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HQ 2.5/12 AIRFOIL (hq2512-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: HQ 2.5/12 AIRFOIL (hq2512-il)
Reynolds number: 1,000,000
Max Cl/Cd: 92.87 at α=5.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-hq2512-il-1000000-n5.txt
Download as CSV file: xf-hq2512-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: HQ 2.5/12 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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.000  -0.6096   0.12108   0.11925  -0.0269   1.0000   0.0040
 -14.750  -0.9370   0.05048   0.04786  -0.0689   1.0000   0.0032
 -14.500  -0.9570   0.04380   0.04101  -0.0739   1.0000   0.0031
 -14.250  -0.9699   0.03904   0.03609  -0.0769   1.0000   0.0031
 -14.000  -0.9841   0.03478   0.03167  -0.0788   1.0000   0.0031
 -13.750  -0.9895   0.03201   0.02877  -0.0794   1.0000   0.0031
 -13.500  -0.9913   0.02998   0.02664  -0.0789   1.0000   0.0032
 -13.250  -0.9998   0.02819   0.02474  -0.0768   1.0000   0.0032
 -13.000  -1.0030   0.02683   0.02327  -0.0739   1.0000   0.0033
 -12.750  -0.9972   0.02570   0.02205  -0.0718   1.0000   0.0034
 -12.500  -0.9782   0.02447   0.02072  -0.0722   0.9971   0.0035
 -12.250  -0.9559   0.02319   0.01932  -0.0730   0.9899   0.0035
 -12.000  -0.9290   0.02205   0.01806  -0.0745   0.9856   0.0037
 -11.750  -0.9008   0.02104   0.01695  -0.0760   0.9812   0.0038
 -11.500  -0.8727   0.02006   0.01586  -0.0773   0.9755   0.0039
 -11.250  -0.8424   0.01924   0.01492  -0.0789   0.9702   0.0042
 -11.000  -0.8145   0.01849   0.01408  -0.0798   0.9613   0.0044
 -10.750  -0.7877   0.01775   0.01323  -0.0805   0.9511   0.0045
 -10.500  -0.7629   0.01707   0.01244  -0.0806   0.9389   0.0046
 -10.250  -0.7400   0.01641   0.01166  -0.0802   0.9253   0.0047
 -10.000  -0.7192   0.01558   0.01067  -0.0795   0.9128   0.0049
  -9.750  -0.6970   0.01493   0.00991  -0.0788   0.9024   0.0052
  -9.500  -0.6738   0.01439   0.00928  -0.0783   0.8931   0.0054
  -9.250  -0.6500   0.01394   0.00873  -0.0779   0.8844   0.0057
  -9.000  -0.6257   0.01350   0.00821  -0.0775   0.8759   0.0059
  -8.750  -0.6012   0.01308   0.00770  -0.0771   0.8684   0.0061
  -8.500  -0.5762   0.01270   0.00724  -0.0767   0.8608   0.0065
  -8.250  -0.5510   0.01233   0.00680  -0.0764   0.8540   0.0067
  -8.000  -0.5254   0.01199   0.00638  -0.0761   0.8470   0.0069
  -7.750  -0.5002   0.01159   0.00589  -0.0758   0.8407   0.0075
  -7.500  -0.4745   0.01121   0.00547  -0.0756   0.8340   0.0082
  -7.250  -0.4486   0.01091   0.00511  -0.0753   0.8277   0.0088
  -7.000  -0.4221   0.01061   0.00476  -0.0752   0.8214   0.0094
  -6.750  -0.3956   0.01036   0.00444  -0.0750   0.8150   0.0100
  -6.500  -0.3691   0.01005   0.00411  -0.0749   0.8088   0.0118
  -6.250  -0.3424   0.00979   0.00381  -0.0747   0.8022   0.0141
  -6.000  -0.3158   0.00953   0.00356  -0.0746   0.7963   0.0187
  -5.750  -0.2888   0.00931   0.00336  -0.0745   0.7898   0.0239
  -5.500  -0.2614   0.00917   0.00317  -0.0744   0.7839   0.0262
  -5.250  -0.2339   0.00900   0.00297  -0.0744   0.7777   0.0284
  -5.000  -0.2066   0.00883   0.00277  -0.0743   0.7715   0.0315
  -4.750  -0.1790   0.00868   0.00261  -0.0743   0.7656   0.0339
  -4.500  -0.1513   0.00856   0.00245  -0.0743   0.7592   0.0359
  -4.250  -0.1238   0.00840   0.00229  -0.0743   0.7533   0.0416
  -4.000  -0.0960   0.00827   0.00215  -0.0743   0.7468   0.0470
  -3.750  -0.0685   0.00813   0.00200  -0.0743   0.7406   0.0541
  -3.500  -0.0406   0.00801   0.00187  -0.0743   0.7336   0.0612
  -3.250  -0.0131   0.00789   0.00175  -0.0742   0.7263   0.0715
  -3.000   0.0147   0.00775   0.00163  -0.0742   0.7183   0.0848
  -2.750   0.0423   0.00762   0.00152  -0.0742   0.7114   0.1036
  -2.500   0.0699   0.00743   0.00142  -0.0743   0.7048   0.1317
  -2.250   0.0973   0.00724   0.00132  -0.0743   0.6986   0.1721
  -2.000   0.1249   0.00705   0.00123  -0.0743   0.6912   0.2123
  -1.750   0.1521   0.00688   0.00116  -0.0743   0.6830   0.2530
  -1.500   0.1790   0.00659   0.00106  -0.0743   0.6733   0.3256
  -1.250   0.2057   0.00631   0.00100  -0.0743   0.6641   0.4072
  -1.000   0.2325   0.00611   0.00096  -0.0742   0.6545   0.4771
  -0.750   0.2598   0.00598   0.00096  -0.0741   0.6438   0.5298
  -0.500   0.2871   0.00591   0.00099  -0.0740   0.6325   0.5760
  -0.250   0.3148   0.00592   0.00100  -0.0740   0.6221   0.5974
   0.250   0.3707   0.00599   0.00104  -0.0739   0.6010   0.6205
   0.500   0.3986   0.00603   0.00106  -0.0739   0.5891   0.6304
   0.750   0.4261   0.00610   0.00110  -0.0738   0.5736   0.6410
   1.000   0.4534   0.00619   0.00114  -0.0737   0.5575   0.6514
   1.250   0.4806   0.00629   0.00119  -0.0736   0.5402   0.6583
   1.500   0.5077   0.00641   0.00125  -0.0734   0.5195   0.6643
   1.750   0.5345   0.00655   0.00132  -0.0733   0.4986   0.6698
   2.000   0.5611   0.00671   0.00140  -0.0731   0.4756   0.6755
   2.250   0.5872   0.00692   0.00151  -0.0728   0.4473   0.6815
   2.500   0.6126   0.00717   0.00164  -0.0724   0.4149   0.6872
   2.750   0.6382   0.00742   0.00178  -0.0720   0.3849   0.6936
   3.000   0.6640   0.00764   0.00191  -0.0717   0.3587   0.6997
   3.250   0.6892   0.00791   0.00207  -0.0714   0.3291   0.7067
   3.500   0.7144   0.00818   0.00224  -0.0710   0.3013   0.7132
   3.750   0.7400   0.00839   0.00240  -0.0706   0.2831   0.7202
   4.000   0.7659   0.00860   0.00255  -0.0704   0.2682   0.7271
   4.250   0.7914   0.00881   0.00273  -0.0700   0.2521   0.7343
   4.500   0.8169   0.00903   0.00291  -0.0697   0.2362   0.7415
   4.750   0.8423   0.00924   0.00309  -0.0693   0.2215   0.7491
   5.000   0.8679   0.00943   0.00326  -0.0690   0.2109   0.7570
   5.250   0.8934   0.00962   0.00344  -0.0686   0.1993   0.7654
   5.500   0.9174   0.00991   0.00368  -0.0681   0.1800   0.7742
   5.750   0.9419   0.01016   0.00389  -0.0676   0.1664   0.7838
   6.000   0.9658   0.01043   0.00413  -0.0670   0.1513   0.7942
   6.250   0.9888   0.01074   0.00440  -0.0663   0.1337   0.8057
   6.500   1.0104   0.01115   0.00473  -0.0653   0.1125   0.8194
   6.750   1.0331   0.01143   0.00502  -0.0645   0.1013   0.8364
   7.000   1.0538   0.01176   0.00535  -0.0634   0.0850   0.8601
   7.250   1.0746   0.01199   0.00570  -0.0622   0.0699   0.9433
   7.500   1.1012   0.01252   0.00613  -0.0625   0.0534   1.0000
   7.750   1.1218   0.01302   0.00656  -0.0614   0.0404   1.0000
   8.000   1.1407   0.01362   0.00707  -0.0601   0.0257   1.0000
   8.250   1.1538   0.01463   0.00793  -0.0579   0.0049   1.0000
   8.500   1.1740   0.01508   0.00840  -0.0568   0.0037   1.0000
   8.750   1.1945   0.01547   0.00882  -0.0557   0.0035   1.0000
   9.000   1.2141   0.01590   0.00928  -0.0545   0.0032   1.0000
   9.250   1.2316   0.01634   0.00978  -0.0529   0.0030   1.0000
   9.500   1.2479   0.01680   0.01027  -0.0511   0.0029   1.0000
   9.750   1.2627   0.01734   0.01086  -0.0491   0.0027   1.0000
  10.000   1.2772   0.01791   0.01147  -0.0471   0.0026   1.0000
  10.250   1.2912   0.01852   0.01214  -0.0452   0.0024   1.0000
  10.500   1.3037   0.01924   0.01293  -0.0431   0.0023   1.0000
  10.750   1.3157   0.02001   0.01376  -0.0411   0.0022   1.0000
  11.000   1.3286   0.02073   0.01454  -0.0393   0.0022   1.0000
  11.250   1.3412   0.02150   0.01537  -0.0375   0.0022   1.0000
  11.500   1.3539   0.02228   0.01621  -0.0358   0.0021   1.0000
  11.750   1.3649   0.02318   0.01718  -0.0341   0.0020   1.0000
  12.000   1.3749   0.02420   0.01826  -0.0324   0.0020   1.0000
  12.250   1.3843   0.02528   0.01942  -0.0307   0.0019   1.0000
  12.500   1.3928   0.02646   0.02068  -0.0291   0.0019   1.0000
  12.750   1.4002   0.02777   0.02207  -0.0275   0.0019   1.0000
  13.000   1.4065   0.02921   0.02359  -0.0259   0.0019   1.0000
  13.250   1.4131   0.03069   0.02515  -0.0246   0.0017   1.0000
  13.500   1.4173   0.03242   0.02697  -0.0233   0.0017   1.0000
  13.750   1.4212   0.03424   0.02889  -0.0221   0.0017   1.0000
  14.000   1.4248   0.03616   0.03090  -0.0211   0.0016   1.0000
  14.250   1.4257   0.03842   0.03326  -0.0202   0.0016   1.0000
  14.500   1.4257   0.04086   0.03580  -0.0195   0.0016   1.0000
  14.750   1.4254   0.04344   0.03847  -0.0190   0.0015   1.0000
  15.000   1.4219   0.04650   0.04165  -0.0187   0.0016   1.0000
  15.250   1.4194   0.04960   0.04485  -0.0187   0.0015   1.0000
  15.500   1.4157   0.05301   0.04836  -0.0190   0.0014   1.0000
  15.750   1.4093   0.05694   0.05243  -0.0197   0.0015   1.0000
  16.000   1.4022   0.06118   0.05679  -0.0207   0.0015   1.0000
  16.250   1.3945   0.06574   0.06146  -0.0220   0.0014   1.0000
  16.500   1.3824   0.07121   0.06707  -0.0240   0.0014   1.0000
  16.750   1.3728   0.07655   0.07253  -0.0261   0.0014   1.0000
  17.000   1.3571   0.08317   0.07929  -0.0291   0.0014   1.0000
  17.250   1.3441   0.08959   0.08584  -0.0321   0.0014   1.0000
  17.500   1.3241   0.09754   0.09394  -0.0360   0.0014   1.0000
  17.750   1.3097   0.10464   0.10117  -0.0396   0.0014   1.0000
  18.000   1.2927   0.11249   0.10915  -0.0437   0.0014   1.0000
  18.250   1.2732   0.12095   0.11775  -0.0483   0.0014   1.0000
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