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HQ 3.5/14 AIRFOIL (hq3514-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: HQ 3.5/14 AIRFOIL (hq3514-il)
Reynolds number: 1,000,000
Max Cl/Cd: 112.77 at α=4.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-hq3514-il-1000000.txt
Download as CSV file: xf-hq3514-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: HQ 3.5/14 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
  ------ -------- --------- --------- -------- -------- --------
 -16.750  -0.6986   0.10513   0.10295  -0.0548   1.0000   0.0102
 -16.500  -0.7806   0.08621   0.08383  -0.0655   1.0000   0.0099
 -16.250  -0.8474   0.07041   0.06783  -0.0751   1.0000   0.0098
 -16.000  -0.8929   0.05812   0.05532  -0.0834   1.0000   0.0097
 -15.750  -0.9216   0.05008   0.04710  -0.0889   1.0000   0.0096
 -15.500  -0.9372   0.04487   0.04175  -0.0921   1.0000   0.0097
 -15.250  -0.9495   0.04051   0.03727  -0.0944   1.0000   0.0097
 -15.000  -0.9568   0.03710   0.03373  -0.0958   1.0000   0.0098
 -14.750  -0.9614   0.03430   0.03083  -0.0965   1.0000   0.0099
 -14.500  -0.9603   0.03235   0.02878  -0.0964   1.0000   0.0101
 -14.250  -0.9671   0.03022   0.02657  -0.0954   1.0000   0.0101
 -14.000  -0.9765   0.02889   0.02518  -0.0926   1.0000   0.0101
 -13.750  -0.9639   0.02551   0.02161  -0.0977   0.9942   0.0105
 -13.500  -0.9455   0.02355   0.01954  -0.1004   0.9872   0.0109
 -13.250  -0.9173   0.02235   0.01827  -0.1028   0.9841   0.0113
 -13.000  -0.8866   0.02138   0.01723  -0.1051   0.9815   0.0117
 -12.750  -0.8599   0.02040   0.01615  -0.1066   0.9758   0.0121
 -12.500  -0.8288   0.01961   0.01527  -0.1085   0.9718   0.0126
 -12.250  -0.8023   0.01889   0.01445  -0.1093   0.9649   0.0129
 -12.000  -0.7823   0.01764   0.01310  -0.1096   0.9559   0.0137
 -11.750  -0.7623   0.01714   0.01256  -0.1088   0.9456   0.0143
 -11.500  -0.7409   0.01666   0.01200  -0.1081   0.9366   0.0149
 -11.250  -0.7193   0.01621   0.01147  -0.1074   0.9273   0.0155
 -11.000  -0.6969   0.01584   0.01101  -0.1067   0.9180   0.0160
 -10.750  -0.6778   0.01508   0.01017  -0.1058   0.9087   0.0171
 -10.500  -0.6546   0.01471   0.00976  -0.1052   0.8997   0.0179
 -10.250  -0.6304   0.01442   0.00940  -0.1048   0.8921   0.0188
 -10.000  -0.6058   0.01414   0.00903  -0.1044   0.8842   0.0195
  -9.750  -0.5835   0.01358   0.00840  -0.1038   0.8770   0.0207
  -9.500  -0.5584   0.01332   0.00811  -0.1035   0.8702   0.0218
  -9.250  -0.5328   0.01312   0.00785  -0.1032   0.8639   0.0229
  -9.000  -0.5066   0.01291   0.00759  -0.1030   0.8584   0.0238
  -8.750  -0.4829   0.01239   0.00700  -0.1026   0.8526   0.0251
  -8.500  -0.4572   0.01212   0.00670  -0.1024   0.8473   0.0263
  -8.250  -0.4308   0.01188   0.00644  -0.1022   0.8419   0.0274
  -8.000  -0.4041   0.01169   0.00619  -0.1021   0.8364   0.0285
  -7.750  -0.3784   0.01136   0.00580  -0.1019   0.8309   0.0298
  -7.500  -0.3524   0.01102   0.00547  -0.1017   0.8246   0.0315
  -7.250  -0.3257   0.01084   0.00524  -0.1015   0.8185   0.0330
  -7.000  -0.2984   0.01067   0.00503  -0.1015   0.8124   0.0344
  -6.750  -0.2717   0.01039   0.00470  -0.1014   0.8061   0.0358
  -6.500  -0.2454   0.01008   0.00438  -0.1012   0.8005   0.0381
  -6.250  -0.2179   0.00989   0.00417  -0.1012   0.7945   0.0398
  -6.000  -0.1903   0.00975   0.00399  -0.1012   0.7886   0.0416
  -5.750  -0.1633   0.00948   0.00367  -0.1011   0.7831   0.0439
  -5.500  -0.1359   0.00926   0.00345  -0.1010   0.7769   0.0467
  -5.250  -0.1084   0.00915   0.00329  -0.1010   0.7710   0.0493
  -5.000  -0.0805   0.00899   0.00310  -0.1010   0.7652   0.0518
  -4.750  -0.0530   0.00877   0.00289  -0.1010   0.7595   0.0564
  -4.500  -0.0252   0.00868   0.00275  -0.1010   0.7540   0.0597
  -4.250   0.0028   0.00851   0.00258  -0.1011   0.7482   0.0645
  -4.000   0.0306   0.00838   0.00244  -0.1011   0.7422   0.0698
  -3.750   0.0587   0.00830   0.00233  -0.1011   0.7367   0.0735
  -3.500   0.0867   0.00813   0.00218  -0.1012   0.7308   0.0819
  -3.250   0.1147   0.00805   0.00207  -0.1012   0.7256   0.0890
  -3.000   0.1428   0.00791   0.00194  -0.1013   0.7210   0.0998
  -2.750   0.1707   0.00768   0.00181  -0.1014   0.7161   0.1253
  -2.500   0.1978   0.00733   0.00170  -0.1015   0.7112   0.2068
  -2.250   0.2251   0.00705   0.00159  -0.1016   0.7065   0.2671
  -2.000   0.2522   0.00659   0.00145  -0.1018   0.7018   0.3658
  -1.750   0.2793   0.00626   0.00145  -0.1019   0.6969   0.4839
  -1.500   0.3075   0.00626   0.00144  -0.1019   0.6920   0.5063
  -1.250   0.3363   0.00622   0.00143  -0.1020   0.6871   0.5219
  -1.000   0.3647   0.00620   0.00142  -0.1021   0.6815   0.5367
  -0.750   0.3929   0.00622   0.00142  -0.1021   0.6766   0.5482
  -0.500   0.4218   0.00620   0.00142  -0.1023   0.6722   0.5583
  -0.250   0.4503   0.00619   0.00143  -0.1024   0.6671   0.5686
   0.000   0.4784   0.00621   0.00145  -0.1024   0.6616   0.5795
   0.250   0.5069   0.00621   0.00147  -0.1025   0.6552   0.5907
   0.500   0.5349   0.00623   0.00150  -0.1025   0.6482   0.6037
   0.750   0.5630   0.00625   0.00153  -0.1025   0.6405   0.6144
   1.000   0.5907   0.00629   0.00156  -0.1024   0.6307   0.6261
   1.250   0.6188   0.00632   0.00160  -0.1025   0.6224   0.6364
   1.500   0.6463   0.00639   0.00164  -0.1024   0.6128   0.6446
   1.750   0.6738   0.00645   0.00169  -0.1023   0.6000   0.6537
   2.000   0.7006   0.00654   0.00175  -0.1021   0.5840   0.6626
   2.250   0.7271   0.00666   0.00181  -0.1018   0.5652   0.6715
   2.500   0.7526   0.00682   0.00191  -0.1014   0.5393   0.6791
   2.750   0.7770   0.00707   0.00203  -0.1007   0.5078   0.6872
   3.000   0.8004   0.00736   0.00219  -0.1000   0.4771   0.6950
   3.250   0.8250   0.00761   0.00236  -0.0994   0.4582   0.7032
   3.500   0.8499   0.00781   0.00252  -0.0989   0.4429   0.7106
   3.750   0.8757   0.00797   0.00266  -0.0986   0.4311   0.7178
   4.000   0.9015   0.00812   0.00280  -0.0982   0.4209   0.7239
   4.250   0.9266   0.00830   0.00296  -0.0978   0.4092   0.7306
   4.500   0.9516   0.00850   0.00311  -0.0973   0.3947   0.7374
   4.750   0.9766   0.00866   0.00326  -0.0969   0.3765   0.7452
   5.000   0.9988   0.00899   0.00345  -0.0960   0.3407   0.7528
   5.250   1.0198   0.00935   0.00371  -0.0948   0.3165   0.7600
   5.500   1.0422   0.00965   0.00395  -0.0940   0.3029   0.7675
   5.750   1.0656   0.00985   0.00417  -0.0932   0.2931   0.7753
   6.250   1.1111   0.01031   0.00463  -0.0916   0.2747   0.7938
   6.500   1.1339   0.01050   0.00485  -0.0907   0.2653   0.8049
   6.750   1.1550   0.01075   0.00510  -0.0896   0.2537   0.8189
   7.000   1.1753   0.01099   0.00534  -0.0884   0.2409   0.8371
   7.250   1.1941   0.01119   0.00559  -0.0868   0.2261   0.8661
   7.500   1.2146   0.01140   0.00589  -0.0856   0.2024   1.0000
   7.750   1.2280   0.01192   0.00627  -0.0832   0.1821   1.0000
   8.000   1.2438   0.01234   0.00663  -0.0812   0.1712   1.0000
   8.250   1.2607   0.01272   0.00699  -0.0795   0.1637   1.0000
   8.500   1.2774   0.01312   0.00737  -0.0778   0.1577   1.0000
   8.750   1.2943   0.01352   0.00777  -0.0761   0.1517   1.0000
   9.000   1.3120   0.01390   0.00814  -0.0746   0.1459   1.0000
   9.250   1.3270   0.01441   0.00862  -0.0728   0.1389   1.0000
   9.500   1.3460   0.01474   0.00899  -0.0716   0.1353   1.0000
   9.750   1.3631   0.01517   0.00942  -0.0701   0.1304   1.0000
  10.000   1.3783   0.01571   0.00994  -0.0685   0.1242   1.0000
  10.250   1.3961   0.01613   0.01037  -0.0672   0.1193   1.0000
  10.500   1.4107   0.01672   0.01094  -0.0656   0.1129   1.0000
  10.750   1.4270   0.01724   0.01148  -0.0642   0.1076   1.0000
  11.000   1.4407   0.01791   0.01212  -0.0626   0.1005   1.0000
  11.250   1.4545   0.01861   0.01280  -0.0610   0.0921   1.0000
  11.500   1.4657   0.01947   0.01362  -0.0592   0.0823   1.0000
  11.750   1.4717   0.02068   0.01472  -0.0570   0.0668   1.0000
  12.000   1.4738   0.02219   0.01612  -0.0544   0.0499   1.0000
  12.250   1.4782   0.02361   0.01749  -0.0522   0.0405   1.0000
  12.500   1.4860   0.02485   0.01872  -0.0505   0.0355   1.0000
  12.750   1.4933   0.02617   0.02005  -0.0488   0.0317   1.0000
  13.000   1.5037   0.02729   0.02122  -0.0475   0.0293   1.0000
  13.250   1.5112   0.02867   0.02261  -0.0461   0.0268   1.0000
  13.500   1.5198   0.02999   0.02397  -0.0449   0.0243   1.0000
  13.750   1.5266   0.03150   0.02550  -0.0436   0.0216   1.0000
  14.000   1.5335   0.03305   0.02708  -0.0424   0.0186   1.0000
  14.250   1.5381   0.03483   0.02888  -0.0412   0.0157   1.0000
  14.500   1.5409   0.03685   0.03092  -0.0400   0.0132   1.0000
  14.750   1.5458   0.03873   0.03285  -0.0391   0.0119   1.0000
  15.000   1.5487   0.04087   0.03503  -0.0382   0.0109   1.0000
  15.250   1.5514   0.04311   0.03734  -0.0375   0.0102   1.0000
  15.500   1.5554   0.04528   0.03959  -0.0369   0.0097   1.0000
  15.750   1.5579   0.04766   0.04204  -0.0364   0.0092   1.0000
  16.000   1.5588   0.05030   0.04475  -0.0361   0.0089   1.0000
  16.250   1.5554   0.05352   0.04806  -0.0358   0.0084   1.0000
  16.500   1.5515   0.05695   0.05159  -0.0358   0.0081   1.0000
  16.750   1.5519   0.05993   0.05465  -0.0359   0.0080   1.0000
  17.000   1.5506   0.06323   0.05806  -0.0363   0.0078   1.0000
  17.250   1.5468   0.06698   0.06190  -0.0368   0.0076   1.0000
  17.500   1.5425   0.07093   0.06596  -0.0376   0.0075   1.0000
  17.750   1.5369   0.07517   0.07031  -0.0387   0.0073   1.0000
  18.000   1.5310   0.07961   0.07485  -0.0400   0.0071   1.0000
  18.250   1.5225   0.08459   0.07995  -0.0416   0.0071   1.0000
  18.500   1.5122   0.09000   0.08548  -0.0435   0.0069   1.0000
  18.750   1.5007   0.09571   0.09131  -0.0458   0.0069   1.0000
  19.000   1.4888   0.10158   0.09729  -0.0482   0.0068   1.0000
  19.250   1.4739   0.10812   0.10396  -0.0511   0.0067   1.0000
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