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HQ 1.0/12 AIRFOIL (hq1012-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: HQ 1.0/12 AIRFOIL (hq1012-il)
Reynolds number: 500,000
Max Cl/Cd: 69.65 at α=6.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-hq1012-il-500000-n5.txt
Download as CSV file: xf-hq1012-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: HQ 1.0/12 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
  ------ -------- --------- --------- -------- -------- --------
 -16.500  -0.7993   0.12761   0.12497  -0.0038   1.0000   0.0060
 -16.250  -0.8508   0.11137   0.10856  -0.0123   1.0000   0.0058
 -16.000  -0.8967   0.09745   0.09445  -0.0199   1.0000   0.0056
 -15.750  -0.9337   0.08570   0.08253  -0.0266   1.0000   0.0055
 -15.500  -0.9620   0.07585   0.07249  -0.0323   1.0000   0.0054
 -15.250  -0.9877   0.06686   0.06333  -0.0380   1.0000   0.0055
 -15.000  -1.0066   0.05974   0.05604  -0.0424   1.0000   0.0054
 -14.750  -1.0230   0.05363   0.04977  -0.0460   1.0000   0.0054
 -14.500  -1.0359   0.04857   0.04456  -0.0487   1.0000   0.0054
 -14.250  -1.0425   0.04471   0.04058  -0.0504   1.0000   0.0056
 -14.000  -1.0476   0.04132   0.03705  -0.0515   1.0000   0.0056
 -13.750  -1.0513   0.03832   0.03392  -0.0522   1.0000   0.0057
 -13.500  -1.0553   0.03549   0.03095  -0.0524   1.0000   0.0058
 -13.250  -1.0535   0.03342   0.02877  -0.0522   1.0000   0.0058
 -13.000  -1.0525   0.03140   0.02664  -0.0515   1.0000   0.0059
 -12.750  -1.0485   0.02980   0.02493  -0.0506   1.0000   0.0061
 -12.500  -1.0436   0.02840   0.02343  -0.0494   1.0000   0.0064
 -12.250  -1.0390   0.02711   0.02203  -0.0477   1.0000   0.0065
 -12.000  -1.0344   0.02596   0.02078  -0.0455   1.0000   0.0067
 -11.750  -1.0284   0.02493   0.01963  -0.0430   1.0000   0.0069
 -11.500  -1.0166   0.02399   0.01859  -0.0414   1.0000   0.0071
 -11.250  -1.0023   0.02316   0.01762  -0.0400   1.0000   0.0074
 -11.000  -0.9916   0.02196   0.01633  -0.0381   1.0000   0.0077
 -10.750  -0.9771   0.02103   0.01532  -0.0367   1.0000   0.0080
 -10.500  -0.9606   0.02024   0.01446  -0.0353   1.0000   0.0084
 -10.250  -0.9432   0.01952   0.01367  -0.0341   1.0000   0.0088
 -10.000  -0.9255   0.01883   0.01291  -0.0328   1.0000   0.0092
  -9.750  -0.9076   0.01819   0.01219  -0.0314   1.0000   0.0096
  -9.500  -0.8896   0.01758   0.01151  -0.0300   1.0000   0.0101
  -9.250  -0.8680   0.01687   0.01072  -0.0294   0.9973   0.0108
  -9.000  -0.8373   0.01617   0.00997  -0.0307   0.9890   0.0120
  -8.750  -0.8052   0.01558   0.00933  -0.0321   0.9809   0.0134
  -8.500  -0.7732   0.01495   0.00865  -0.0335   0.9716   0.0151
  -8.250  -0.7415   0.01440   0.00808  -0.0348   0.9607   0.0174
  -8.000  -0.7101   0.01390   0.00753  -0.0359   0.9479   0.0203
  -7.750  -0.6802   0.01350   0.00709  -0.0367   0.9330   0.0242
  -7.500  -0.6526   0.01311   0.00666  -0.0369   0.9178   0.0278
  -7.250  -0.6268   0.01280   0.00630  -0.0366   0.9038   0.0315
  -7.000  -0.6014   0.01254   0.00595  -0.0362   0.8912   0.0340
  -6.750  -0.5769   0.01222   0.00559  -0.0357   0.8796   0.0380
  -6.500  -0.5517   0.01198   0.00528  -0.0353   0.8689   0.0418
  -6.250  -0.5264   0.01171   0.00497  -0.0348   0.8588   0.0461
  -6.000  -0.5011   0.01145   0.00468  -0.0345   0.8499   0.0521
  -5.750  -0.4755   0.01121   0.00440  -0.0341   0.8413   0.0580
  -5.500  -0.4498   0.01095   0.00412  -0.0338   0.8328   0.0653
  -5.250  -0.4241   0.01071   0.00385  -0.0334   0.8251   0.0739
  -5.000  -0.3979   0.01046   0.00361  -0.0332   0.8171   0.0840
  -4.750  -0.3719   0.01023   0.00337  -0.0329   0.8099   0.0969
  -4.500  -0.3458   0.00996   0.00314  -0.0327   0.8023   0.1143
  -4.250  -0.3198   0.00970   0.00292  -0.0324   0.7954   0.1371
  -4.000  -0.2938   0.00940   0.00272  -0.0322   0.7881   0.1673
  -3.500  -0.2414   0.00887   0.00237  -0.0318   0.7744   0.2349
  -3.250  -0.2155   0.00856   0.00218  -0.0316   0.7677   0.2753
  -3.000  -0.1898   0.00821   0.00201  -0.0314   0.7608   0.3271
  -2.750  -0.1644   0.00785   0.00185  -0.0310   0.7537   0.3952
  -2.500  -0.1383   0.00758   0.00175  -0.0308   0.7467   0.4472
  -2.250  -0.1119   0.00739   0.00167  -0.0305   0.7394   0.4930
  -2.000  -0.0852   0.00723   0.00163  -0.0303   0.7327   0.5352
  -1.750  -0.0579   0.00715   0.00160  -0.0301   0.7259   0.5654
  -1.500  -0.0306   0.00709   0.00159  -0.0300   0.7187   0.5914
  -1.250  -0.0030   0.00707   0.00156  -0.0298   0.7092   0.6070
  -0.750   0.0527   0.00706   0.00151  -0.0296   0.6899   0.6293
  -0.500   0.0805   0.00706   0.00150  -0.0295   0.6809   0.6408
  -0.250   0.1084   0.00707   0.00149  -0.0294   0.6722   0.6517
   0.000   0.1362   0.00709   0.00149  -0.0294   0.6637   0.6621
   0.250   0.1640   0.00709   0.00150  -0.0292   0.6529   0.6717
   0.500   0.1918   0.00711   0.00152  -0.0292   0.6424   0.6809
   0.750   0.2195   0.00714   0.00153  -0.0290   0.6314   0.6911
   1.000   0.2471   0.00717   0.00156  -0.0289   0.6201   0.6993
   1.250   0.2750   0.00721   0.00159  -0.0289   0.6084   0.7063
   1.500   0.3027   0.00724   0.00162  -0.0288   0.5964   0.7125
   1.750   0.3303   0.00730   0.00166  -0.0287   0.5820   0.7195
   2.000   0.3576   0.00737   0.00171  -0.0285   0.5654   0.7261
   2.500   0.4113   0.00758   0.00184  -0.0280   0.5223   0.7404
   2.750   0.4372   0.00775   0.00193  -0.0277   0.4910   0.7479
   3.000   0.4626   0.00799   0.00205  -0.0272   0.4535   0.7551
   3.250   0.4877   0.00825   0.00219  -0.0268   0.4161   0.7627
   3.500   0.5124   0.00856   0.00237  -0.0263   0.3741   0.7701
   3.750   0.5360   0.00898   0.00258  -0.0257   0.3199   0.7782
   4.000   0.5600   0.00936   0.00281  -0.0251   0.2805   0.7861
   4.250   0.5855   0.00959   0.00300  -0.0248   0.2620   0.7948
   4.500   0.6112   0.00979   0.00321  -0.0244   0.2485   0.8033
   4.750   0.6368   0.00999   0.00340  -0.0240   0.2354   0.8126
   5.000   0.6621   0.01019   0.00361  -0.0236   0.2206   0.8227
   5.250   0.6870   0.01041   0.00382  -0.0231   0.2043   0.8335
   5.500   0.7116   0.01063   0.00405  -0.0226   0.1873   0.8453
   5.750   0.7358   0.01086   0.00428  -0.0220   0.1710   0.8587
   6.000   0.7592   0.01112   0.00453  -0.0212   0.1528   0.8756
   6.500   0.8100   0.01175   0.00518  -0.0206   0.1142   0.9349
   6.750   0.8490   0.01219   0.00558  -0.0234   0.0972   0.9856
   7.000   0.8740   0.01262   0.00595  -0.0232   0.0839   1.0000
   7.250   0.8967   0.01304   0.00632  -0.0226   0.0732   1.0000
   7.500   0.9198   0.01342   0.00670  -0.0219   0.0656   1.0000
   7.750   0.9426   0.01383   0.00709  -0.0212   0.0586   1.0000
   8.000   0.9649   0.01427   0.00750  -0.0205   0.0519   1.0000
   8.250   0.9875   0.01467   0.00791  -0.0198   0.0466   1.0000
   8.500   1.0093   0.01512   0.00836  -0.0190   0.0413   1.0000
   8.750   1.0309   0.01557   0.00881  -0.0182   0.0362   1.0000
   9.000   1.0513   0.01611   0.00932  -0.0172   0.0305   1.0000
   9.250   1.0724   0.01657   0.00981  -0.0164   0.0271   1.0000
   9.500   1.0921   0.01711   0.01036  -0.0153   0.0234   1.0000
   9.750   1.1118   0.01764   0.01091  -0.0142   0.0206   1.0000
  10.000   1.1301   0.01823   0.01152  -0.0130   0.0176   1.0000
  10.250   1.1477   0.01884   0.01216  -0.0117   0.0152   1.0000
  10.500   1.1637   0.01951   0.01287  -0.0102   0.0131   1.0000
  10.750   1.1775   0.02017   0.01358  -0.0083   0.0115   1.0000
  11.000   1.1895   0.02090   0.01435  -0.0061   0.0098   1.0000
  11.250   1.2003   0.02172   0.01522  -0.0040   0.0086   1.0000
  11.500   1.2117   0.02254   0.01611  -0.0020   0.0076   1.0000
  11.750   1.2225   0.02341   0.01704  -0.0002   0.0069   1.0000
  12.000   1.2304   0.02453   0.01822   0.0017   0.0062   1.0000
  12.250   1.2406   0.02553   0.01930   0.0033   0.0060   1.0000
  12.500   1.2489   0.02670   0.02057   0.0049   0.0056   1.0000
  12.750   1.2564   0.02798   0.02196   0.0064   0.0054   1.0000
  13.000   1.2631   0.02938   0.02346   0.0077   0.0052   1.0000
  13.250   1.2694   0.03087   0.02504   0.0089   0.0050   1.0000
  13.500   1.2744   0.03253   0.02680   0.0099   0.0048   1.0000
  13.750   1.2777   0.03441   0.02878   0.0108   0.0047   1.0000
  14.000   1.2784   0.03664   0.03112   0.0116   0.0045   1.0000
  14.250   1.2765   0.03923   0.03383   0.0121   0.0043   1.0000
  14.500   1.2734   0.04207   0.03679   0.0123   0.0043   1.0000
  14.750   1.2711   0.04498   0.03982   0.0122   0.0042   1.0000
  15.000   1.2657   0.04838   0.04336   0.0117   0.0042   1.0000
  15.250   1.2611   0.05190   0.04701   0.0110   0.0041   1.0000
  15.500   1.2560   0.05565   0.05089   0.0098   0.0041   1.0000
  15.750   1.2472   0.06015   0.05554   0.0082   0.0040   1.0000
  16.000   1.2352   0.06546   0.06100   0.0059   0.0040   1.0000
  16.250   1.2230   0.07112   0.06681   0.0032   0.0040   1.0000
  16.500   1.2076   0.07765   0.07350  -0.0001   0.0040   1.0000
  16.750   1.1918   0.08459   0.08058  -0.0038   0.0040   1.0000
  17.000   1.1734   0.09228   0.08843  -0.0080   0.0040   1.0000
  17.250   1.1527   0.10067   0.09697  -0.0126   0.0040   1.0000
  17.500   1.1328   0.10906   0.10551  -0.0172   0.0040   1.0000
  17.750   1.1114   0.11789   0.11445  -0.0221   0.0041   1.0000
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