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HQ 1.0/12 AIRFOIL (hq1012-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: HQ 1.0/12 AIRFOIL (hq1012-il)
Reynolds number: 1,000,000
Max Cl/Cd: 87.52 at α=6.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-hq1012-il-1000000.txt
Download as CSV file: xf-hq1012-il-1000000.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 =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.750  -0.8408   0.12107   0.11905  -0.0078   1.0000   0.0063
 -16.500  -0.8722   0.10969   0.10756  -0.0139   1.0000   0.0063
 -16.250  -0.9228   0.09504   0.09272  -0.0219   1.0000   0.0061
 -16.000  -0.9462   0.08612   0.08369  -0.0270   1.0000   0.0061
 -15.750  -0.9877   0.07393   0.07130  -0.0342   1.0000   0.0060
 -15.500  -1.0082   0.06619   0.06340  -0.0390   1.0000   0.0059
 -15.250  -1.0278   0.05908   0.05614  -0.0434   1.0000   0.0059
 -15.000  -1.0439   0.05301   0.04992  -0.0470   1.0000   0.0060
 -14.750  -1.0604   0.04747   0.04421  -0.0499   1.0000   0.0059
 -14.500  -1.0671   0.04355   0.04017  -0.0517   1.0000   0.0059
 -14.250  -1.0753   0.03976   0.03624  -0.0529   1.0000   0.0060
 -14.000  -1.0733   0.03734   0.03373  -0.0536   1.0000   0.0062
 -13.750  -1.0760   0.03460   0.03086  -0.0538   1.0000   0.0062
 -13.500  -1.0791   0.03202   0.02815  -0.0536   1.0000   0.0062
 -13.250  -1.0788   0.02994   0.02595  -0.0530   1.0000   0.0064
 -13.000  -1.0780   0.02810   0.02400  -0.0519   1.0000   0.0063
 -12.750  -1.0754   0.02657   0.02236  -0.0505   1.0000   0.0065
 -12.500  -1.0727   0.02525   0.02093  -0.0484   1.0000   0.0066
 -12.250  -1.0691   0.02416   0.01973  -0.0458   1.0000   0.0067
 -12.000  -1.0633   0.02321   0.01868  -0.0432   1.0000   0.0068
 -11.750  -1.0521   0.02224   0.01762  -0.0413   1.0000   0.0069
 -11.500  -1.0373   0.02147   0.01677  -0.0399   1.0000   0.0070
 -11.250  -1.0236   0.02054   0.01574  -0.0382   1.0000   0.0072
 -11.000  -1.0162   0.01899   0.01404  -0.0358   1.0000   0.0075
 -10.750  -1.0018   0.01803   0.01301  -0.0342   1.0000   0.0079
 -10.500  -0.9834   0.01743   0.01236  -0.0329   1.0000   0.0082
 -10.250  -0.9650   0.01683   0.01171  -0.0316   1.0000   0.0086
 -10.000  -0.9463   0.01628   0.01112  -0.0303   1.0000   0.0090
  -9.750  -0.9277   0.01576   0.01053  -0.0289   1.0000   0.0094
  -9.500  -0.9090   0.01530   0.01002  -0.0275   1.0000   0.0097
  -9.250  -0.8907   0.01447   0.00911  -0.0262   0.9993   0.0103
  -9.000  -0.8577   0.01370   0.00830  -0.0279   0.9953   0.0112
  -8.750  -0.8251   0.01317   0.00773  -0.0293   0.9900   0.0122
  -8.500  -0.7908   0.01272   0.00723  -0.0310   0.9852   0.0132
  -8.250  -0.7574   0.01204   0.00654  -0.0326   0.9793   0.0157
  -8.000  -0.7233   0.01157   0.00604  -0.0343   0.9714   0.0186
  -7.750  -0.6908   0.01119   0.00567  -0.0355   0.9601   0.0226
  -7.500  -0.6618   0.01080   0.00530  -0.0360   0.9446   0.0280
  -7.250  -0.6354   0.01056   0.00499  -0.0358   0.9270   0.0316
  -7.000  -0.6106   0.01031   0.00471  -0.0352   0.9110   0.0357
  -6.750  -0.5849   0.01018   0.00451  -0.0348   0.8976   0.0380
  -6.500  -0.5601   0.00989   0.00419  -0.0342   0.8853   0.0431
  -6.250  -0.5343   0.00970   0.00397  -0.0339   0.8744   0.0469
  -6.000  -0.5084   0.00952   0.00373  -0.0335   0.8646   0.0509
  -5.750  -0.4826   0.00928   0.00348  -0.0332   0.8551   0.0575
  -5.500  -0.4563   0.00908   0.00326  -0.0329   0.8464   0.0646
  -5.250  -0.4302   0.00887   0.00304  -0.0326   0.8380   0.0747
  -5.000  -0.4041   0.00860   0.00283  -0.0324   0.8298   0.0902
  -4.500  -0.3521   0.00803   0.00240  -0.0319   0.8143   0.1403
  -4.250  -0.3264   0.00773   0.00221  -0.0316   0.8070   0.1775
  -4.000  -0.2998   0.00746   0.00205  -0.0314   0.7994   0.2123
  -3.750  -0.2734   0.00723   0.00190  -0.0312   0.7922   0.2448
  -3.500  -0.2470   0.00693   0.00174  -0.0311   0.7846   0.2856
  -3.250  -0.2216   0.00657   0.00157  -0.0308   0.7774   0.3490
  -3.000  -0.1955   0.00623   0.00144  -0.0306   0.7700   0.4132
  -2.750  -0.1691   0.00599   0.00134  -0.0303   0.7633   0.4675
  -2.500  -0.1422   0.00578   0.00128  -0.0302   0.7566   0.5154
  -2.250  -0.1147   0.00569   0.00123  -0.0301   0.7495   0.5438
  -2.000  -0.0868   0.00562   0.00119  -0.0300   0.7411   0.5656
  -1.500  -0.0311   0.00554   0.00114  -0.0299   0.7249   0.6070
  -1.000   0.0252   0.00550   0.00112  -0.0298   0.7099   0.6369
  -0.750   0.0532   0.00552   0.00111  -0.0298   0.7023   0.6476
  -0.500   0.0819   0.00551   0.00110  -0.0298   0.6948   0.6564
  -0.250   0.1099   0.00552   0.00109  -0.0298   0.6869   0.6640
   0.000   0.1384   0.00553   0.00109  -0.0298   0.6777   0.6730
   0.250   0.1665   0.00553   0.00110  -0.0298   0.6698   0.6817
   0.500   0.1948   0.00555   0.00111  -0.0298   0.6617   0.6900
   0.750   0.2230   0.00556   0.00113  -0.0298   0.6533   0.6982
   1.000   0.2512   0.00559   0.00115  -0.0298   0.6443   0.7060
   1.250   0.2794   0.00560   0.00118  -0.0298   0.6349   0.7145
   1.500   0.3074   0.00563   0.00121  -0.0298   0.6244   0.7226
   1.750   0.3354   0.00568   0.00124  -0.0297   0.6126   0.7303
   2.000   0.3632   0.00572   0.00128  -0.0297   0.5981   0.7367
   2.250   0.3909   0.00578   0.00132  -0.0296   0.5804   0.7435
   2.500   0.4183   0.00587   0.00136  -0.0295   0.5591   0.7502
   2.750   0.4454   0.00598   0.00143  -0.0293   0.5361   0.7574
   3.000   0.4719   0.00615   0.00151  -0.0290   0.5039   0.7648
   3.250   0.4974   0.00640   0.00162  -0.0286   0.4603   0.7726
   3.500   0.5230   0.00665   0.00176  -0.0283   0.4218   0.7805
   3.750   0.5481   0.00696   0.00192  -0.0278   0.3775   0.7891
   4.000   0.5727   0.00730   0.00210  -0.0273   0.3287   0.7973
   4.250   0.5978   0.00761   0.00228  -0.0269   0.2933   0.8066
   4.500   0.6232   0.00784   0.00247  -0.0265   0.2703   0.8158
   4.750   0.6488   0.00806   0.00264  -0.0262   0.2507   0.8259
   5.000   0.6746   0.00826   0.00281  -0.0259   0.2347   0.8368
   5.250   0.7003   0.00841   0.00298  -0.0255   0.2213   0.8488
   5.500   0.7256   0.00856   0.00316  -0.0250   0.2078   0.8625
   5.750   0.7503   0.00873   0.00334  -0.0244   0.1923   0.8798
   6.000   0.7735   0.00891   0.00354  -0.0235   0.1736   0.9050
   6.250   0.8008   0.00915   0.00379  -0.0235   0.1497   0.9534
   6.750   0.8679   0.01002   0.00444  -0.0268   0.1025   1.0000
   7.000   0.8913   0.01039   0.00473  -0.0262   0.0882   1.0000
   7.250   0.9147   0.01077   0.00505  -0.0255   0.0760   1.0000
   7.500   0.9380   0.01115   0.00537  -0.0249   0.0661   1.0000
   7.750   0.9614   0.01151   0.00569  -0.0243   0.0582   1.0000
   8.000   0.9853   0.01183   0.00601  -0.0237   0.0522   1.0000
   8.250   1.0083   0.01222   0.00636  -0.0230   0.0461   1.0000
   8.500   1.0320   0.01255   0.00670  -0.0224   0.0420   1.0000
   8.750   1.0544   0.01296   0.00708  -0.0217   0.0367   1.0000
   9.000   1.0773   0.01333   0.00746  -0.0210   0.0330   1.0000
   9.250   1.0990   0.01378   0.00788  -0.0202   0.0284   1.0000
   9.500   1.1211   0.01419   0.00830  -0.0194   0.0251   1.0000
   9.750   1.1412   0.01474   0.00883  -0.0184   0.0205   1.0000
  10.000   1.1620   0.01520   0.00929  -0.0174   0.0176   1.0000
  10.250   1.1811   0.01577   0.00987  -0.0162   0.0143   1.0000
  10.500   1.1981   0.01648   0.01057  -0.0148   0.0114   1.0000
  10.750   1.2167   0.01702   0.01115  -0.0135   0.0101   1.0000
  11.000   1.2303   0.01789   0.01205  -0.0116   0.0085   1.0000
  11.250   1.2462   0.01843   0.01266  -0.0099   0.0079   1.0000
  11.500   1.2590   0.01903   0.01332  -0.0077   0.0074   1.0000
  11.750   1.2699   0.01974   0.01407  -0.0053   0.0069   1.0000
  12.000   1.2793   0.02057   0.01495  -0.0029   0.0066   1.0000
  12.250   1.2831   0.02177   0.01625  -0.0001   0.0061   1.0000
  12.500   1.2913   0.02277   0.01733   0.0020   0.0060   1.0000
  12.750   1.2999   0.02378   0.01842   0.0039   0.0060   1.0000
  13.000   1.3092   0.02480   0.01952   0.0055   0.0057   1.0000
  13.250   1.3149   0.02613   0.02094   0.0072   0.0056   1.0000
  13.500   1.3239   0.02727   0.02215   0.0084   0.0054   1.0000
  13.750   1.3271   0.02893   0.02392   0.0099   0.0053   1.0000
  14.000   1.3316   0.03057   0.02564   0.0111   0.0052   1.0000
  14.250   1.3366   0.03224   0.02740   0.0120   0.0051   1.0000
  14.500   1.3349   0.03459   0.02987   0.0129   0.0051   1.0000
  14.750   1.3389   0.03654   0.03188   0.0134   0.0048   1.0000
  15.000   1.3373   0.03913   0.03458   0.0137   0.0048   1.0000
  15.250   1.3331   0.04212   0.03768   0.0138   0.0046   1.0000
  15.500   1.3295   0.04523   0.04089   0.0136   0.0046   1.0000
  15.750   1.3221   0.04891   0.04470   0.0129   0.0046   1.0000
  16.000   1.3085   0.05366   0.04958   0.0116   0.0045   1.0000
  16.250   1.3024   0.05772   0.05375   0.0102   0.0045   1.0000
  16.500   1.2849   0.06370   0.05988   0.0078   0.0044   1.0000
  16.750   1.2758   0.06878   0.06508   0.0054   0.0045   1.0000
  17.000   1.2555   0.07593   0.07238   0.0019   0.0044   1.0000
  17.250   1.2364   0.08328   0.07988  -0.0020   0.0044   1.0000
  17.500   1.2266   0.08920   0.08592  -0.0051   0.0045   1.0000
  17.750   1.2061   0.09730   0.09415  -0.0095   0.0045   1.0000
  18.000   1.1782   0.10701   0.10400  -0.0148   0.0044   1.0000
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