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NACA 5-H-15 AIRFOIL (n5h15-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: NACA 5-H-15 AIRFOIL (n5h15-il)
Reynolds number: 100,000
Max Cl/Cd: 43.08 at α=8°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-n5h15-il-100000-n5.txt
Download as CSV file: xf-n5h15-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 5-H-15 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
  ------ -------- --------- --------- -------- -------- --------
 -12.250  -0.4099   0.12456   0.11947  -0.0328   0.8088   0.0692
 -12.000  -0.3981   0.12093   0.11581  -0.0332   0.8054   0.0700
 -11.750  -0.3923   0.11717   0.11204  -0.0346   0.8023   0.0706
 -11.500  -0.4195   0.10664   0.10152  -0.0433   0.8003   0.0556
 -11.250  -0.4116   0.10308   0.09793  -0.0434   0.7976   0.0551
 -11.000  -0.4089   0.09898   0.09381  -0.0447   0.7947   0.0546
 -10.750  -0.4064   0.09491   0.08975  -0.0462   0.7912   0.0536
 -10.500  -0.4104   0.08992   0.08476  -0.0489   0.7880   0.0527
 -10.250  -0.4231   0.08354   0.07839  -0.0533   0.7851   0.0516
 -10.000  -0.4442   0.07732   0.07210  -0.0566   0.7824   0.0506
  -9.750  -0.4673   0.07216   0.06684  -0.0577   0.7794   0.0498
  -9.500  -0.4897   0.06781   0.06237  -0.0569   0.7757   0.0493
  -9.250  -0.5114   0.06419   0.05857  -0.0542   0.7721   0.0487
  -9.000  -0.5273   0.06122   0.05540  -0.0509   0.7690   0.0486
  -8.750  -0.5354   0.05838   0.05232  -0.0480   0.7664   0.0489
  -8.500  -0.5376   0.05571   0.04942  -0.0458   0.7628   0.0496
  -8.250  -0.5378   0.05302   0.04648  -0.0434   0.7591   0.0502
  -8.000  -0.5361   0.05034   0.04348  -0.0407   0.7560   0.0505
  -7.750  -0.5320   0.04768   0.04048  -0.0381   0.7534   0.0504
  -7.500  -0.5249   0.04523   0.03767  -0.0355   0.7512   0.0504
  -7.250  -0.5137   0.04297   0.03508  -0.0336   0.7481   0.0505
  -7.000  -0.5001   0.04090   0.03266  -0.0320   0.7445   0.0507
  -6.750  -0.4849   0.03911   0.03053  -0.0303   0.7412   0.0513
  -6.500  -0.4681   0.03757   0.02864  -0.0287   0.7385   0.0525
  -6.250  -0.4497   0.03612   0.02683  -0.0271   0.7363   0.0534
  -6.000  -0.4284   0.03467   0.02508  -0.0262   0.7336   0.0538
  -5.750  -0.4048   0.03333   0.02347  -0.0259   0.7295   0.0541
  -5.500  -0.3806   0.03209   0.02197  -0.0254   0.7258   0.0544
  -5.250  -0.3555   0.03093   0.02056  -0.0248   0.7226   0.0549
  -5.000  -0.3297   0.02986   0.01923  -0.0242   0.7199   0.0554
  -4.750  -0.3011   0.02887   0.01814  -0.0247   0.7137   0.0559
  -4.500  -0.2722   0.02756   0.01683  -0.0252   0.7091   0.0577
  -4.250  -0.2454   0.02665   0.01588  -0.0249   0.7058   0.0596
  -4.000  -0.2179   0.02596   0.01514  -0.0251   0.7014   0.0615
  -3.750  -0.1903   0.02532   0.01448  -0.0254   0.6970   0.0628
  -3.500  -0.1644   0.02468   0.01380  -0.0251   0.6936   0.0641
  -3.250  -0.1400   0.02408   0.01313  -0.0244   0.6909   0.0657
  -3.000  -0.1167   0.02358   0.01253  -0.0235   0.6885   0.0674
  -2.750  -0.0947   0.02327   0.01226  -0.0230   0.6831   0.0694
  -2.500  -0.0728   0.02284   0.01181  -0.0221   0.6792   0.0726
  -2.250  -0.0495   0.02245   0.01135  -0.0212   0.6761   0.0780
  -2.000  -0.0253   0.02199   0.01084  -0.0204   0.6737   0.0857
  -1.750  -0.0014   0.02184   0.01080  -0.0202   0.6680   0.0984
  -1.500   0.0791   0.02038   0.01242  -0.0277   0.6652   0.8376
  -1.250   0.1270   0.02174   0.01359  -0.0290   0.6620   0.8926
  -1.000   0.2328   0.02290   0.01448  -0.0414   0.6598   0.9437
  -0.750   0.2804   0.02266   0.01408  -0.0454   0.6566   0.9518
  -0.500   0.3064   0.02275   0.01412  -0.0459   0.6508   0.9557
  -0.250   0.3302   0.02267   0.01395  -0.0455   0.6469   0.9593
   0.000   0.3609   0.02238   0.01353  -0.0463   0.6438   0.9616
   0.250   0.3900   0.02234   0.01345  -0.0472   0.6388   0.9644
   0.500   0.4168   0.02232   0.01340  -0.0476   0.6334   0.9671
   0.750   0.4426   0.02218   0.01319  -0.0475   0.6297   0.9703
   1.000   0.4689   0.02197   0.01289  -0.0474   0.6269   0.9729
   1.250   0.4975   0.02214   0.01310  -0.0486   0.6199   0.9749
   1.500   0.5260   0.02203   0.01297  -0.0491   0.6157   0.9773
   1.750   0.5537   0.02185   0.01273  -0.0494   0.6126   0.9798
   2.000   0.5790   0.02204   0.01296  -0.0497   0.6069   0.9822
   2.250   0.6055   0.02210   0.01304  -0.0500   0.6018   0.9844
   2.500   0.6350   0.02194   0.01287  -0.0507   0.5984   0.9864
   2.750   0.6632   0.02186   0.01277  -0.0512   0.5950   0.9884
   3.000   0.6889   0.02221   0.01323  -0.0518   0.5884   0.9905
   3.250   0.7161   0.02222   0.01326  -0.0522   0.5845   0.9927
   3.500   0.7442   0.02211   0.01315  -0.0525   0.5817   0.9945
   3.750   0.7705   0.02247   0.01363  -0.0533   0.5759   0.9964
   4.000   0.7976   0.02264   0.01387  -0.0539   0.5712   0.9984
   4.250   0.8254   0.02263   0.01390  -0.0543   0.5681   1.0000
   4.500   0.8478   0.02263   0.01393  -0.0534   0.5658   1.0000
   4.750   0.8639   0.02348   0.01495  -0.0526   0.5595   1.0000
   5.000   0.8833   0.02384   0.01539  -0.0517   0.5559   1.0000
   5.250   0.9040   0.02403   0.01567  -0.0508   0.5533   1.0000
   5.500   0.9257   0.02414   0.01585  -0.0499   0.5513   1.0000
   5.750   0.9372   0.02525   0.01713  -0.0486   0.5459   1.0000
   6.000   0.9526   0.02584   0.01784  -0.0472   0.5417   1.0000
   6.250   0.9733   0.02587   0.01798  -0.0461   0.5385   1.0000
   6.500   0.9911   0.02602   0.01823  -0.0447   0.5336   1.0000
   6.750   1.0053   0.02616   0.01847  -0.0427   0.5250   1.0000
   7.000   1.0212   0.02591   0.01830  -0.0405   0.5142   1.0000
   7.250   1.0402   0.02538   0.01781  -0.0386   0.5025   1.0000
   7.500   1.0598   0.02492   0.01740  -0.0367   0.4910   1.0000
   7.750   1.0693   0.02509   0.01764  -0.0339   0.4780   1.0000
   8.000   1.0797   0.02506   0.01761  -0.0310   0.4617   1.0000
   8.250   1.0807   0.02550   0.01805  -0.0270   0.4450   1.0000
   8.500   1.0763   0.02610   0.01863  -0.0224   0.4296   1.0000
   8.750   1.0503   0.02737   0.01997  -0.0152   0.4214   1.0000
   9.000   1.0346   0.02836   0.02097  -0.0095   0.4098   1.0000
   9.250   1.0185   0.02956   0.02217  -0.0042   0.3960   1.0000
   9.500   1.0000   0.03112   0.02376   0.0010   0.3815   1.0000
   9.750   0.9795   0.03313   0.02585   0.0057   0.3642   1.0000
  10.000   0.9641   0.03439   0.02658   0.0105   0.2758   1.0000
  10.250   0.9416   0.03680   0.02858   0.0149   0.2437   1.0000
  10.500   0.9210   0.03957   0.03113   0.0185   0.2127   1.0000
  10.750   0.9059   0.04225   0.03366   0.0212   0.1841   1.0000
  11.000   0.8906   0.04522   0.03644   0.0235   0.1514   1.0000
  11.250   0.8768   0.04830   0.03930   0.0254   0.1184   1.0000
  11.500   0.8649   0.05135   0.04211   0.0271   0.0848   1.0000
  11.750   0.8578   0.05404   0.04460   0.0285   0.0626   1.0000
  12.000   0.8564   0.05627   0.04676   0.0298   0.0498   1.0000
  12.250   0.8572   0.05837   0.04882   0.0309   0.0403   1.0000
  12.500   0.8599   0.06035   0.05080   0.0319   0.0357   1.0000
  12.750   0.8639   0.06224   0.05271   0.0327   0.0322   1.0000
  13.000   0.8675   0.06422   0.05470   0.0335   0.0303   1.0000
  13.250   0.8723   0.06616   0.05676   0.0342   0.0290   1.0000
  13.500   0.8765   0.06818   0.05887   0.0348   0.0279   1.0000
  13.750   0.8805   0.07026   0.06103   0.0353   0.0270   1.0000
  14.000   0.8835   0.07248   0.06331   0.0359   0.0258   1.0000
  14.250   0.8871   0.07465   0.06553   0.0363   0.0252   1.0000
  14.500   0.8917   0.07668   0.06762   0.0368   0.0245   1.0000
  14.750   0.8981   0.07855   0.06959   0.0373   0.0235   1.0000
  15.000   0.9046   0.08040   0.07153   0.0378   0.0226   1.0000
  15.250   0.9119   0.08215   0.07338   0.0383   0.0220   1.0000
  15.500   0.9205   0.08375   0.07504   0.0389   0.0215   1.0000
  15.750   0.9301   0.08522   0.07658   0.0395   0.0211   1.0000
  16.000   0.9403   0.08662   0.07802   0.0403   0.0206   1.0000
  16.250   0.9514   0.08799   0.07945   0.0410   0.0202   1.0000
  16.500   0.9639   0.08926   0.08078   0.0419   0.0199   1.0000
  16.750   0.9735   0.09113   0.08278   0.0425   0.0196   1.0000
  17.000   0.9766   0.09392   0.08578   0.0423   0.0194   1.0000
  17.250   0.9743   0.09758   0.08970   0.0417   0.0190   1.0000
  17.500   0.9727   0.10115   0.09348   0.0410   0.0188   1.0000
  17.750   0.9651   0.10570   0.09828   0.0397   0.0184   1.0000
  18.000   0.9606   0.10990   0.10268   0.0386   0.0185   1.0000
  18.250   0.9497   0.11522   0.10824   0.0365   0.0182   1.0000
  18.500   0.9394   0.12060   0.11383   0.0344   0.0182   1.0000
  18.750   0.9241   0.12710   0.12056   0.0314   0.0181   1.0000
  19.000   0.9091   0.13383   0.12749   0.0281   0.0181   1.0000
  19.250   0.8918   0.14146   0.13532   0.0241   0.0183   1.0000
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