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HQ 3.0/13 AIRFOIL (hq3013-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: HQ 3.0/13 AIRFOIL (hq3013-il)
Reynolds number: 1,000,000
Max Cl/Cd: 115.3 at α=3.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-hq3013-il-1000000.txt
Download as CSV file: xf-hq3013-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: HQ 3.0/13 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
  ------ -------- --------- --------- -------- -------- --------
 -14.250  -0.7376   0.06815   0.06587  -0.0653   1.0000   0.0074
 -14.000  -0.7635   0.05833   0.05589  -0.0722   1.0000   0.0073
 -13.750  -0.7873   0.05043   0.04782  -0.0780   1.0000   0.0073
 -13.500  -0.7955   0.04589   0.04316  -0.0811   1.0000   0.0072
 -13.250  -0.8166   0.04030   0.03740  -0.0843   1.0000   0.0073
 -13.000  -0.8275   0.03666   0.03363  -0.0857   1.0000   0.0073
 -12.750  -0.8469   0.03298   0.02980  -0.0858   1.0000   0.0074
 -12.500  -0.8649   0.03084   0.02756  -0.0834   1.0000   0.0074
 -12.250  -0.8692   0.02832   0.02488  -0.0838   0.9966   0.0075
 -12.000  -0.8476   0.02606   0.02246  -0.0867   0.9914   0.0077
 -11.750  -0.8239   0.02426   0.02050  -0.0888   0.9869   0.0078
 -11.500  -0.7958   0.02284   0.01897  -0.0910   0.9840   0.0080
 -11.250  -0.7664   0.02159   0.01760  -0.0931   0.9811   0.0082
 -11.000  -0.7406   0.02034   0.01622  -0.0943   0.9751   0.0084
 -10.750  -0.7106   0.01922   0.01497  -0.0961   0.9709   0.0086
 -10.500  -0.6860   0.01818   0.01380  -0.0966   0.9620   0.0088
 -10.250  -0.6604   0.01728   0.01277  -0.0970   0.9536   0.0089
 -10.000  -0.6380   0.01654   0.01191  -0.0966   0.9423   0.0092
  -9.750  -0.6159   0.01590   0.01117  -0.0960   0.9311   0.0093
  -9.500  -0.5935   0.01531   0.01046  -0.0954   0.9206   0.0095
  -9.250  -0.5725   0.01452   0.00952  -0.0945   0.9104   0.0097
  -9.000  -0.5523   0.01364   0.00852  -0.0936   0.9002   0.0101
  -8.750  -0.5294   0.01306   0.00784  -0.0930   0.8918   0.0106
  -8.500  -0.5053   0.01261   0.00732  -0.0925   0.8835   0.0111
  -8.250  -0.4805   0.01223   0.00687  -0.0921   0.8762   0.0117
  -8.000  -0.4552   0.01189   0.00645  -0.0918   0.8690   0.0123
  -7.750  -0.4306   0.01142   0.00589  -0.0913   0.8624   0.0131
  -7.500  -0.4055   0.01098   0.00541  -0.0910   0.8557   0.0142
  -7.250  -0.3796   0.01069   0.00505  -0.0907   0.8498   0.0154
  -7.000  -0.3537   0.01031   0.00466  -0.0904   0.8437   0.0179
  -6.750  -0.3275   0.01002   0.00436  -0.0902   0.8379   0.0222
  -6.500  -0.3006   0.00982   0.00415  -0.0901   0.8326   0.0274
  -6.250  -0.2734   0.00965   0.00399  -0.0900   0.8269   0.0312
  -6.000  -0.2462   0.00949   0.00379  -0.0899   0.8216   0.0341
  -5.750  -0.2189   0.00930   0.00361  -0.0899   0.8164   0.0376
  -5.500  -0.1912   0.00918   0.00346  -0.0899   0.8110   0.0399
  -5.250  -0.1640   0.00901   0.00323  -0.0898   0.8058   0.0424
  -5.000  -0.1366   0.00879   0.00302  -0.0897   0.8007   0.0462
  -4.750  -0.1089   0.00866   0.00287  -0.0897   0.7952   0.0495
  -4.500  -0.0814   0.00851   0.00267  -0.0896   0.7900   0.0543
  -4.250  -0.0537   0.00833   0.00252  -0.0896   0.7846   0.0607
  -4.000  -0.0262   0.00815   0.00234  -0.0896   0.7787   0.0694
  -3.750   0.0013   0.00800   0.00218  -0.0895   0.7729   0.0802
  -3.500   0.0289   0.00779   0.00204  -0.0895   0.7665   0.0982
  -3.250   0.0560   0.00757   0.00189  -0.0894   0.7607   0.1300
  -3.000   0.0829   0.00722   0.00175  -0.0895   0.7554   0.1915
  -2.750   0.1099   0.00688   0.00162  -0.0895   0.7499   0.2585
  -2.500   0.1361   0.00646   0.00146  -0.0894   0.7448   0.3500
  -2.250   0.1626   0.00605   0.00140  -0.0894   0.7396   0.4649
  -2.000   0.1906   0.00595   0.00137  -0.0894   0.7340   0.5013
  -1.750   0.2186   0.00592   0.00135  -0.0894   0.7284   0.5264
  -1.500   0.2469   0.00586   0.00134  -0.0894   0.7217   0.5492
  -1.250   0.2749   0.00587   0.00133  -0.0894   0.7146   0.5650
  -1.000   0.3034   0.00586   0.00131  -0.0894   0.7071   0.5751
  -0.750   0.3314   0.00588   0.00130  -0.0894   0.6998   0.5845
  -0.500   0.3597   0.00587   0.00131  -0.0894   0.6927   0.6001
  -0.250   0.3876   0.00589   0.00133  -0.0893   0.6860   0.6160
   0.000   0.4160   0.00590   0.00134  -0.0894   0.6794   0.6246
   0.250   0.4441   0.00593   0.00136  -0.0894   0.6721   0.6326
   0.500   0.4722   0.00595   0.00137  -0.0894   0.6641   0.6402
   1.000   0.5276   0.00602   0.00142  -0.0892   0.6445   0.6583
   1.250   0.5555   0.00607   0.00145  -0.0892   0.6359   0.6659
   1.500   0.5830   0.00611   0.00149  -0.0891   0.6261   0.6725
   1.750   0.6108   0.00615   0.00153  -0.0891   0.6154   0.6798
   2.000   0.6383   0.00621   0.00157  -0.0889   0.6048   0.6870
   2.250   0.6654   0.00628   0.00163  -0.0888   0.5919   0.6950
   2.500   0.6922   0.00636   0.00169  -0.0886   0.5771   0.7026
   2.750   0.7189   0.00647   0.00176  -0.0883   0.5608   0.7112
   3.000   0.7451   0.00659   0.00185  -0.0880   0.5418   0.7198
   3.250   0.7707   0.00675   0.00195  -0.0876   0.5210   0.7294
   3.500   0.7961   0.00692   0.00207  -0.0872   0.4980   0.7395
   3.750   0.8209   0.00712   0.00221  -0.0866   0.4755   0.7497
   4.000   0.8457   0.00734   0.00237  -0.0861   0.4511   0.7606
   4.250   0.8699   0.00757   0.00254  -0.0855   0.4271   0.7722
   4.500   0.8941   0.00780   0.00271  -0.0849   0.4043   0.7845
   4.750   0.9180   0.00804   0.00291  -0.0842   0.3822   0.7973
   5.000   0.9412   0.00831   0.00311  -0.0834   0.3564   0.8111
   5.250   0.9641   0.00857   0.00332  -0.0826   0.3313   0.8260
   5.500   0.9862   0.00886   0.00355  -0.0816   0.3079   0.8435
   5.750   1.0080   0.00909   0.00377  -0.0805   0.2880   0.8663
   6.000   1.0291   0.00918   0.00399  -0.0792   0.2710   0.9360
   6.250   1.0603   0.00950   0.00425  -0.0803   0.2530   1.0000
   6.500   1.0833   0.00983   0.00450  -0.0796   0.2369   1.0000
   6.750   1.1058   0.01016   0.00475  -0.0788   0.2204   1.0000
   7.000   1.1282   0.01049   0.00501  -0.0780   0.2055   1.0000
   7.250   1.1501   0.01083   0.00530  -0.0771   0.1917   1.0000
   7.500   1.1713   0.01120   0.00560  -0.0760   0.1767   1.0000
   7.750   1.1916   0.01160   0.00591  -0.0749   0.1614   1.0000
   8.000   1.2117   0.01199   0.00624  -0.0737   0.1493   1.0000
   8.250   1.2325   0.01232   0.00654  -0.0726   0.1398   1.0000
   8.500   1.2520   0.01268   0.00688  -0.0713   0.1299   1.0000
   8.750   1.2691   0.01307   0.00723  -0.0696   0.1205   1.0000
   9.000   1.2851   0.01349   0.00760  -0.0676   0.1109   1.0000
   9.250   1.2997   0.01397   0.00802  -0.0655   0.0990   1.0000
   9.500   1.3150   0.01444   0.00846  -0.0636   0.0896   1.0000
   9.750   1.3294   0.01497   0.00895  -0.0616   0.0804   1.0000
  10.000   1.3427   0.01556   0.00949  -0.0595   0.0707   1.0000
  10.250   1.3561   0.01618   0.01006  -0.0575   0.0623   1.0000
  10.500   1.3692   0.01682   0.01068  -0.0555   0.0544   1.0000
  10.750   1.3817   0.01751   0.01134  -0.0535   0.0477   1.0000
  11.000   1.3940   0.01824   0.01206  -0.0516   0.0422   1.0000
  11.250   1.4069   0.01895   0.01277  -0.0498   0.0375   1.0000
  11.500   1.4169   0.01986   0.01365  -0.0478   0.0315   1.0000
  11.750   1.4297   0.02063   0.01443  -0.0462   0.0285   1.0000
  12.000   1.4379   0.02171   0.01549  -0.0442   0.0221   1.0000
  12.250   1.4466   0.02281   0.01657  -0.0423   0.0175   1.0000
  12.500   1.4515   0.02420   0.01793  -0.0403   0.0116   1.0000
  12.750   1.4568   0.02563   0.01935  -0.0383   0.0071   1.0000
  13.000   1.4603   0.02725   0.02101  -0.0364   0.0053   1.0000
  13.250   1.4703   0.02841   0.02223  -0.0351   0.0052   1.0000
  13.500   1.4775   0.02984   0.02372  -0.0337   0.0048   1.0000
  13.750   1.4845   0.03132   0.02528  -0.0325   0.0046   1.0000
  14.000   1.4912   0.03287   0.02691  -0.0313   0.0044   1.0000
  14.250   1.4968   0.03455   0.02868  -0.0302   0.0043   1.0000
  14.500   1.5009   0.03644   0.03064  -0.0291   0.0041   1.0000
  14.750   1.5035   0.03852   0.03281  -0.0281   0.0039   1.0000
  15.000   1.5076   0.04053   0.03491  -0.0274   0.0039   1.0000
  15.250   1.5079   0.04300   0.03748  -0.0267   0.0038   1.0000
  15.500   1.5052   0.04591   0.04049  -0.0261   0.0036   1.0000
  15.750   1.5036   0.04880   0.04349  -0.0258   0.0036   1.0000
  16.000   1.5050   0.05147   0.04625  -0.0257   0.0036   1.0000
  16.250   1.4918   0.05605   0.05097  -0.0259   0.0034   1.0000
  16.500   1.4880   0.05965   0.05468  -0.0264   0.0034   1.0000
  16.750   1.4771   0.06434   0.05951  -0.0273   0.0033   1.0000
  17.000   1.4713   0.06855   0.06383  -0.0283   0.0033   1.0000
  17.250   1.4600   0.07374   0.06915  -0.0298   0.0033   1.0000
  17.500   1.4515   0.07870   0.07423  -0.0315   0.0033   1.0000
  17.750   1.4378   0.08468   0.08035  -0.0338   0.0033   1.0000
  18.000   1.4281   0.09021   0.08599  -0.0361   0.0033   1.0000
  18.250   1.4143   0.09657   0.09249  -0.0389   0.0033   1.0000
  18.500   1.3998   0.10325   0.09930  -0.0420   0.0033   1.0000
  18.750   1.3859   0.10997   0.10615  -0.0452   0.0033   1.0000
  19.000   1.3682   0.11757   0.11388  -0.0491   0.0033   1.0000
  19.250   1.3523   0.12497   0.12141  -0.0530   0.0033   1.0000
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