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NASA/LANGLEY NLF(1)-0416 AIRFOIL (nlf416-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: NASA/LANGLEY NLF(1)-0416 AIRFOIL (nlf416-il)
Reynolds number: 100,000
Max Cl/Cd: 48.29 at α=9°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-nlf416-il-100000-n5.txt
Download as CSV file: xf-nlf416-il-100000-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 =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.750  -0.5542   0.08497   0.07921  -0.0583   1.0000   0.0230
 -12.500  -0.5774   0.07766   0.07179  -0.0627   1.0000   0.0229
 -12.250  -0.6002   0.07139   0.06537  -0.0661   1.0000   0.0228
 -12.000  -0.6200   0.06628   0.06012  -0.0683   1.0000   0.0227
 -11.750  -0.6379   0.06196   0.05564  -0.0694   1.0000   0.0226
 -11.500  -0.6553   0.05811   0.05162  -0.0697   1.0000   0.0226
 -11.250  -0.6714   0.05472   0.04805  -0.0691   1.0000   0.0226
 -11.000  -0.6855   0.05182   0.04497  -0.0679   1.0000   0.0227
 -10.750  -0.6991   0.04927   0.04224  -0.0660   1.0000   0.0228
 -10.500  -0.7122   0.04712   0.03991  -0.0633   1.0000   0.0229
 -10.250  -0.7241   0.04518   0.03779  -0.0603   1.0000   0.0230
 -10.000  -0.7247   0.04340   0.03596  -0.0584   1.0000   0.0235
  -9.750  -0.7224   0.04180   0.03431  -0.0565   1.0000   0.0239
  -9.500  -0.7185   0.04027   0.03268  -0.0545   1.0000   0.0244
  -9.250  -0.7132   0.03885   0.03116  -0.0526   1.0000   0.0254
  -9.000  -0.7062   0.03726   0.02940  -0.0507   1.0000   0.0260
  -8.750  -0.6971   0.03573   0.02768  -0.0488   1.0000   0.0266
  -8.500  -0.6866   0.03427   0.02603  -0.0468   1.0000   0.0272
  -8.250  -0.6640   0.03269   0.02436  -0.0469   0.9974   0.0279
  -8.000  -0.6295   0.03118   0.02281  -0.0493   0.9911   0.0289
  -7.750  -0.5947   0.02977   0.02133  -0.0517   0.9841   0.0303
  -7.500  -0.5628   0.02842   0.01987  -0.0534   0.9752   0.0322
  -7.250  -0.5321   0.02713   0.01857  -0.0552   0.9649   0.0347
  -7.000  -0.5010   0.02599   0.01735  -0.0568   0.9538   0.0383
  -6.750  -0.4705   0.02473   0.01610  -0.0585   0.9421   0.0424
  -6.500  -0.4382   0.02348   0.01481  -0.0604   0.9308   0.0485
  -6.250  -0.4083   0.02231   0.01367  -0.0617   0.9171   0.0600
  -6.000  -0.3776   0.02107   0.01260  -0.0631   0.9032   0.0851
  -5.750  -0.3451   0.01981   0.01169  -0.0652   0.8892   0.1368
  -5.500  -0.3096   0.01866   0.01090  -0.0678   0.8753   0.2085
  -5.250  -0.2728   0.01755   0.01020  -0.0706   0.8601   0.2947
  -5.000  -0.2359   0.01665   0.00968  -0.0731   0.8434   0.3839
  -4.750  -0.2002   0.01628   0.00954  -0.0744   0.8251   0.4556
  -4.500  -0.1673   0.01650   0.00989  -0.0740   0.8060   0.5076
  -4.250  -0.1356   0.01706   0.01042  -0.0732   0.7868   0.5421
  -4.000  -0.1023   0.01747   0.01064  -0.0733   0.7676   0.5704
  -3.750  -0.0703   0.01787   0.01081  -0.0734   0.7491   0.5911
  -3.500  -0.0389   0.01818   0.01088  -0.0737   0.7317   0.6093
  -3.250  -0.0090   0.01849   0.01098  -0.0737   0.7157   0.6237
  -3.000   0.0202   0.01877   0.01106  -0.0736   0.7014   0.6367
  -2.750   0.0497   0.01897   0.01104  -0.0739   0.6884   0.6496
  -2.500   0.0761   0.01933   0.01125  -0.0728   0.6768   0.6567
  -2.250   0.1041   0.01945   0.01121  -0.0728   0.6650   0.6671
  -2.000   0.1297   0.01971   0.01134  -0.0718   0.6549   0.6739
  -1.750   0.1582   0.01979   0.01126  -0.0720   0.6458   0.6833
  -1.500   0.1829   0.01999   0.01137  -0.0709   0.6368   0.6889
  -1.250   0.2125   0.02001   0.01122  -0.0716   0.6285   0.6983
  -1.000   0.2365   0.02017   0.01132  -0.0703   0.6205   0.7025
  -0.750   0.2627   0.02027   0.01132  -0.0699   0.6130   0.7086
  -0.500   0.2915   0.02029   0.01122  -0.0704   0.6062   0.7156
  -0.250   0.3157   0.02039   0.01128  -0.0694   0.5989   0.7197
   0.000   0.3429   0.02046   0.01124  -0.0693   0.5929   0.7252
   0.250   0.3716   0.02047   0.01119  -0.0699   0.5859   0.7314
   0.500   0.3962   0.02055   0.01123  -0.0691   0.5797   0.7348
   0.750   0.4230   0.02062   0.01121  -0.0688   0.5743   0.7389
   1.000   0.4508   0.02066   0.01124  -0.0692   0.5676   0.7438
   1.250   0.4793   0.02071   0.01123  -0.0697   0.5617   0.7479
   1.500   0.5051   0.02078   0.01125  -0.0692   0.5566   0.7508
   1.750   0.5305   0.02085   0.01136  -0.0689   0.5502   0.7541
   2.000   0.5585   0.02092   0.01139  -0.0692   0.5445   0.7577
   2.250   0.5888   0.02102   0.01142  -0.0701   0.5393   0.7616
   2.500   0.6146   0.02110   0.01155  -0.0699   0.5329   0.7643
   2.750   0.6405   0.02119   0.01163  -0.0696   0.5274   0.7669
   3.000   0.6676   0.02129   0.01172  -0.0696   0.5222   0.7694
   3.250   0.6936   0.02141   0.01190  -0.0696   0.5156   0.7723
   3.500   0.7224   0.02153   0.01199  -0.0701   0.5099   0.7752
   3.750   0.7517   0.02167   0.01214  -0.0708   0.5042   0.7779
   4.000   0.7772   0.02180   0.01235  -0.0706   0.4974   0.7800
   4.250   0.8038   0.02190   0.01244  -0.0705   0.4918   0.7820
   4.500   0.8291   0.02206   0.01268  -0.0703   0.4854   0.7840
   4.750   0.8551   0.02220   0.01289  -0.0702   0.4786   0.7862
   5.250   0.9081   0.02253   0.01334  -0.0703   0.4652   0.7905
   5.500   0.9362   0.02267   0.01348  -0.0707   0.4585   0.7923
   5.750   0.9628   0.02288   0.01378  -0.0709   0.4511   0.7944
   6.000   0.9871   0.02302   0.01401  -0.0704   0.4436   0.7962
   6.250   1.0115   0.02318   0.01423  -0.0700   0.4364   0.7979
   6.500   1.0353   0.02336   0.01453  -0.0696   0.4279   0.7996
   6.750   1.0602   0.02353   0.01476  -0.0693   0.4201   0.8012
   7.000   1.0837   0.02373   0.01507  -0.0689   0.4108   0.8029
   7.250   1.1075   0.02394   0.01538  -0.0685   0.4020   0.8049
   7.500   1.1314   0.02413   0.01565  -0.0681   0.3927   0.8071
   7.750   1.1543   0.02443   0.01608  -0.0677   0.3823   0.8093
   8.000   1.1769   0.02465   0.01635  -0.0671   0.3727   0.8111
   8.250   1.1969   0.02492   0.01675  -0.0661   0.3617   0.8127
   8.500   1.2164   0.02526   0.01719  -0.0651   0.3504   0.8144
   8.750   1.2357   0.02560   0.01758  -0.0640   0.3394   0.8163
   9.000   1.2541   0.02597   0.01798  -0.0628   0.3282   0.8183
   9.250   1.2708   0.02648   0.01859  -0.0616   0.3158   0.8205
   9.500   1.2865   0.02704   0.01921  -0.0602   0.3038   0.8229
   9.750   1.3000   0.02766   0.01986  -0.0585   0.2924   0.8256
  10.000   1.3101   0.02831   0.02052  -0.0562   0.2816   0.8280
  10.250   1.3197   0.02911   0.02143  -0.0541   0.2702   0.8306
  10.500   1.3289   0.03001   0.02240  -0.0521   0.2595   0.8332
  10.750   1.3368   0.03103   0.02343  -0.0502   0.2496   0.8359
  11.000   1.3438   0.03221   0.02470  -0.0485   0.2390   0.8388
  11.500   1.3530   0.03495   0.02753  -0.0450   0.2206   0.8444
  11.750   1.3562   0.03655   0.02929  -0.0435   0.2114   0.8476
  12.000   1.3581   0.03835   0.03112  -0.0422   0.2034   0.8511
  12.250   1.3597   0.04036   0.03326  -0.0413   0.1949   0.8550
  12.500   1.3599   0.04251   0.03547  -0.0404   0.1874   0.8590
  12.750   1.3592   0.04487   0.03795  -0.0397   0.1797   0.8635
  13.000   1.3586   0.04737   0.04052  -0.0393   0.1728   0.8686
  13.250   1.3569   0.05011   0.04340  -0.0392   0.1656   0.8738
  13.500   1.3548   0.05289   0.04625  -0.0390   0.1594   0.8796
  13.750   1.3524   0.05592   0.04944  -0.0392   0.1526   0.8865
  14.250   1.3450   0.06209   0.05585  -0.0395   0.1409   0.9092
  14.500   1.3375   0.06524   0.05911  -0.0396   0.1358   1.0000
  14.750   1.3362   0.06884   0.06278  -0.0407   0.1303   1.0000
  15.000   1.3335   0.07275   0.06681  -0.0421   0.1246   1.0000
  15.250   1.3317   0.07644   0.07046  -0.0434   0.1197   1.0000
  15.500   1.3281   0.08072   0.07495  -0.0451   0.1143   1.0000
  15.750   1.3244   0.08494   0.07923  -0.0468   0.1095   1.0000
  16.000   1.3215   0.08911   0.08347  -0.0484   0.1050   1.0000
  16.250   1.3163   0.09382   0.08833  -0.0505   0.1003   1.0000
  16.500   1.3130   0.09817   0.09270  -0.0524   0.0962   1.0000
  16.750   1.3084   0.10289   0.09754  -0.0546   0.0920   1.0000
  17.000   1.3022   0.10797   0.10276  -0.0570   0.0879   1.0000
  17.250   1.2993   0.11239   0.10718  -0.0592   0.0843   1.0000
  17.500   1.2933   0.11760   0.11252  -0.0618   0.0807   1.0000
  17.750   1.2863   0.12309   0.11815  -0.0648   0.0770   1.0000
  18.000   1.2833   0.12771   0.12278  -0.0674   0.0737   1.0000
  18.250   1.2776   0.13300   0.12818  -0.0704   0.0706   1.0000
  18.500   1.2686   0.13910   0.13444  -0.0740   0.0674   1.0000
  18.750   1.2650   0.14407   0.13945  -0.0771   0.0644   1.0000
  19.000   1.2630   0.14870   0.14409  -0.0800   0.0617   1.0000
  19.250   1.2507   0.15582   0.15142  -0.0845   0.0591   1.0000
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