.00928   0.00334  -0.1022   0.3353   0.6690
   5.000   1.0178   0.00947   0.00349  -0.1021   0.3235   0.6697
   5.250   1.0442   0.00968   0.00366  -0.1019   0.3114   0.6704
   5.500   1.0706   0.00990   0.00383  -0.1017   0.2990   0.6711
   5.750   1.0967   0.01012   0.00402  -0.1015   0.2864   0.6719
   6.000   1.1226   0.01037   0.00423  -0.1012   0.2740   0.6726
   6.250   1.1480   0.01064   0.00445  -0.1009   0.2611   0.6735
   6.500   1.1732   0.01093   0.00468  -0.1005   0.2487   0.6744
   6.750   1.1983   0.01121   0.00493  -0.1001   0.2369   0.6754
   7.000   1.2233   0.01148   0.00517  -0.0997   0.2252   0.6762
   7.250   1.2479   0.01179   0.00543  -0.0993   0.2136   0.6769
   7.500   1.2720   0.01211   0.00572  -0.0988   0.2025   0.6776
   7.750   1.2958   0.01245   0.00601  -0.0982   0.1916   0.6783
   8.000   1.3198   0.01276   0.00630  -0.0976   0.1815   0.6790
   8.250   1.3429   0.01311   0.00662  -0.0970   0.1714   0.6797
   8.500   1.3651   0.01351   0.00697  -0.0962   0.1604   0.6803
   8.750   1.3876   0.01388   0.00731  -0.0954   0.1509   0.6809
   9.000   1.4095   0.01425   0.00767  -0.0945   0.1422   0.6815
   9.250   1.4301   0.01469   0.00807  -0.0935   0.1329   0.6825
   9.500   1.4512   0.01506   0.00845  -0.0925   0.1253   0.6834
   9.750   1.4707   0.01550   0.00887  -0.0913   0.1173   0.6843
  10.000   1.4882   0.01603   0.00936  -0.0898   0.1077   0.6852
  10.250   1.5040   0.01653   0.00984  -0.0879   0.0986   0.6861
  10.500   1.5169   0.01707   0.01036  -0.0856   0.0897   0.6871
  10.750   1.5289   0.01768   0.01095  -0.0832   0.0819   0.6882
  11.000   1.5412   0.01829   0.01155  -0.0808   0.0753   0.6893
  11.250   1.5540   0.01889   0.01215  -0.0787   0.0704   0.6904
  11.500   1.5646   0.01960   0.01287  -0.0763   0.0648   0.6914
  11.750   1.5756   0.02031   0.01359  -0.0741   0.0607   0.6923
  12.000   1.5853   0.02110   0.01441  -0.0718   0.0564   0.6933
  12.250   1.5937   0.02200   0.01532  -0.0696   0.0527   0.6943
  12.500   1.6021   0.02295   0.01630  -0.0674   0.0492   0.6952
  12.750   1.6070   0.02415   0.01751  -0.0651   0.0456   0.6961
  13.000   1.6137   0.02533   0.01874  -0.0632   0.0424   0.6969
  13.250   1.6171   0.02682   0.02025  -0.0613   0.0394   0.6977
  13.500   1.6217   0.02834   0.02182  -0.0597   0.0369   0.6988
  13.750   1.6249   0.03007   0.02361  -0.0583   0.0345   0.7000
  14.000   1.6263   0.03210   0.02570  -0.0571   0.0323   0.7011
  14.250   1.6290   0.03417   0.02783  -0.0562   0.0303   0.7023
  14.500   1.6289   0.03661   0.03033  -0.0555   0.0282   0.7034
  14.750   1.6288   0.03920   0.03298  -0.0550   0.0263   0.7046
  15.000   1.6283   0.04196   0.03582  -0.0548   0.0246   0.7057
  15.250   1.6246   0.04516   0.03907  -0.0547   0.0227   0.7069
  15.500   1.6236   0.04818   0.04218  -0.0548   0.0214   0.7080
  15.750   1.6198   0.05161   0.04567  -0.0551   0.0198   0.7091
  16.000   1.6151   0.05524   0.04938  -0.0556   0.0187   0.7102
  16.250   1.6120   0.05879   0.05300  -0.0561   0.0176   0.7112
  16.500   1.6070   0.06266   0.05694  -0.0569   0.0165   0.7123
  17.000   1.5965   0.07077   0.06521  -0.0588   0.0146   0.7142
  17.250   1.5911   0.07501   0.06954  -0.0600   0.0137   0.7156
  17.500   1.5847   0.07947   0.07409  -0.0614   0.0130   0.7169
  17.750   1.5789   0.08395   0.07866  -0.0628   0.0123   0.7181
  18.000   1.5743   0.08832   0.08312  -0.0643   0.0118   0.7195
  18.250   1.5685   0.09299   0.08788  -0.0660   0.0112   0.7207
  18.500   1.5616   0.09788   0.09286  -0.0679   0.0107   0.7220
  18.750   1.5544   0.10290   0.09797  -0.0700   0.0103   0.7232
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