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HQ 3.0/14 AIRFOIL (hq3014-il) Xfoil prediction polar at RE=100,000 Ncrit=9


Details Polar file
Airfoil: HQ 3.0/14 AIRFOIL (hq3014-il)
Reynolds number: 100,000
Max Cl/Cd: 54.24 at α=6.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-hq3014-il-100000.txt
Download as CSV file: xf-hq3014-il-100000.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 =     0.100 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -10.250  -0.3385   0.10644   0.10159  -0.0452   1.0000   0.1304
 -10.000  -0.3639   0.10384   0.09914  -0.0472   1.0000   0.1341
  -9.750  -0.4024   0.10163   0.09712  -0.0485   1.0000   0.1350
  -9.500  -0.3596   0.09856   0.09398  -0.0427   1.0000   0.1414
  -9.250  -0.3745   0.09687   0.09240  -0.0405   1.0000   0.1456
  -9.000  -0.4119   0.09560   0.09129  -0.0389   1.0000   0.1486
  -8.750  -0.4534   0.09417   0.09002  -0.0374   1.0000   0.1494
  -8.500  -0.4894   0.09232   0.08829  -0.0356   1.0000   0.1496
  -8.250  -0.4496   0.08976   0.08569  -0.0305   1.0000   0.1562
  -8.000  -0.4694   0.08803   0.08404  -0.0281   1.0000   0.1588
  -7.750  -0.6409   0.06293   0.05824  -0.0436   0.9989   0.0790
  -7.500  -0.6218   0.05719   0.05227  -0.0465   0.9941   0.0741
  -7.250  -0.6096   0.05114   0.04572  -0.0496   0.9879   0.0733
  -7.000  -0.5888   0.04561   0.03953  -0.0527   0.9829   0.0736
  -6.750  -0.5698   0.04125   0.03454  -0.0536   0.9772   0.0745
  -6.500  -0.5431   0.03762   0.03010  -0.0553   0.9723   0.0786
  -6.250  -0.5135   0.03599   0.02852  -0.0569   0.9677   0.0853
  -6.000  -0.4870   0.03420   0.02602  -0.0573   0.9618   0.0917
  -5.750  -0.4544   0.03241   0.02427  -0.0593   0.9576   0.0991
  -5.500  -0.4249   0.03144   0.02277  -0.0598   0.9522   0.1055
  -5.250  -0.3972   0.02983   0.02122  -0.0605   0.9470   0.1120
  -5.000  -0.3607   0.02898   0.02007  -0.0622   0.9426   0.1194
  -4.750  -0.3328   0.02786   0.01902  -0.0626   0.9374   0.1257
  -4.500  -0.3043   0.02716   0.01822  -0.0629   0.9315   0.1332
  -4.250  -0.2681   0.02636   0.01753  -0.0647   0.9273   0.1455
  -4.000  -0.2448   0.02578   0.01703  -0.0642   0.9211   0.1581
  -3.750  -0.2160   0.02518   0.01654  -0.0647   0.9153   0.1796
  -3.500  -0.1799   0.02419   0.01603  -0.0667   0.9113   0.2382
  -3.250  -0.1720   0.02273   0.01613  -0.0639   0.9037   0.4919
  -3.000  -0.1445   0.02331   0.01690  -0.0627   0.8980   0.6113
  -2.750  -0.1246   0.02392   0.01749  -0.0605   0.8909   0.6532
  -2.500  -0.1002   0.02444   0.01797  -0.0590   0.8842   0.6846
  -2.250  -0.0704   0.02492   0.01837  -0.0584   0.8787   0.7128
  -2.000  -0.0561   0.02532   0.01875  -0.0555   0.8703   0.7328
  -1.750  -0.0234   0.02564   0.01902  -0.0551   0.8656   0.7598
  -1.500  -0.0170   0.02600   0.01939  -0.0507   0.8563   0.7798
  -1.250   0.0109   0.02614   0.01949  -0.0494   0.8510   0.8060
  -1.000   0.0195   0.02636   0.01971  -0.0457   0.8421   0.8240
  -0.750   0.0487   0.02631   0.01959  -0.0453   0.8364   0.8410
  -0.500   0.0638   0.02643   0.01969  -0.0431   0.8281   0.8564
  -0.250   0.0902   0.02636   0.01957  -0.0423   0.8217   0.8740
   0.000   0.1126   0.02640   0.01959  -0.0413   0.8144   0.8911
   0.250   0.1403   0.02640   0.01954  -0.0413   0.8070   0.9061
   0.500   0.1904   0.02617   0.01924  -0.0448   0.8035   0.9169
   0.750   0.2107   0.02653   0.01960  -0.0446   0.7926   0.9318
   1.000   0.2686   0.02627   0.01928  -0.0496   0.7890   0.9426
   1.250   0.3089   0.02651   0.01951  -0.0527   0.7787   0.9570
   1.500   0.3810   0.02573   0.01868  -0.0596   0.7747   0.9632
   1.750   0.4354   0.02550   0.01843  -0.0646   0.7657   0.9741
   2.000   0.4982   0.02482   0.01773  -0.0703   0.7605   0.9822
   2.250   0.5666   0.02389   0.01677  -0.0766   0.7576   0.9874
   2.500   0.5939   0.02401   0.01691  -0.0777   0.7457   1.0000
   2.750   0.5900   0.02415   0.01703  -0.0732   0.7340   1.0000
   3.000   0.6320   0.02338   0.01623  -0.0750   0.7284   1.0000
   3.250   0.6518   0.02344   0.01626  -0.0741   0.7168   1.0000
   3.500   0.7008   0.02242   0.01523  -0.0766   0.7118   1.0000
   3.750   0.7250   0.02236   0.01516  -0.0760   0.6993   1.0000
   4.000   0.7554   0.02204   0.01483  -0.0760   0.6879   1.0000
   4.250   0.8026   0.02100   0.01376  -0.0780   0.6806   1.0000
   4.500   0.8294   0.02081   0.01357  -0.0775   0.6670   1.0000
   4.750   0.8577   0.02057   0.01334  -0.0771   0.6532   1.0000
   5.000   0.8870   0.02030   0.01306  -0.0768   0.6391   1.0000
   5.250   0.9165   0.02001   0.01276  -0.0765   0.6239   1.0000
   5.500   0.9457   0.01974   0.01248  -0.0762   0.6076   1.0000
   5.750   0.9752   0.01947   0.01216  -0.0758   0.5900   1.0000
   6.000   0.9984   0.01945   0.01212  -0.0746   0.5691   1.0000
   6.250   1.0229   0.01942   0.01205  -0.0736   0.5471   1.0000
   6.500   1.0461   0.01952   0.01207  -0.0724   0.5234   1.0000
   6.750   1.0690   0.01971   0.01214  -0.0713   0.4990   1.0000
   7.000   1.0884   0.02010   0.01244  -0.0697   0.4734   1.0000
   7.250   1.1094   0.02055   0.01275  -0.0684   0.4493   1.0000
   7.500   1.1279   0.02114   0.01324  -0.0668   0.4254   1.0000
   7.750   1.1473   0.02179   0.01375  -0.0655   0.4032   1.0000
   8.000   1.1645   0.02250   0.01440  -0.0639   0.3820   1.0000
   8.250   1.1829   0.02324   0.01504  -0.0625   0.3627   1.0000
   8.500   1.2024   0.02403   0.01569  -0.0613   0.3447   1.0000
   8.750   1.2189   0.02485   0.01648  -0.0597   0.3277   1.0000
   9.000   1.2356   0.02571   0.01730  -0.0582   0.3115   1.0000
   9.250   1.2530   0.02661   0.01816  -0.0569   0.2964   1.0000
   9.500   1.2703   0.02755   0.01907  -0.0555   0.2821   1.0000
   9.750   1.2879   0.02851   0.01996  -0.0543   0.2683   1.0000
  10.000   1.3006   0.02942   0.02092  -0.0523   0.2554   1.0000
  10.250   1.3105   0.03036   0.02195  -0.0500   0.2433   1.0000
  10.500   1.3208   0.03134   0.02297  -0.0477   0.2319   1.0000
  10.750   1.3325   0.03232   0.02394  -0.0458   0.2208   1.0000
  11.000   1.3440   0.03329   0.02489  -0.0438   0.2099   1.0000
  11.250   1.3477   0.03445   0.02621  -0.0410   0.2000   1.0000
  11.500   1.3574   0.03566   0.02745  -0.0391   0.1900   1.0000
  11.750   1.3728   0.03687   0.02852  -0.0379   0.1796   1.0000
  12.000   1.3709   0.03830   0.03021  -0.0348   0.1711   1.0000
  12.250   1.3799   0.03976   0.03169  -0.0332   0.1620   1.0000
  12.500   1.3871   0.04116   0.03311  -0.0314   0.1534   1.0000
  12.750   1.3900   0.04303   0.03516  -0.0294   0.1458   1.0000
  13.000   1.4096   0.04447   0.03639  -0.0290   0.1370   1.0000
  13.250   1.4001   0.04664   0.03894  -0.0261   0.1319   1.0000
  13.500   1.4096   0.04812   0.04037  -0.0250   0.1253   1.0000
  13.750   1.4079   0.05045   0.04290  -0.0233   0.1200   1.0000
  14.000   1.4045   0.05256   0.04519  -0.0216   0.1150   1.0000
  14.250   1.4147   0.05423   0.04674  -0.0209   0.1090   1.0000
  14.500   1.4025   0.05722   0.05010  -0.0193   0.1056   1.0000
  14.750   1.3990   0.05964   0.05265  -0.0184   0.1015   1.0000
  15.000   1.4124   0.06138   0.05426  -0.0180   0.0964   1.0000
  15.250   1.3970   0.06509   0.05833  -0.0172   0.0942   1.0000
  15.500   1.3849   0.06888   0.06239  -0.0168   0.0916   1.0000
  15.750   1.3799   0.07208   0.06574  -0.0167   0.0887   1.0000
  16.000   1.3936   0.07369   0.06719  -0.0165   0.0841   1.0000
  16.250   1.3722   0.07875   0.07260  -0.0171   0.0828   1.0000
  16.500   1.3501   0.08433   0.07850  -0.0183   0.0813   1.0000
  16.750   1.3279   0.09046   0.08490  -0.0201   0.0801   1.0000
  17.000   1.3027   0.09740   0.09211  -0.0228   0.0791   1.0000
  17.250   1.2649   0.10723   0.10225  -0.0274   0.0797   1.0000
  17.500   1.2055   0.12224   0.11755  -0.0357   0.0826   1.0000
  17.750   1.2533   0.11611   0.11125  -0.0318   0.0743   1.0000
  18.000   1.2287   0.12459   0.11988  -0.0365   0.0735   1.0000
  18.250   0.7216   0.20553   0.20136  -0.0839   0.1408   1.0000
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