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HORSTMANN AND QUAST HQ-300 GD(MOD 2) AIRFOIL (hq300gd2-il) Xfoil prediction polar at RE=50,000 Ncrit=5


Details Polar file
Airfoil: HORSTMANN AND QUAST HQ-300 GD(MOD 2) AIRFOIL (hq300gd2-il)
Reynolds number: 50,000
Max Cl/Cd: 15.1 at α=11.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-hq300gd2-il-50000-n5.txt
Download as CSV file: xf-hq300gd2-il-50000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: HORSTMANN AND QUAST HQ-300 GD(MOD 2) AIRFOIL    
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.050 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.500  -0.3028   0.12270   0.11613  -0.0570   1.0000   0.0711
 -11.250  -0.3020   0.12058   0.11411  -0.0550   1.0000   0.0687
 -10.750  -0.3294   0.11138   0.10508  -0.0604   0.9913   0.0602
 -10.500  -0.3189   0.10607   0.09977  -0.0651   0.9833   0.0598
 -10.250  -0.3114   0.10049   0.09418  -0.0702   0.9743   0.0595
 -10.000  -0.3048   0.09443   0.08810  -0.0761   0.9662   0.0591
  -9.750  -0.3015   0.08784   0.08147  -0.0827   0.9575   0.0584
  -9.500  -0.3054   0.08175   0.07533  -0.0886   0.9467   0.0576
  -9.250  -0.3140   0.07624   0.06970  -0.0935   0.9356   0.0568
  -9.000  -0.3247   0.07145   0.06475  -0.0969   0.9241   0.0561
  -8.750  -0.3351   0.06748   0.06057  -0.0984   0.9117   0.0556
  -8.500  -0.3408   0.06369   0.05651  -0.0993   0.9013   0.0551
  -8.250  -0.3396   0.05987   0.05233  -0.1002   0.8931   0.0548
  -8.000  -0.3389   0.05685   0.04897  -0.0996   0.8833   0.0547
  -7.750  -0.3276   0.05357   0.04526  -0.1002   0.8767   0.0551
  -7.500  -0.3194   0.05121   0.04253  -0.0994   0.8682   0.0563
  -7.250  -0.3031   0.04858   0.03940  -0.0995   0.8618   0.0582
  -7.000  -0.2859   0.04624   0.03652  -0.0992   0.8555   0.0595
  -6.750  -0.2677   0.04421   0.03402  -0.0986   0.8484   0.0603
  -6.500  -0.2411   0.04194   0.03146  -0.0991   0.8441   0.0615
  -6.250  -0.2218   0.04062   0.03005  -0.0984   0.8375   0.0638
  -6.000  -0.1985   0.03939   0.02861  -0.0981   0.8317   0.0671
  -5.750  -0.1685   0.03795   0.02682  -0.0983   0.8278   0.0702
  -5.500  -0.1464   0.03705   0.02564  -0.0970   0.8218   0.0721
  -5.250  -0.1240   0.03609   0.02475  -0.0960   0.8162   0.0755
  -5.000  -0.0957   0.03529   0.02384  -0.0956   0.8123   0.0814
  -4.750  -0.0707   0.03470   0.02306  -0.0946   0.8078   0.0862
  -4.500  -0.0554   0.03428   0.02269  -0.0927   0.8011   0.0906
  -4.250  -0.0311   0.03372   0.02197  -0.0921   0.7968   0.0999
  -4.000  -0.0050   0.03285   0.02110  -0.0921   0.7936   0.1125
  -3.750   0.0037   0.03272   0.02106  -0.0900   0.7858   0.1259
  -3.500   0.0240   0.03167   0.02040  -0.0898   0.7812   0.1702
  -3.250   0.0290   0.02987   0.02090  -0.0852   0.7779   0.5264
  -3.000   0.0245   0.03159   0.02299  -0.0762   0.7704   0.6757
  -2.750   0.0374   0.03296   0.02414  -0.0716   0.7655   0.7536
  -2.500   0.0522   0.03416   0.02515  -0.0658   0.7622   0.8057
  -2.250   0.0532   0.03525   0.02617  -0.0591   0.7555   0.8434
  -2.000   0.0733   0.03564   0.02636  -0.0559   0.7510   0.8771
  -1.750   0.1020   0.03553   0.02597  -0.0559   0.7476   0.8915
  -1.500   0.1346   0.03531   0.02549  -0.0568   0.7450   0.9028
  -1.250   0.1350   0.03590   0.02601  -0.0536   0.7365   0.9158
  -1.000   0.1628   0.03586   0.02575  -0.0541   0.7326   0.9267
  -0.750   0.2015   0.03568   0.02535  -0.0564   0.7299   0.9356
  -0.500   0.2156   0.03624   0.02582  -0.0557   0.7229   0.9455
  -0.250   0.2435   0.03643   0.02585  -0.0568   0.7180   0.9534
   0.000   0.2815   0.03640   0.02565  -0.0592   0.7148   0.9595
   0.250   0.3095   0.03675   0.02589  -0.0606   0.7100   0.9656
   0.500   0.3268   0.03745   0.02652  -0.0607   0.7029   0.9727
   0.750   0.3661   0.03755   0.02650  -0.0635   0.6994   0.9765
   1.000   0.4075   0.03749   0.02631  -0.0664   0.6969   0.9800
   1.250   0.4129   0.03889   0.02772  -0.0655   0.6872   0.9874
   1.500   0.4470   0.03906   0.02782  -0.0673   0.6834   0.9915
   1.750   0.4864   0.03896   0.02763  -0.0696   0.6808   0.9949
   2.000   0.4659   0.04066   0.02938  -0.0645   0.6693   1.0000
   2.250   0.4892   0.04065   0.02930  -0.0639   0.6659   1.0000
   2.500   0.4549   0.04213   0.03081  -0.0562   0.6546   1.0000
   2.750   0.4781   0.04224   0.03087  -0.0558   0.6506   1.0000
   3.000   0.4696   0.04358   0.03222  -0.0523   0.6409   1.0000
   3.250   0.4942   0.04389   0.03250  -0.0524   0.6360   1.0000
   3.500   0.5248   0.04400   0.03257  -0.0531   0.6323   1.0000
   3.750   0.5251   0.04560   0.03421  -0.0515   0.6216   1.0000
   4.000   0.5594   0.04561   0.03420  -0.0525   0.6181   1.0000
   4.250   0.5626   0.04734   0.03598  -0.0516   0.6072   1.0000
   4.500   0.5960   0.04742   0.03605  -0.0526   0.6031   1.0000
   4.750   0.6033   0.04909   0.03777  -0.0521   0.5926   1.0000
   5.000   0.6356   0.04922   0.03794  -0.0531   0.5880   1.0000
   5.500   0.6768   0.05102   0.03982  -0.0537   0.5726   1.0000
   6.000   0.7187   0.05280   0.04174  -0.0544   0.5569   1.0000
   6.250   0.7278   0.05460   0.04362  -0.0543   0.5459   1.0000
   6.500   0.7610   0.05454   0.04362  -0.0550   0.5411   1.0000
   6.750   0.7686   0.05650   0.04567  -0.0549   0.5294   1.0000
   7.000   0.8034   0.05623   0.04550  -0.0556   0.5252   1.0000
   7.250   0.8094   0.05837   0.04773  -0.0554   0.5129   1.0000
   7.500   0.8458   0.05784   0.04730  -0.0560   0.5091   1.0000
   8.000   0.8597   0.06209   0.05177  -0.0558   0.4852   1.0000
   8.250   0.8912   0.06186   0.05165  -0.0562   0.4800   1.0000
   8.500   0.8972   0.06413   0.05403  -0.0561   0.4677   1.0000
   8.750   0.9326   0.06336   0.05341  -0.0563   0.4637   1.0000
   9.000   0.9361   0.06593   0.05609  -0.0563   0.4509   1.0000
   9.500   0.9755   0.06752   0.05793  -0.0562   0.4344   1.0000
   9.750   0.9794   0.07016   0.06071  -0.0562   0.4221   1.0000
  10.000   1.0154   0.06886   0.05956  -0.0560   0.4182   1.0000
  10.250   1.0164   0.07186   0.06268  -0.0560   0.4053   1.0000
  10.750   1.0544   0.07330   0.06442  -0.0557   0.3889   1.0000
  11.250   1.0937   0.07444   0.06586  -0.0552   0.3726   1.0000
  11.750   1.1350   0.07519   0.06692  -0.0545   0.3563   1.0000
  12.000   1.1280   0.07930   0.07117  -0.0547   0.3432   1.0000
  12.250   1.1227   0.08334   0.07533  -0.0550   0.3310   1.0000
  12.500   1.1694   0.07987   0.07204  -0.0539   0.3266   1.0000
  12.750   1.1571   0.08486   0.07715  -0.0543   0.3138   1.0000
  13.250   1.1981   0.08528   0.07789  -0.0534   0.2967   1.0000
  13.500   1.1799   0.09135   0.08409  -0.0543   0.2842   1.0000
  13.750   1.1785   0.09493   0.08779  -0.0548   0.2738   1.0000
  14.000   1.2215   0.09137   0.08439  -0.0532   0.2664   1.0000
  14.250   1.1960   0.09881   0.09195  -0.0548   0.2544   1.0000
  14.500   1.1957   0.10226   0.09552  -0.0554   0.2442   1.0000
  14.750   1.2517   0.09609   0.08946  -0.0528   0.2351   1.0000
  15.000   1.2121   0.10611   0.09964  -0.0558   0.2240   1.0000
  15.250   1.2007   0.11158   0.10523  -0.0574   0.2135   1.0000
  15.500   1.2251   0.11040   0.10414  -0.0565   0.2028   1.0000
  15.750   1.2446   0.11004   0.10380  -0.0560   0.1907   1.0000
  16.000   1.2182   0.11847   0.11241  -0.0592   0.1809   1.0000
  16.250   1.2118   0.12324   0.11727  -0.0611   0.1704   1.0000
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