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HQ 3.0/14 AIRFOIL (hq3014-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: HQ 3.0/14 AIRFOIL (hq3014-il)
Reynolds number: 500,000
Max Cl/Cd: 85.43 at α=4.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-hq3014-il-500000-n5.txt
Download as CSV file: xf-hq3014-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: HQ 3.0/14 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
  ------ -------- --------- --------- -------- -------- --------
 -16.000  -0.5638   0.12631   0.12362  -0.0394   1.0000   0.0086
 -15.750  -0.6414   0.10546   0.10258  -0.0495   1.0000   0.0085
 -15.500  -0.6925   0.09162   0.08863  -0.0568   1.0000   0.0083
 -15.250  -0.7470   0.07746   0.07429  -0.0647   1.0000   0.0081
 -15.000  -0.7873   0.06581   0.06245  -0.0719   1.0000   0.0080
 -14.750  -0.8140   0.05717   0.05362  -0.0777   1.0000   0.0080
 -14.500  -0.8337   0.05078   0.04706  -0.0817   1.0000   0.0080
 -14.250  -0.8476   0.04589   0.04203  -0.0845   1.0000   0.0080
 -14.000  -0.8584   0.04185   0.03785  -0.0863   1.0000   0.0080
 -13.750  -0.8660   0.03855   0.03443  -0.0873   1.0000   0.0081
 -13.500  -0.8708   0.03587   0.03163  -0.0876   1.0000   0.0082
 -13.250  -0.8766   0.03344   0.02909  -0.0872   1.0000   0.0082
 -13.000  -0.8816   0.03150   0.02706  -0.0861   1.0000   0.0084
 -12.500  -0.8588   0.02766   0.02294  -0.0890   0.9850   0.0086
 -12.250  -0.8385   0.02587   0.02099  -0.0915   0.9764   0.0088
 -12.000  -0.8158   0.02426   0.01924  -0.0936   0.9683   0.0090
 -11.750  -0.7924   0.02290   0.01777  -0.0951   0.9587   0.0093
 -11.500  -0.7682   0.02180   0.01656  -0.0962   0.9487   0.0096
 -11.250  -0.7439   0.02084   0.01549  -0.0969   0.9387   0.0098
 -11.000  -0.7217   0.02000   0.01453  -0.0970   0.9275   0.0101
 -10.750  -0.7008   0.01924   0.01363  -0.0966   0.9166   0.0104
 -10.500  -0.6798   0.01856   0.01283  -0.0961   0.9070   0.0107
 -10.250  -0.6590   0.01793   0.01207  -0.0954   0.8979   0.0110
 -10.000  -0.6379   0.01735   0.01138  -0.0947   0.8897   0.0113
  -9.750  -0.6170   0.01671   0.01065  -0.0940   0.8816   0.0118
  -9.500  -0.5952   0.01615   0.01001  -0.0933   0.8741   0.0124
  -9.250  -0.5726   0.01565   0.00943  -0.0927   0.8673   0.0133
  -9.000  -0.5494   0.01519   0.00888  -0.0922   0.8610   0.0144
  -8.750  -0.5262   0.01472   0.00838  -0.0917   0.8544   0.0159
  -8.500  -0.5021   0.01433   0.00793  -0.0912   0.8488   0.0180
  -8.250  -0.4775   0.01397   0.00756  -0.0909   0.8428   0.0208
  -8.000  -0.4524   0.01366   0.00719  -0.0905   0.8371   0.0234
  -7.750  -0.4270   0.01338   0.00687  -0.0902   0.8318   0.0260
  -7.500  -0.4012   0.01313   0.00655  -0.0900   0.8260   0.0281
  -7.250  -0.3758   0.01283   0.00622  -0.0897   0.8206   0.0303
  -7.000  -0.3498   0.01258   0.00592  -0.0895   0.8155   0.0324
  -6.750  -0.3236   0.01234   0.00564  -0.0893   0.8098   0.0342
  -6.500  -0.2975   0.01209   0.00533  -0.0891   0.8047   0.0361
  -6.250  -0.2712   0.01184   0.00508  -0.0889   0.7996   0.0389
  -6.000  -0.2445   0.01166   0.00486  -0.0888   0.7940   0.0419
  -5.750  -0.2181   0.01143   0.00460  -0.0886   0.7890   0.0454
  -5.500  -0.1914   0.01121   0.00438  -0.0885   0.7840   0.0491
  -5.250  -0.1644   0.01102   0.00414  -0.0884   0.7785   0.0520
  -5.000  -0.1376   0.01080   0.00387  -0.0882   0.7735   0.0554
  -4.750  -0.1107   0.01059   0.00366  -0.0881   0.7685   0.0599
  -4.500  -0.0835   0.01042   0.00346  -0.0880   0.7630   0.0643
  -4.250  -0.0565   0.01023   0.00325  -0.0879   0.7580   0.0714
  -4.000  -0.0291   0.01006   0.00308  -0.0878   0.7528   0.0796
  -3.750  -0.0019   0.00987   0.00292  -0.0878   0.7472   0.0920
  -3.500   0.0250   0.00967   0.00274  -0.0877   0.7420   0.1113
  -3.250   0.0518   0.00941   0.00259  -0.0876   0.7359   0.1419
  -3.000   0.0784   0.00912   0.00244  -0.0876   0.7296   0.1866
  -2.750   0.1052   0.00888   0.00230  -0.0875   0.7239   0.2296
  -2.500   0.1319   0.00858   0.00216  -0.0875   0.7179   0.2828
  -2.250   0.1569   0.00804   0.00200  -0.0873   0.7126   0.3992
  -2.000   0.1835   0.00780   0.00197  -0.0872   0.7073   0.4740
  -1.750   0.2112   0.00772   0.00196  -0.0871   0.7016   0.5066
  -1.500   0.2389   0.00770   0.00193  -0.0871   0.6963   0.5261
  -1.250   0.2668   0.00766   0.00194  -0.0870   0.6906   0.5503
  -1.000   0.2942   0.00764   0.00197  -0.0868   0.6838   0.5787
  -0.750   0.3218   0.00765   0.00198  -0.0867   0.6763   0.5955
  -0.500   0.3495   0.00768   0.00197  -0.0866   0.6675   0.6042
  -0.250   0.3773   0.00770   0.00197  -0.0865   0.6590   0.6121
   0.000   0.4048   0.00775   0.00198  -0.0864   0.6507   0.6201
   0.250   0.4326   0.00777   0.00200  -0.0863   0.6422   0.6296
   0.750   0.4878   0.00786   0.00206  -0.0861   0.6264   0.6477
   1.000   0.5150   0.00791   0.00210  -0.0860   0.6180   0.6537
   1.250   0.5425   0.00796   0.00213  -0.0858   0.6080   0.6596
   1.500   0.5697   0.00802   0.00217  -0.0857   0.5969   0.6649
   1.750   0.5961   0.00811   0.00222  -0.0854   0.5824   0.6703
   2.000   0.6223   0.00821   0.00228  -0.0850   0.5667   0.6764
   2.250   0.6484   0.00832   0.00235  -0.0847   0.5520   0.6822
   2.500   0.6743   0.00844   0.00244  -0.0843   0.5364   0.6884
   2.750   0.6998   0.00859   0.00253  -0.0839   0.5192   0.6947
   3.000   0.7250   0.00874   0.00265  -0.0834   0.5025   0.7006
   3.250   0.7495   0.00894   0.00278  -0.0828   0.4831   0.7075
   3.500   0.7738   0.00914   0.00292  -0.0821   0.4630   0.7140
   3.750   0.7976   0.00937   0.00310  -0.0814   0.4424   0.7208
   4.000   0.8207   0.00964   0.00328  -0.0806   0.4207   0.7278
   4.250   0.8440   0.00988   0.00348  -0.0798   0.4003   0.7350
   4.750   0.8889   0.01045   0.00392  -0.0780   0.3561   0.7500
   5.000   0.9112   0.01075   0.00415  -0.0771   0.3354   0.7583
   5.500   0.9537   0.01138   0.00468  -0.0750   0.2981   0.7752
   5.750   0.9749   0.01167   0.00495  -0.0739   0.2838   0.7844
   6.000   0.9961   0.01195   0.00522  -0.0728   0.2706   0.7939
   6.500   1.0375   0.01249   0.00578  -0.0704   0.2475   0.8168
   6.750   1.0569   0.01276   0.00607  -0.0690   0.2365   0.8307
   7.000   1.0749   0.01303   0.00636  -0.0673   0.2247   0.8489
   7.250   1.0906   0.01322   0.00664  -0.0651   0.2136   0.8803
   7.500   1.1203   0.01352   0.00702  -0.0660   0.2007   1.0000
   7.750   1.1373   0.01392   0.00737  -0.0643   0.1901   1.0000
   8.000   1.1532   0.01438   0.00777  -0.0624   0.1782   1.0000
   8.250   1.1686   0.01487   0.00821  -0.0606   0.1660   1.0000
   8.500   1.1851   0.01533   0.00864  -0.0590   0.1559   1.0000
   8.750   1.2011   0.01581   0.00911  -0.0573   0.1472   1.0000
   9.000   1.2165   0.01635   0.00961  -0.0557   0.1385   1.0000
   9.250   1.2329   0.01685   0.01011  -0.0542   0.1309   1.0000
   9.500   1.2470   0.01748   0.01071  -0.0524   0.1211   1.0000
   9.750   1.2598   0.01820   0.01137  -0.0506   0.1094   1.0000
  10.000   1.2721   0.01896   0.01208  -0.0488   0.0979   1.0000
  10.250   1.2843   0.01977   0.01284  -0.0471   0.0868   1.0000
  10.500   1.2976   0.02052   0.01359  -0.0456   0.0801   1.0000
  10.750   1.3089   0.02143   0.01448  -0.0439   0.0716   1.0000
  11.000   1.3212   0.02230   0.01535  -0.0424   0.0650   1.0000
  11.250   1.3320   0.02329   0.01632  -0.0408   0.0581   1.0000
  11.500   1.3423   0.02435   0.01737  -0.0393   0.0521   1.0000
  11.750   1.3537   0.02535   0.01839  -0.0379   0.0478   1.0000
  12.000   1.3639   0.02647   0.01953  -0.0366   0.0436   1.0000
  12.250   1.3734   0.02767   0.02075  -0.0352   0.0392   1.0000
  12.500   1.3826   0.02892   0.02202  -0.0339   0.0356   1.0000
  12.750   1.3900   0.03034   0.02345  -0.0326   0.0312   1.0000
  13.000   1.3981   0.03175   0.02489  -0.0315   0.0282   1.0000
  13.250   1.4051   0.03328   0.02644  -0.0303   0.0246   1.0000
  13.500   1.4104   0.03499   0.02817  -0.0292   0.0212   1.0000
  13.750   1.4156   0.03677   0.02999  -0.0282   0.0176   1.0000
  14.000   1.4200   0.03868   0.03194  -0.0273   0.0148   1.0000
  14.250   1.4234   0.04074   0.03404  -0.0265   0.0123   1.0000
  14.500   1.4232   0.04323   0.03657  -0.0257   0.0077   1.0000
  14.750   1.4216   0.04597   0.03935  -0.0251   0.0056   1.0000
  15.000   1.4224   0.04857   0.04202  -0.0247   0.0051   1.0000
  15.250   1.4222   0.05135   0.04490  -0.0245   0.0047   1.0000
  15.500   1.4215   0.05432   0.04796  -0.0244   0.0043   1.0000
  15.750   1.4235   0.05705   0.05078  -0.0245   0.0043   1.0000
  16.000   1.4221   0.06027   0.05412  -0.0248   0.0041   1.0000
  16.250   1.4210   0.06357   0.05752  -0.0253   0.0040   1.0000
  16.500   1.4178   0.06726   0.06134  -0.0259   0.0039   1.0000
  16.750   1.4155   0.07092   0.06512  -0.0268   0.0038   1.0000
  17.000   1.4103   0.07513   0.06946  -0.0279   0.0038   1.0000
  17.250   1.4052   0.07943   0.07387  -0.0292   0.0037   1.0000
  17.500   1.3988   0.08405   0.07863  -0.0307   0.0037   1.0000
  17.750   1.3914   0.08897   0.08368  -0.0325   0.0036   1.0000
  18.000   1.3796   0.09472   0.08957  -0.0348   0.0035   1.0000
  18.250   1.3702   0.10020   0.09518  -0.0371   0.0035   1.0000
  18.500   1.3602   0.10594   0.10105  -0.0397   0.0035   1.0000
  18.750   1.3493   0.11191   0.10715  -0.0425   0.0035   1.0000
  19.000   1.3384   0.11799   0.11336  -0.0454   0.0035   1.0000
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