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HQ 0/10 AIRFOIL (hq010-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: HQ 0/10 AIRFOIL (hq010-il)
Reynolds number: 500,000
Max Cl/Cd: 56.92 at α=8.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-hq010-il-500000-n5.txt
Download as CSV file: xf-hq010-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: HQ 0/10 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
  ------ -------- --------- --------- -------- -------- --------
 -15.500  -0.8276   0.13902   0.13665   0.0252   1.0000   0.0029
 -15.250  -0.9098   0.11351   0.11102   0.0121   1.0000   0.0026
 -15.000  -0.9716   0.09462   0.09200   0.0021   1.0000   0.0024
 -14.750  -1.0258   0.07753   0.07469  -0.0081   1.0000   0.0023
 -14.500  -1.0569   0.06632   0.06327  -0.0156   1.0000   0.0023
 -14.250  -1.0778   0.05847   0.05524  -0.0208   1.0000   0.0022
 -14.000  -1.0971   0.05191   0.04849  -0.0247   1.0000   0.0022
 -13.750  -1.1120   0.04680   0.04320  -0.0270   1.0000   0.0022
 -13.500  -1.1223   0.04282   0.03904  -0.0282   1.0000   0.0022
 -13.250  -1.1312   0.03938   0.03542  -0.0285   1.0000   0.0023
 -13.000  -1.1386   0.03641   0.03227  -0.0280   1.0000   0.0023
 -12.750  -1.1428   0.03402   0.02972  -0.0269   1.0000   0.0023
 -12.500  -1.1448   0.03203   0.02756  -0.0253   1.0000   0.0023
 -12.250  -1.1453   0.03031   0.02569  -0.0231   1.0000   0.0023
 -12.000  -1.1443   0.02880   0.02401  -0.0204   1.0000   0.0024
 -11.750  -1.1390   0.02736   0.02240  -0.0181   1.0000   0.0025
 -11.500  -1.1281   0.02609   0.02095  -0.0165   1.0000   0.0025
 -11.250  -1.1151   0.02488   0.01959  -0.0150   1.0000   0.0025
 -11.000  -1.1009   0.02367   0.01822  -0.0137   1.0000   0.0027
 -10.750  -1.0846   0.02262   0.01703  -0.0125   1.0000   0.0027
 -10.500  -1.0672   0.02162   0.01588  -0.0114   1.0000   0.0028
 -10.250  -1.0486   0.02069   0.01482  -0.0104   1.0000   0.0030
 -10.000  -1.0292   0.01981   0.01381  -0.0094   1.0000   0.0032
  -9.750  -1.0097   0.01889   0.01279  -0.0085   1.0000   0.0036
  -9.500  -0.9892   0.01809   0.01193  -0.0077   1.0000   0.0042
  -9.250  -0.9680   0.01736   0.01113  -0.0069   1.0000   0.0056
  -9.000  -0.9455   0.01679   0.01055  -0.0063   1.0000   0.0077
  -8.750  -0.9225   0.01629   0.00998  -0.0058   1.0000   0.0090
  -8.500  -0.8993   0.01580   0.00948  -0.0052   1.0000   0.0105
  -8.250  -0.8753   0.01541   0.00906  -0.0048   1.0000   0.0120
  -8.000  -0.8514   0.01500   0.00858  -0.0043   1.0000   0.0130
  -7.750  -0.8269   0.01468   0.00822  -0.0039   1.0000   0.0138
  -7.500  -0.8038   0.01414   0.00768  -0.0033   1.0000   0.0162
  -7.250  -0.7794   0.01380   0.00732  -0.0029   1.0000   0.0182
  -7.000  -0.7546   0.01354   0.00704  -0.0026   1.0000   0.0202
  -6.750  -0.7301   0.01322   0.00668  -0.0021   1.0000   0.0211
  -6.500  -0.7074   0.01266   0.00605  -0.0013   1.0000   0.0229
  -6.250  -0.6829   0.01220   0.00558  -0.0008   0.9986   0.0252
  -6.000  -0.6496   0.01180   0.00516  -0.0023   0.9821   0.0281
  -5.750  -0.6144   0.01147   0.00475  -0.0041   0.9675   0.0309
  -5.500  -0.5810   0.01107   0.00436  -0.0055   0.9510   0.0376
  -5.250  -0.5504   0.01077   0.00404  -0.0062   0.9322   0.0453
  -5.000  -0.5232   0.01048   0.00375  -0.0062   0.9122   0.0567
  -4.750  -0.4979   0.01021   0.00348  -0.0057   0.8937   0.0709
  -4.500  -0.4728   0.00994   0.00320  -0.0052   0.8784   0.0870
  -4.250  -0.4478   0.00964   0.00294  -0.0047   0.8654   0.1110
  -4.000  -0.4239   0.00916   0.00268  -0.0042   0.8533   0.1678
  -3.750  -0.3982   0.00894   0.00250  -0.0038   0.8416   0.2016
  -3.500  -0.3724   0.00870   0.00231  -0.0035   0.8298   0.2278
  -3.000  -0.3211   0.00812   0.00193  -0.0028   0.8069   0.3034
  -2.750  -0.2966   0.00768   0.00175  -0.0024   0.7949   0.3816
  -2.500  -0.2715   0.00735   0.00160  -0.0020   0.7827   0.4447
  -2.250  -0.2459   0.00709   0.00149  -0.0016   0.7723   0.4960
  -2.000  -0.2200   0.00686   0.00141  -0.0012   0.7632   0.5496
  -1.750  -0.1937   0.00671   0.00139  -0.0008   0.7549   0.5967
  -1.500  -0.1664   0.00667   0.00135  -0.0007   0.7462   0.6175
  -1.250  -0.1386   0.00664   0.00131  -0.0006   0.7374   0.6311
  -1.000  -0.1109   0.00662   0.00128  -0.0004   0.7302   0.6445
  -0.750  -0.0830   0.00660   0.00127  -0.0004   0.7225   0.6568
  -0.500  -0.0553   0.00659   0.00125  -0.0003   0.7143   0.6689
  -0.250  -0.0276   0.00658   0.00124  -0.0001   0.7044   0.6801
   0.000   0.0000   0.00658   0.00124   0.0000   0.6920   0.6919
   0.250   0.0276   0.00658   0.00124   0.0001   0.6801   0.7044
   0.500   0.0553   0.00658   0.00125   0.0003   0.6690   0.7143
   0.750   0.0831   0.00660   0.00127   0.0004   0.6568   0.7225
   1.000   0.1110   0.00662   0.00128   0.0004   0.6445   0.7302
   1.250   0.1387   0.00664   0.00131   0.0006   0.6311   0.7374
   1.500   0.1664   0.00667   0.00135   0.0007   0.6175   0.7462
   1.750   0.1938   0.00671   0.00139   0.0008   0.5964   0.7549
   2.000   0.2200   0.00686   0.00141   0.0012   0.5496   0.7631
   2.250   0.2459   0.00709   0.00148   0.0016   0.4956   0.7721
   2.500   0.2715   0.00735   0.00160   0.0020   0.4450   0.7827
   2.750   0.2966   0.00769   0.00175   0.0024   0.3813   0.7949
   3.000   0.3212   0.00812   0.00193   0.0028   0.3036   0.8069
   3.250   0.3466   0.00845   0.00212   0.0032   0.2589   0.8181
   3.500   0.3725   0.00870   0.00231   0.0035   0.2281   0.8298
   3.750   0.3982   0.00894   0.00250   0.0038   0.2017   0.8416
   4.000   0.4239   0.00917   0.00268   0.0042   0.1672   0.8533
   4.250   0.4478   0.00964   0.00294   0.0047   0.1112   0.8654
   4.500   0.4728   0.00995   0.00320   0.0052   0.0867   0.8784
   4.750   0.4979   0.01021   0.00348   0.0057   0.0708   0.8938
   5.250   0.5504   0.01077   0.00404   0.0062   0.0451   0.9322
   5.500   0.5810   0.01107   0.00436   0.0055   0.0376   0.9510
   5.750   0.6145   0.01147   0.00475   0.0041   0.0308   0.9675
   6.000   0.6496   0.01180   0.00516   0.0023   0.0279   0.9823
   6.250   0.6829   0.01220   0.00558   0.0008   0.0251   0.9985
   6.500   0.7073   0.01267   0.00607   0.0013   0.0227   1.0000
   6.750   0.7301   0.01323   0.00669   0.0021   0.0211   1.0000
   7.000   0.7548   0.01351   0.00700   0.0025   0.0200   1.0000
   7.250   0.7795   0.01379   0.00731   0.0029   0.0181   1.0000
   7.500   0.8038   0.01414   0.00767   0.0033   0.0160   1.0000
   7.750   0.8270   0.01467   0.00820   0.0039   0.0138   1.0000
   8.000   0.8513   0.01501   0.00860   0.0043   0.0131   1.0000
   8.250   0.8754   0.01540   0.00905   0.0048   0.0120   1.0000
   8.500   0.8993   0.01580   0.00948   0.0052   0.0105   1.0000
   8.750   0.9225   0.01629   0.00997   0.0058   0.0089   1.0000
   9.000   0.9455   0.01679   0.01055   0.0063   0.0076   1.0000
   9.250   0.9678   0.01738   0.01113   0.0069   0.0053   1.0000
   9.500   0.9893   0.01806   0.01191   0.0077   0.0044   1.0000
   9.750   1.0097   0.01887   0.01277   0.0085   0.0037   1.0000
  10.000   1.0291   0.01980   0.01380   0.0095   0.0032   1.0000
  10.250   1.0485   0.02067   0.01480   0.0104   0.0030   1.0000
  10.500   1.0671   0.02160   0.01586   0.0114   0.0029   1.0000
  10.750   1.0846   0.02259   0.01699   0.0125   0.0027   1.0000
  11.000   1.1007   0.02367   0.01822   0.0137   0.0026   1.0000
  11.250   1.1153   0.02482   0.01952   0.0150   0.0026   1.0000
  11.500   1.1276   0.02611   0.02097   0.0166   0.0025   1.0000
  11.750   1.1383   0.02739   0.02244   0.0182   0.0024   1.0000
  12.000   1.1434   0.02884   0.02405   0.0205   0.0024   1.0000
  12.250   1.1453   0.03029   0.02565   0.0231   0.0023   1.0000
  12.500   1.1450   0.03199   0.02751   0.0253   0.0023   1.0000
  12.750   1.1431   0.03396   0.02966   0.0270   0.0023   1.0000
  13.000   1.1369   0.03656   0.03243   0.0281   0.0022   1.0000
  13.250   1.1331   0.03915   0.03518   0.0285   0.0023   1.0000
  13.500   1.1232   0.04270   0.03892   0.0282   0.0022   1.0000
  13.750   1.1122   0.04678   0.04317   0.0270   0.0022   1.0000
  14.000   1.0991   0.05161   0.04818   0.0248   0.0023   1.0000
  14.250   1.0778   0.05848   0.05525   0.0208   0.0022   1.0000
  14.500   1.0568   0.06640   0.06336   0.0155   0.0023   1.0000
  14.750   1.0248   0.07786   0.07502   0.0078   0.0023   1.0000
  15.000   0.9782   0.09323   0.09060  -0.0014   0.0024   1.0000
  15.250   0.9050   0.11478   0.11230  -0.0129   0.0026   1.0000
  15.500   0.8147   0.14285   0.14049  -0.0271   0.0028   1.0000
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