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HQ 2.0/12 AIRFOIL (hq2012-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: HQ 2.0/12 AIRFOIL (hq2012-il)
Reynolds number: 1,000,000
Max Cl/Cd: 100.85 at α=6.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-hq2012-il-1000000.txt
Download as CSV file: xf-hq2012-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: HQ 2.0/12 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
  ------ -------- --------- --------- -------- -------- --------
 -14.750  -0.8056   0.08140   0.07925  -0.0410   1.0000   0.0067
 -14.500  -0.8380   0.07012   0.06781  -0.0481   1.0000   0.0066
 -14.250  -0.8597   0.06106   0.05857  -0.0544   1.0000   0.0065
 -14.000  -0.8652   0.05585   0.05327  -0.0583   1.0000   0.0064
 -13.750  -0.8943   0.04754   0.04474  -0.0643   1.0000   0.0065
 -13.500  -0.9149   0.04157   0.03859  -0.0680   1.0000   0.0066
 -13.250  -0.9215   0.03797   0.03485  -0.0696   1.0000   0.0065
 -13.000  -0.9216   0.03543   0.03220  -0.0704   1.0000   0.0065
 -12.750  -0.9410   0.03139   0.02796  -0.0707   1.0000   0.0067
 -12.500  -0.9463   0.02929   0.02575  -0.0696   1.0000   0.0068
 -12.250  -0.9540   0.02762   0.02394  -0.0666   1.0000   0.0067
 -12.000  -0.9558   0.02609   0.02229  -0.0636   1.0000   0.0068
 -11.750  -0.9483   0.02500   0.02111  -0.0616   1.0000   0.0069
 -11.500  -0.9411   0.02374   0.01974  -0.0594   1.0000   0.0070
 -11.250  -0.9300   0.02292   0.01885  -0.0574   1.0000   0.0072
 -11.000  -0.9215   0.02198   0.01782  -0.0549   1.0000   0.0073
 -10.750  -0.8969   0.02102   0.01678  -0.0555   0.9983   0.0075
 -10.500  -0.8665   0.01981   0.01542  -0.0573   0.9948   0.0077
 -10.250  -0.8371   0.01877   0.01427  -0.0587   0.9901   0.0080
 -10.000  -0.8064   0.01778   0.01316  -0.0601   0.9859   0.0083
  -9.750  -0.7736   0.01684   0.01211  -0.0620   0.9830   0.0085
  -9.500  -0.7424   0.01621   0.01140  -0.0632   0.9768   0.0087
  -9.250  -0.7125   0.01483   0.00986  -0.0647   0.9703   0.0092
  -9.000  -0.6843   0.01397   0.00892  -0.0655   0.9602   0.0098
  -8.750  -0.6559   0.01348   0.00838  -0.0660   0.9493   0.0104
  -8.500  -0.6300   0.01302   0.00784  -0.0658   0.9368   0.0109
  -8.250  -0.6053   0.01262   0.00735  -0.0653   0.9248   0.0115
  -8.000  -0.5806   0.01227   0.00691  -0.0648   0.9139   0.0119
  -7.750  -0.5583   0.01157   0.00609  -0.0640   0.9039   0.0130
  -7.500  -0.5336   0.01121   0.00567  -0.0635   0.8956   0.0141
  -7.250  -0.5081   0.01091   0.00532  -0.0631   0.8876   0.0153
  -7.000  -0.4834   0.01050   0.00486  -0.0626   0.8803   0.0178
  -6.750  -0.4572   0.01025   0.00459  -0.0623   0.8732   0.0204
  -6.250  -0.4053   0.00968   0.00401  -0.0618   0.8601   0.0303
  -6.000  -0.3785   0.00953   0.00382  -0.0616   0.8538   0.0338
  -5.750  -0.3519   0.00929   0.00356  -0.0614   0.8478   0.0379
  -5.500  -0.3251   0.00909   0.00335  -0.0612   0.8415   0.0420
  -5.250  -0.2979   0.00896   0.00317  -0.0611   0.8357   0.0451
  -5.000  -0.2711   0.00870   0.00294  -0.0609   0.8294   0.0521
  -4.750  -0.2440   0.00854   0.00274  -0.0608   0.8234   0.0581
  -4.500  -0.2168   0.00833   0.00255  -0.0607   0.8173   0.0680
  -4.250  -0.1901   0.00807   0.00236  -0.0605   0.8109   0.0869
  -4.000  -0.1633   0.00782   0.00218  -0.0604   0.8049   0.1115
  -3.750  -0.1365   0.00754   0.00201  -0.0603   0.7981   0.1447
  -3.500  -0.1098   0.00729   0.00185  -0.0601   0.7918   0.1833
  -3.250  -0.0830   0.00699   0.00171  -0.0600   0.7845   0.2294
  -3.000  -0.0567   0.00670   0.00156  -0.0599   0.7774   0.2855
  -2.750  -0.0311   0.00620   0.00139  -0.0597   0.7700   0.3829
  -2.500  -0.0049   0.00591   0.00130  -0.0595   0.7628   0.4592
  -2.250   0.0224   0.00574   0.00124  -0.0594   0.7543   0.5052
  -2.000   0.0497   0.00564   0.00120  -0.0592   0.7460   0.5417
  -1.750   0.0777   0.00558   0.00118  -0.0591   0.7380   0.5684
  -1.500   0.1056   0.00556   0.00116  -0.0591   0.7306   0.5864
  -1.250   0.1337   0.00554   0.00114  -0.0590   0.7222   0.6014
  -1.000   0.1618   0.00553   0.00114  -0.0590   0.7151   0.6183
  -0.750   0.1900   0.00553   0.00114  -0.0590   0.7072   0.6309
  -0.500   0.2182   0.00555   0.00113  -0.0590   0.6990   0.6429
  -0.250   0.2461   0.00557   0.00114  -0.0589   0.6901   0.6541
   0.000   0.2743   0.00557   0.00115  -0.0589   0.6814   0.6637
   0.500   0.3304   0.00562   0.00118  -0.0588   0.6642   0.6816
   0.750   0.3583   0.00565   0.00121  -0.0587   0.6555   0.6919
   1.000   0.3863   0.00570   0.00124  -0.0587   0.6465   0.7016
   1.250   0.4144   0.00571   0.00127  -0.0587   0.6375   0.7083
   1.500   0.4423   0.00577   0.00130  -0.0586   0.6272   0.7151
   2.000   0.4977   0.00587   0.00138  -0.0585   0.6027   0.7280
   2.250   0.5253   0.00593   0.00142  -0.0584   0.5888   0.7346
   2.500   0.5523   0.00602   0.00149  -0.0582   0.5719   0.7417
   2.750   0.5795   0.00612   0.00155  -0.0580   0.5530   0.7489
   3.000   0.6058   0.00626   0.00163  -0.0577   0.5290   0.7563
   3.250   0.6316   0.00646   0.00173  -0.0573   0.4983   0.7641
   3.500   0.6567   0.00669   0.00187  -0.0569   0.4621   0.7724
   3.750   0.6812   0.00699   0.00203  -0.0563   0.4239   0.7808
   4.000   0.7051   0.00733   0.00221  -0.0557   0.3806   0.7902
   4.250   0.7276   0.00777   0.00245  -0.0548   0.3244   0.7997
   4.500   0.7508   0.00816   0.00267  -0.0541   0.2849   0.8103
   5.000   0.8009   0.00856   0.00304  -0.0532   0.2542   0.8350
   5.250   0.8259   0.00871   0.00322  -0.0527   0.2433   0.8503
   5.500   0.8500   0.00885   0.00340  -0.0520   0.2326   0.8705
   5.750   0.8730   0.00890   0.00357  -0.0509   0.2222   0.9116
   6.000   0.9135   0.00908   0.00380  -0.0539   0.2080   1.0000
   6.250   0.9389   0.00931   0.00399  -0.0536   0.1967   1.0000
   6.500   0.9635   0.00958   0.00420  -0.0531   0.1815   1.0000
   6.750   0.9869   0.00995   0.00445  -0.0525   0.1605   1.0000
   7.000   1.0090   0.01041   0.00477  -0.0517   0.1343   1.0000
   7.250   1.0302   0.01093   0.00515  -0.0507   0.1088   1.0000
   7.500   1.0514   0.01143   0.00554  -0.0498   0.0880   1.0000
   7.750   1.0724   0.01195   0.00595  -0.0488   0.0716   1.0000
   8.000   1.0939   0.01241   0.00634  -0.0479   0.0602   1.0000
   8.250   1.1159   0.01281   0.00672  -0.0470   0.0526   1.0000
   8.500   1.1371   0.01327   0.00714  -0.0461   0.0459   1.0000
   8.750   1.1596   0.01360   0.00748  -0.0453   0.0431   1.0000
   9.000   1.1804   0.01403   0.00790  -0.0443   0.0394   1.0000
   9.250   1.2012   0.01445   0.00832  -0.0433   0.0359   1.0000
   9.500   1.2227   0.01479   0.00870  -0.0424   0.0342   1.0000
   9.750   1.2428   0.01520   0.00912  -0.0413   0.0320   1.0000
  10.000   1.2610   0.01571   0.00961  -0.0399   0.0288   1.0000
  10.250   1.2805   0.01605   0.00999  -0.0387   0.0271   1.0000
  10.500   1.2977   0.01644   0.01040  -0.0371   0.0252   1.0000
  10.750   1.3122   0.01696   0.01090  -0.0351   0.0224   1.0000
  11.000   1.3269   0.01746   0.01140  -0.0332   0.0187   1.0000
  11.250   1.3391   0.01813   0.01204  -0.0310   0.0144   1.0000
  11.500   1.3486   0.01897   0.01285  -0.0286   0.0094   1.0000
  11.750   1.3560   0.01998   0.01386  -0.0260   0.0062   1.0000
  12.000   1.3668   0.02081   0.01473  -0.0240   0.0056   1.0000
  12.250   1.3764   0.02175   0.01573  -0.0220   0.0051   1.0000
  12.500   1.3870   0.02266   0.01670  -0.0202   0.0049   1.0000
  12.750   1.3948   0.02380   0.01793  -0.0183   0.0045   1.0000
  13.000   1.4040   0.02488   0.01909  -0.0167   0.0044   1.0000
  13.250   1.4122   0.02607   0.02036  -0.0151   0.0043   1.0000
  13.500   1.4203   0.02731   0.02168  -0.0136   0.0042   1.0000
  13.750   1.4267   0.02872   0.02318  -0.0121   0.0041   1.0000
  14.000   1.4328   0.03022   0.02477  -0.0108   0.0041   1.0000
  14.250   1.4367   0.03196   0.02660  -0.0096   0.0040   1.0000
  14.500   1.4397   0.03385   0.02858  -0.0084   0.0039   1.0000
  14.750   1.4416   0.03592   0.03075  -0.0075   0.0038   1.0000
  15.000   1.4418   0.03823   0.03317  -0.0067   0.0038   1.0000
  15.250   1.4419   0.04065   0.03569  -0.0061   0.0037   1.0000
  15.500   1.4408   0.04331   0.03846  -0.0058   0.0037   1.0000
  15.750   1.4368   0.04640   0.04166  -0.0057   0.0036   1.0000
  16.000   1.4340   0.04954   0.04491  -0.0059   0.0036   1.0000
  16.250   1.4227   0.05389   0.04939  -0.0065   0.0035   1.0000
  16.500   1.4133   0.05828   0.05391  -0.0076   0.0034   1.0000
  16.750   1.4049   0.06277   0.05851  -0.0090   0.0034   1.0000
  17.000   1.3979   0.06726   0.06312  -0.0105   0.0035   1.0000
  17.250   1.3853   0.07285   0.06885  -0.0128   0.0035   1.0000
  17.500   1.3591   0.08104   0.07721  -0.0166   0.0033   1.0000
  17.750   1.3466   0.08719   0.08348  -0.0195   0.0034   1.0000
  18.000   1.3292   0.09447   0.09091  -0.0232   0.0034   1.0000
  18.250   1.3108   0.10218   0.09876  -0.0272   0.0034   1.0000
  18.500   1.2924   0.11008   0.10679  -0.0314   0.0034   1.0000
  18.750   1.2754   0.11785   0.11469  -0.0356   0.0034   1.0000
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