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HQ 2.0/12 AIRFOIL (hq2012-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: HQ 2.0/12 AIRFOIL (hq2012-il)
Reynolds number: 500,000
Max Cl/Cd: 79.48 at α=6.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-hq2012-il-500000-n5.txt
Download as CSV file: xf-hq2012-il-500000-n5.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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.500  -0.7488   0.08808   0.08530  -0.0382   1.0000   0.0064
 -14.250  -0.7987   0.07340   0.07046  -0.0469   1.0000   0.0063
 -14.000  -0.8323   0.06208   0.05897  -0.0545   1.0000   0.0061
 -13.750  -0.8532   0.05416   0.05087  -0.0603   1.0000   0.0061
 -13.500  -0.8681   0.04832   0.04486  -0.0643   1.0000   0.0062
 -13.250  -0.8821   0.04333   0.03969  -0.0672   1.0000   0.0062
 -13.000  -0.8908   0.03951   0.03569  -0.0689   1.0000   0.0063
 -12.750  -0.9020   0.03592   0.03195  -0.0697   1.0000   0.0062
 -12.500  -0.9028   0.03368   0.02956  -0.0697   1.0000   0.0063
 -12.250  -0.9083   0.03141   0.02713  -0.0688   1.0000   0.0064
 -12.000  -0.9096   0.02991   0.02550  -0.0669   1.0000   0.0065
 -11.750  -0.9126   0.02845   0.02390  -0.0639   1.0000   0.0065
 -11.500  -0.9117   0.02680   0.02210  -0.0615   1.0000   0.0066
 -11.250  -0.9077   0.02533   0.02051  -0.0591   1.0000   0.0068
 -11.000  -0.8991   0.02422   0.01930  -0.0570   1.0000   0.0070
 -10.750  -0.8778   0.02305   0.01802  -0.0573   0.9955   0.0072
 -10.500  -0.8509   0.02198   0.01683  -0.0585   0.9884   0.0075
 -10.250  -0.8211   0.02091   0.01565  -0.0601   0.9833   0.0078
 -10.000  -0.7926   0.02002   0.01464  -0.0612   0.9760   0.0082
  -9.750  -0.7618   0.01916   0.01365  -0.0627   0.9699   0.0086
  -9.500  -0.7329   0.01834   0.01269  -0.0637   0.9608   0.0090
  -9.250  -0.7046   0.01738   0.01161  -0.0647   0.9514   0.0094
  -9.000  -0.6766   0.01652   0.01066  -0.0654   0.9412   0.0099
  -8.750  -0.6500   0.01589   0.00994  -0.0657   0.9295   0.0104
  -8.500  -0.6244   0.01532   0.00927  -0.0656   0.9185   0.0110
  -8.250  -0.5995   0.01480   0.00863  -0.0653   0.9086   0.0115
  -8.000  -0.5748   0.01434   0.00806  -0.0649   0.8994   0.0123
  -7.750  -0.5511   0.01381   0.00746  -0.0644   0.8904   0.0134
  -7.500  -0.5264   0.01340   0.00700  -0.0640   0.8827   0.0148
  -7.250  -0.5016   0.01302   0.00654  -0.0635   0.8749   0.0165
  -7.000  -0.4767   0.01263   0.00610  -0.0631   0.8680   0.0187
  -6.750  -0.4511   0.01232   0.00574  -0.0628   0.8610   0.0218
  -6.500  -0.4256   0.01200   0.00539  -0.0625   0.8547   0.0252
  -6.250  -0.3994   0.01175   0.00509  -0.0622   0.8482   0.0287
  -6.000  -0.3735   0.01147   0.00478  -0.0619   0.8419   0.0325
  -5.750  -0.3472   0.01123   0.00452  -0.0617   0.8360   0.0366
  -5.500  -0.3207   0.01100   0.00423  -0.0615   0.8295   0.0402
  -5.250  -0.2944   0.01076   0.00398  -0.0613   0.8238   0.0458
  -5.000  -0.2676   0.01054   0.00374  -0.0611   0.8174   0.0512
  -4.750  -0.2411   0.01030   0.00350  -0.0609   0.8114   0.0596
  -4.500  -0.2144   0.01007   0.00327  -0.0608   0.8052   0.0691
  -4.250  -0.1875   0.00986   0.00306  -0.0606   0.7989   0.0796
  -4.000  -0.1607   0.00963   0.00285  -0.0605   0.7930   0.0944
  -3.750  -0.1338   0.00940   0.00267  -0.0604   0.7865   0.1151
  -3.500  -0.1073   0.00915   0.00248  -0.0602   0.7805   0.1450
  -3.250  -0.0806   0.00887   0.00232  -0.0601   0.7738   0.1804
  -3.000  -0.0538   0.00864   0.00217  -0.0600   0.7674   0.2156
  -2.750  -0.0270   0.00838   0.00202  -0.0599   0.7607   0.2569
  -2.500  -0.0015   0.00795   0.00184  -0.0597   0.7536   0.3353
  -2.250   0.0236   0.00748   0.00172  -0.0595   0.7462   0.4451
  -2.000   0.0504   0.00732   0.00166  -0.0592   0.7387   0.4925
  -1.750   0.0775   0.00720   0.00163  -0.0591   0.7305   0.5314
  -1.500   0.1045   0.00714   0.00161  -0.0588   0.7212   0.5632
  -1.250   0.1320   0.00712   0.00159  -0.0586   0.7105   0.5854
  -1.000   0.1595   0.00711   0.00158  -0.0585   0.7013   0.6040
  -0.500   0.2149   0.00712   0.00157  -0.0582   0.6833   0.6335
  -0.250   0.2426   0.00714   0.00157  -0.0581   0.6746   0.6446
   0.000   0.2701   0.00716   0.00158  -0.0579   0.6648   0.6564
   0.250   0.2976   0.00718   0.00160  -0.0578   0.6539   0.6693
   0.500   0.3252   0.00722   0.00162  -0.0576   0.6434   0.6786
   0.750   0.3527   0.00727   0.00164  -0.0575   0.6315   0.6846
   1.000   0.3803   0.00733   0.00166  -0.0574   0.6199   0.6912
   1.250   0.4078   0.00737   0.00169  -0.0573   0.6080   0.6973
   1.500   0.4353   0.00742   0.00173  -0.0571   0.5963   0.7039
   1.750   0.4626   0.00749   0.00178  -0.0570   0.5827   0.7101
   2.000   0.4894   0.00758   0.00184  -0.0567   0.5659   0.7170
   2.250   0.5160   0.00769   0.00190  -0.0565   0.5475   0.7239
   2.500   0.5425   0.00781   0.00199  -0.0562   0.5283   0.7309
   2.750   0.5684   0.00797   0.00209  -0.0558   0.5038   0.7383
   3.000   0.5937   0.00817   0.00221  -0.0553   0.4760   0.7457
   3.250   0.6187   0.00840   0.00235  -0.0548   0.4467   0.7533
   3.500   0.6431   0.00867   0.00252  -0.0542   0.4148   0.7613
   3.750   0.6673   0.00897   0.00271  -0.0536   0.3805   0.7693
   4.000   0.6906   0.00933   0.00293  -0.0529   0.3409   0.7781
   4.250   0.7140   0.00968   0.00316  -0.0522   0.3062   0.7869
   4.500   0.7377   0.01000   0.00340  -0.0516   0.2814   0.7967
   4.750   0.7613   0.01031   0.00364  -0.0509   0.2595   0.8073
   5.000   0.7848   0.01059   0.00389  -0.0502   0.2408   0.8186
   5.250   0.8090   0.01081   0.00412  -0.0496   0.2272   0.8316
   5.500   0.8333   0.01097   0.00433  -0.0490   0.2175   0.8469
   5.750   0.8568   0.01114   0.00455  -0.0482   0.2077   0.8664
   6.000   0.8796   0.01130   0.00478  -0.0472   0.1951   0.9015
   6.250   0.9188   0.01156   0.00508  -0.0500   0.1775   1.0000
   6.500   0.9425   0.01189   0.00536  -0.0494   0.1623   1.0000
   6.750   0.9655   0.01227   0.00566  -0.0487   0.1442   1.0000
   7.000   0.9867   0.01278   0.00604  -0.0478   0.1205   1.0000
   7.250   1.0069   0.01336   0.00649  -0.0468   0.0976   1.0000
   7.500   1.0270   0.01393   0.00696  -0.0457   0.0782   1.0000
   7.750   1.0469   0.01450   0.00743  -0.0447   0.0635   1.0000
   8.000   1.0680   0.01496   0.00786  -0.0437   0.0554   1.0000
   8.250   1.0886   0.01543   0.00832  -0.0427   0.0491   1.0000
   8.500   1.1090   0.01589   0.00879  -0.0417   0.0437   1.0000
   8.750   1.1288   0.01638   0.00927  -0.0406   0.0395   1.0000
   9.000   1.1488   0.01682   0.00973  -0.0395   0.0364   1.0000
   9.250   1.1671   0.01735   0.01025  -0.0382   0.0325   1.0000
   9.500   1.1846   0.01783   0.01076  -0.0367   0.0300   1.0000
   9.750   1.2014   0.01828   0.01126  -0.0351   0.0280   1.0000
  10.000   1.2172   0.01879   0.01182  -0.0334   0.0259   1.0000
  10.250   1.2315   0.01941   0.01243  -0.0315   0.0232   1.0000
  10.500   1.2468   0.01996   0.01304  -0.0299   0.0215   1.0000
  10.750   1.2600   0.02067   0.01374  -0.0281   0.0177   1.0000
  11.000   1.2720   0.02147   0.01454  -0.0262   0.0138   1.0000
  11.250   1.2839   0.02229   0.01540  -0.0244   0.0113   1.0000
  11.500   1.2907   0.02349   0.01658  -0.0222   0.0062   1.0000
  11.750   1.2997   0.02457   0.01771  -0.0204   0.0053   1.0000
  12.000   1.3075   0.02579   0.01901  -0.0186   0.0045   1.0000
  12.250   1.3165   0.02696   0.02026  -0.0170   0.0042   1.0000
  12.500   1.3248   0.02822   0.02161  -0.0155   0.0040   1.0000
  12.750   1.3325   0.02956   0.02305  -0.0142   0.0039   1.0000
  13.000   1.3388   0.03108   0.02466  -0.0128   0.0037   1.0000
  13.250   1.3436   0.03278   0.02647  -0.0115   0.0035   1.0000
  13.500   1.3489   0.03449   0.02828  -0.0105   0.0034   1.0000
  13.750   1.3518   0.03649   0.03040  -0.0095   0.0033   1.0000
  14.000   1.3540   0.03862   0.03265  -0.0087   0.0032   1.0000
  14.250   1.3566   0.04080   0.03494  -0.0081   0.0032   1.0000
  14.500   1.3539   0.04364   0.03791  -0.0076   0.0031   1.0000
  14.750   1.3547   0.04620   0.04060  -0.0074   0.0031   1.0000
  15.000   1.3524   0.04922   0.04376  -0.0075   0.0031   1.0000
  15.250   1.3488   0.05255   0.04722  -0.0078   0.0030   1.0000
  15.500   1.3455   0.05601   0.05081  -0.0084   0.0030   1.0000
  15.750   1.3400   0.05996   0.05489  -0.0094   0.0030   1.0000
  16.000   1.3322   0.06442   0.05950  -0.0108   0.0030   1.0000
  16.250   1.3249   0.06904   0.06425  -0.0125   0.0030   1.0000
  16.500   1.3140   0.07449   0.06985  -0.0147   0.0029   1.0000
  16.750   1.3010   0.08052   0.07604  -0.0174   0.0029   1.0000
  17.000   1.2879   0.08684   0.08251  -0.0205   0.0029   1.0000
  17.250   1.2722   0.09390   0.08972  -0.0241   0.0029   1.0000
  17.500   1.2540   0.10165   0.09763  -0.0281   0.0029   1.0000
  17.750   1.2354   0.10974   0.10587  -0.0324   0.0029   1.0000
  18.000   1.2178   0.11777   0.11404  -0.0368   0.0029   1.0000
  18.250   1.1986   0.12622   0.12262  -0.0415   0.0030   1.0000
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