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NACA 5-H-15 AIRFOIL (n5h15-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: NACA 5-H-15 AIRFOIL (n5h15-il)
Reynolds number: 500,000
Max Cl/Cd: 71.42 at α=7°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-n5h15-il-500000-n5.txt
Download as CSV file: xf-n5h15-il-500000-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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.500  -0.7020   0.05264   0.04904  -0.0525   0.7071   0.0208
 -11.250  -0.8216   0.03902   0.03450  -0.0404   0.7054   0.0222
 -11.000  -0.8353   0.03636   0.03150  -0.0352   0.7028   0.0225
 -10.750  -0.8409   0.03422   0.02912  -0.0310   0.6999   0.0229
 -10.500  -0.8326   0.03302   0.02780  -0.0286   0.6970   0.0232
 -10.250  -0.8200   0.03222   0.02691  -0.0267   0.6942   0.0234
 -10.000  -0.8065   0.03137   0.02595  -0.0249   0.6916   0.0236
  -9.750  -0.7923   0.03047   0.02490  -0.0232   0.6891   0.0239
  -9.500  -0.7761   0.02970   0.02404  -0.0217   0.6864   0.0242
  -9.250  -0.7589   0.02897   0.02321  -0.0204   0.6834   0.0246
  -9.000  -0.7418   0.02802   0.02210  -0.0190   0.6804   0.0250
  -8.750  -0.7244   0.02690   0.02080  -0.0176   0.6774   0.0254
  -8.500  -0.7063   0.02564   0.01933  -0.0163   0.6746   0.0258
  -8.250  -0.6867   0.02445   0.01795  -0.0152   0.6718   0.0262
  -8.000  -0.6655   0.02341   0.01675  -0.0143   0.6688   0.0267
  -7.750  -0.6433   0.02256   0.01574  -0.0135   0.6659   0.0272
  -7.500  -0.6202   0.02168   0.01469  -0.0129   0.6631   0.0275
  -7.250  -0.5964   0.02082   0.01368  -0.0124   0.6604   0.0278
  -6.750  -0.5468   0.01938   0.01200  -0.0117   0.6550   0.0282
  -6.500  -0.5213   0.01874   0.01126  -0.0115   0.6522   0.0283
  -6.250  -0.4954   0.01805   0.01048  -0.0113   0.6494   0.0285
  -6.000  -0.4686   0.01694   0.00928  -0.0115   0.6468   0.0290
  -5.750  -0.4429   0.01626   0.00854  -0.0113   0.6444   0.0295
  -5.500  -0.4175   0.01579   0.00801  -0.0110   0.6422   0.0300
  -5.250  -0.3920   0.01538   0.00759  -0.0108   0.6398   0.0305
  -5.000  -0.3666   0.01498   0.00717  -0.0105   0.6368   0.0309
  -4.750  -0.3414   0.01456   0.00671  -0.0102   0.6336   0.0313
  -4.500  -0.3163   0.01420   0.00631  -0.0098   0.6307   0.0318
  -4.250  -0.2916   0.01385   0.00591  -0.0093   0.6277   0.0321
  -4.000  -0.2667   0.01352   0.00555  -0.0089   0.6247   0.0326
  -3.750  -0.2417   0.01322   0.00523  -0.0085   0.6220   0.0331
  -3.500  -0.2169   0.01293   0.00492  -0.0080   0.6191   0.0335
  -3.250  -0.1921   0.01267   0.00462  -0.0075   0.6165   0.0341
  -3.000  -0.1671   0.01244   0.00435  -0.0071   0.6139   0.0346
  -2.750  -0.1421   0.01222   0.00409  -0.0066   0.6116   0.0350
  -2.500  -0.1167   0.01202   0.00388  -0.0063   0.6090   0.0355
  -2.250  -0.0915   0.01180   0.00365  -0.0059   0.6060   0.0362
  -2.000  -0.0665   0.01157   0.00343  -0.0054   0.6031   0.0378
  -1.750  -0.0410   0.01141   0.00326  -0.0051   0.6001   0.0395
  -1.500  -0.0153   0.01127   0.00310  -0.0048   0.5972   0.0413
  -1.250   0.0106   0.01115   0.00297  -0.0045   0.5944   0.0432
  -1.000   0.0367   0.01102   0.00286  -0.0043   0.5910   0.0458
  -0.750   0.0624   0.01088   0.00275  -0.0040   0.5874   0.0520
  -0.500   0.0880   0.01076   0.00265  -0.0037   0.5839   0.0622
  -0.250   0.1128   0.01059   0.00254  -0.0032   0.5806   0.0869
   0.000   0.1304   0.00995   0.00243  -0.0016   0.5769   0.2470
   0.250   0.1341   0.00879   0.00222   0.0027   0.5728   0.5094
   0.500   0.1276   0.00769   0.00236   0.0103   0.5690   0.8305
   0.750   0.1521   0.00782   0.00251   0.0112   0.5647   0.8616
   1.000   0.1792   0.00792   0.00262   0.0114   0.5595   0.8747
   1.250   0.2062   0.00805   0.00272   0.0117   0.5540   0.8852
   1.500   0.2314   0.00822   0.00288   0.0124   0.5488   0.8977
   1.750   0.2636   0.00848   0.00315   0.0117   0.5424   0.9077
   2.000   0.2884   0.00858   0.00321   0.0123   0.5362   0.9134
   2.250   0.3196   0.00866   0.00328   0.0115   0.5291   0.9152
   2.500   0.3492   0.00875   0.00333   0.0109   0.5218   0.9170
   2.750   0.3777   0.00882   0.00338   0.0106   0.5140   0.9188
   3.000   0.4044   0.00891   0.00342   0.0106   0.5064   0.9209
   3.250   0.4300   0.00897   0.00346   0.0108   0.4986   0.9230
   3.500   0.4537   0.00903   0.00349   0.0114   0.4917   0.9250
   3.750   0.4767   0.00908   0.00352   0.0121   0.4853   0.9269
   4.000   0.5012   0.00915   0.00356   0.0125   0.4794   0.9284
   4.250   0.5293   0.00925   0.00366   0.0121   0.4745   0.9295
   4.500   0.5575   0.00935   0.00377   0.0117   0.4699   0.9305
   4.750   0.5848   0.00947   0.00388   0.0115   0.4653   0.9316
   5.000   0.6114   0.00960   0.00401   0.0113   0.4601   0.9328
   5.250   0.6369   0.00977   0.00415   0.0114   0.4502   0.9342
   5.500   0.6617   0.00993   0.00430   0.0116   0.4425   0.9357
   5.750   0.6852   0.01012   0.00447   0.0120   0.4332   0.9376
   6.000   0.7079   0.01028   0.00463   0.0126   0.4254   0.9399
   6.250   0.7258   0.01049   0.00481   0.0141   0.4149   0.9429
   6.500   0.7490   0.01066   0.00500   0.0145   0.4047   0.9446
   6.750   0.7745   0.01089   0.00524   0.0144   0.3956   0.9460
   7.000   0.7985   0.01118   0.00551   0.0145   0.3802   0.9476
   7.250   0.8200   0.01155   0.00584   0.0149   0.3557   0.9498
   7.500   0.8013   0.01303   0.00691   0.0214   0.2622   0.9590
   7.750   0.8051   0.01530   0.00891   0.0214   0.2016   0.9641
   8.000   0.8108   0.01730   0.01065   0.0215   0.1454   0.9691
   8.250   0.8048   0.02045   0.01334   0.0216   0.0620   0.9742
   8.500   0.8209   0.02185   0.01468   0.0209   0.0430   0.9765
   8.750   0.8294   0.02371   0.01642   0.0208   0.0184   0.9802
   9.000   0.8446   0.02481   0.01756   0.0208   0.0168   0.9838
   9.250   0.8627   0.02607   0.01886   0.0199   0.0150   0.9857
   9.500   0.8816   0.02718   0.02002   0.0192   0.0143   0.9879
   9.750   0.8986   0.02840   0.02130   0.0186   0.0136   0.9907
  10.000   0.9139   0.02972   0.02268   0.0182   0.0127   0.9937
  10.250   0.9301   0.03115   0.02416   0.0175   0.0122   0.9973
  10.500   0.9444   0.03287   0.02594   0.0166   0.0116   0.9993
  10.750   0.9499   0.03436   0.02747   0.0177   0.0112   1.0000
  11.000   0.9516   0.03555   0.02870   0.0200   0.0110   1.0000
  11.250   0.9540   0.03692   0.03011   0.0219   0.0109   1.0000
  11.500   0.9578   0.03834   0.03158   0.0235   0.0105   1.0000
  11.750   0.9637   0.03971   0.03299   0.0249   0.0100   1.0000
  12.000   0.9669   0.04139   0.03472   0.0261   0.0102   1.0000
  12.250   0.9730   0.04289   0.03625   0.0272   0.0096   1.0000
  12.500   0.9786   0.04451   0.03791   0.0281   0.0092   1.0000
  12.750   0.9840   0.04620   0.03963   0.0289   0.0089   1.0000
  13.000   0.9876   0.04812   0.04161   0.0298   0.0089   1.0000
  13.250   0.9917   0.05002   0.04355   0.0305   0.0087   1.0000
  13.500   0.9930   0.05225   0.04582   0.0312   0.0085   1.0000
  13.750   0.9943   0.05452   0.04813   0.0319   0.0084   1.0000
  14.000   0.9997   0.05645   0.05014   0.0324   0.0081   1.0000
  14.250   1.0074   0.05817   0.05192   0.0326   0.0079   1.0000
  14.500   1.0120   0.06024   0.05404   0.0330   0.0078   1.0000
  14.750   1.0165   0.06233   0.05619   0.0334   0.0077   1.0000
  15.000   1.0215   0.06441   0.05833   0.0336   0.0076   1.0000
  15.250   1.0269   0.06645   0.06043   0.0338   0.0075   1.0000
  15.500   1.0318   0.06858   0.06262   0.0340   0.0073   1.0000
  15.750   1.0366   0.07072   0.06483   0.0342   0.0073   1.0000
  16.000   1.0422   0.07288   0.06706   0.0341   0.0070   1.0000
  16.250   1.0469   0.07513   0.06937   0.0341   0.0069   1.0000
  16.500   1.0517   0.07739   0.07169   0.0340   0.0068   1.0000
  16.750   1.0559   0.07976   0.07412   0.0339   0.0066   1.0000
  17.000   1.0604   0.08219   0.07660   0.0335   0.0065   1.0000
  17.250   1.0635   0.08479   0.07925   0.0331   0.0063   1.0000
  17.500   1.0664   0.08734   0.08187   0.0328   0.0063   1.0000
  17.750   1.0683   0.09003   0.08461   0.0326   0.0061   1.0000
  18.000   1.0708   0.09271   0.08738   0.0321   0.0061   1.0000
  18.250   1.0714   0.09552   0.09027   0.0319   0.0060   1.0000
  18.500   1.0730   0.09846   0.09331   0.0313   0.0060   1.0000
  18.750   1.0724   0.10179   0.09677   0.0304   0.0059   1.0000
  19.000   1.0724   0.10497   0.10006   0.0297   0.0058   1.0000
  19.250   1.0713   0.10839   0.10358   0.0288   0.0058   1.0000
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