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HQ 1.5/12 AIRFOIL (hq1512-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: HQ 1.5/12 AIRFOIL (hq1512-il)
Reynolds number: 500,000
Max Cl/Cd: 73.2 at α=6.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-hq1512-il-500000-n5.txt
Download as CSV file: xf-hq1512-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: HQ 1.5/12 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
  ------ -------- --------- --------- -------- -------- --------
 -15.250  -0.8258   0.09075   0.08786  -0.0307   1.0000   0.0065
 -15.000  -0.8604   0.07921   0.07615  -0.0376   1.0000   0.0066
 -14.750  -0.8885   0.06940   0.06618  -0.0438   1.0000   0.0065
 -14.500  -0.9139   0.06066   0.05725  -0.0497   1.0000   0.0065
 -14.250  -0.9283   0.05458   0.05101  -0.0536   1.0000   0.0065
 -14.000  -0.9432   0.04901   0.04528  -0.0570   1.0000   0.0065
 -13.750  -0.9536   0.04458   0.04068  -0.0592   1.0000   0.0066
 -13.500  -0.9635   0.04061   0.03655  -0.0607   1.0000   0.0065
 -13.250  -0.9651   0.03782   0.03360  -0.0614   1.0000   0.0067
 -13.000  -0.9706   0.03491   0.03054  -0.0617   1.0000   0.0068
 -12.750  -0.9762   0.03230   0.02782  -0.0613   1.0000   0.0070
 -12.500  -0.9770   0.03034   0.02573  -0.0604   1.0000   0.0070
 -12.250  -0.9748   0.02889   0.02419  -0.0589   1.0000   0.0072
 -12.000  -0.9719   0.02771   0.02292  -0.0568   1.0000   0.0073
 -11.750  -0.9683   0.02656   0.02167  -0.0542   1.0000   0.0075
 -11.500  -0.9577   0.02559   0.02061  -0.0526   1.0000   0.0077
 -11.250  -0.9460   0.02462   0.01955  -0.0510   1.0000   0.0079
 -11.000  -0.9332   0.02369   0.01850  -0.0493   1.0000   0.0082
 -10.750  -0.9197   0.02279   0.01749  -0.0477   1.0000   0.0085
 -10.500  -0.9060   0.02190   0.01649  -0.0460   1.0000   0.0088
 -10.250  -0.8908   0.02117   0.01566  -0.0443   1.0000   0.0091
  -9.750  -0.8450   0.01930   0.01362  -0.0444   0.9908   0.0100
  -9.500  -0.8140   0.01858   0.01284  -0.0459   0.9850   0.0106
  -9.250  -0.7835   0.01788   0.01205  -0.0471   0.9779   0.0112
  -9.000  -0.7519   0.01715   0.01123  -0.0486   0.9708   0.0119
  -8.750  -0.7217   0.01648   0.01046  -0.0496   0.9613   0.0124
  -8.500  -0.6908   0.01590   0.00978  -0.0507   0.9514   0.0129
  -8.250  -0.6631   0.01507   0.00889  -0.0514   0.9391   0.0139
  -8.000  -0.6354   0.01456   0.00831  -0.0517   0.9261   0.0149
  -7.750  -0.6094   0.01411   0.00778  -0.0516   0.9136   0.0158
  -7.500  -0.5845   0.01370   0.00726  -0.0512   0.9021   0.0166
  -7.250  -0.5599   0.01330   0.00677  -0.0507   0.8915   0.0175
  -7.000  -0.5359   0.01285   0.00626  -0.0501   0.8815   0.0192
  -6.750  -0.5110   0.01251   0.00587  -0.0497   0.8720   0.0211
  -6.500  -0.4856   0.01222   0.00548  -0.0493   0.8635   0.0229
  -6.250  -0.4608   0.01185   0.00508  -0.0488   0.8552   0.0263
  -6.000  -0.4350   0.01157   0.00476  -0.0485   0.8473   0.0300
  -5.750  -0.4096   0.01126   0.00444  -0.0481   0.8399   0.0362
  -5.500  -0.3837   0.01098   0.00414  -0.0478   0.8322   0.0436
  -5.250  -0.3577   0.01074   0.00387  -0.0476   0.8251   0.0523
  -5.000  -0.3314   0.01048   0.00362  -0.0473   0.8178   0.0625
  -4.750  -0.3053   0.01022   0.00338  -0.0471   0.8108   0.0764
  -4.500  -0.2791   0.00994   0.00315  -0.0469   0.8038   0.0952
  -4.250  -0.2529   0.00967   0.00294  -0.0467   0.7969   0.1183
  -4.000  -0.2267   0.00937   0.00274  -0.0465   0.7901   0.1486
  -3.750  -0.2006   0.00907   0.00255  -0.0463   0.7832   0.1861
  -3.500  -0.1740   0.00883   0.00238  -0.0461   0.7767   0.2177
  -3.250  -0.1476   0.00856   0.00221  -0.0460   0.7697   0.2542
  -3.000  -0.1215   0.00824   0.00203  -0.0458   0.7631   0.3035
  -2.750  -0.0961   0.00782   0.00187  -0.0456   0.7559   0.3815
  -2.500  -0.0703   0.00751   0.00176  -0.0453   0.7493   0.4484
  -2.250  -0.0437   0.00731   0.00170  -0.0451   0.7419   0.4997
  -2.000  -0.0166   0.00722   0.00165  -0.0449   0.7352   0.5314
  -1.750   0.0111   0.00715   0.00161  -0.0448   0.7273   0.5548
  -1.500   0.0386   0.00712   0.00158  -0.0446   0.7187   0.5746
  -1.250   0.0660   0.00709   0.00156  -0.0444   0.7083   0.5946
  -1.000   0.0937   0.00708   0.00154  -0.0443   0.6992   0.6114
  -0.750   0.1214   0.00709   0.00153  -0.0442   0.6906   0.6241
  -0.500   0.1492   0.00708   0.00153  -0.0441   0.6812   0.6378
  -0.250   0.1769   0.00709   0.00153  -0.0439   0.6726   0.6502
   0.000   0.2047   0.00713   0.00153  -0.0438   0.6632   0.6613
   0.250   0.2324   0.00713   0.00155  -0.0437   0.6526   0.6708
   0.500   0.2601   0.00716   0.00156  -0.0436   0.6414   0.6797
   0.750   0.2877   0.00720   0.00158  -0.0435   0.6306   0.6890
   1.000   0.3153   0.00724   0.00161  -0.0434   0.6196   0.6963
   1.250   0.3430   0.00728   0.00164  -0.0433   0.6072   0.7030
   1.500   0.3706   0.00733   0.00168  -0.0432   0.5953   0.7093
   1.750   0.3981   0.00739   0.00172  -0.0430   0.5823   0.7161
   2.000   0.4253   0.00747   0.00177  -0.0429   0.5660   0.7228
   2.250   0.4521   0.00756   0.00184  -0.0426   0.5474   0.7298
   2.500   0.4788   0.00768   0.00191  -0.0424   0.5278   0.7371
   2.750   0.5049   0.00782   0.00201  -0.0420   0.5026   0.7443
   3.000   0.5307   0.00802   0.00212  -0.0416   0.4741   0.7519
   3.250   0.5557   0.00825   0.00226  -0.0411   0.4417   0.7593
   3.500   0.5804   0.00854   0.00243  -0.0406   0.4037   0.7672
   3.750   0.6042   0.00889   0.00263  -0.0400   0.3607   0.7753
   4.000   0.6276   0.00929   0.00285  -0.0393   0.3152   0.7836
   4.250   0.6506   0.00971   0.00311  -0.0386   0.2764   0.7927
   4.500   0.6745   0.01004   0.00336  -0.0380   0.2500   0.8018
   4.750   0.6995   0.01027   0.00356  -0.0375   0.2344   0.8118
   5.000   0.7245   0.01047   0.00377  -0.0371   0.2227   0.8229
   5.250   0.7494   0.01064   0.00398  -0.0366   0.2107   0.8346
   5.500   0.7740   0.01083   0.00420  -0.0360   0.1985   0.8481
   5.750   0.7978   0.01102   0.00442  -0.0353   0.1846   0.8645
   6.000   0.8204   0.01126   0.00467  -0.0343   0.1659   0.8881
   6.250   0.8469   0.01157   0.00498  -0.0343   0.1408   0.9304
   6.500   0.8828   0.01208   0.00538  -0.0365   0.1135   1.0000
   6.750   0.9049   0.01257   0.00577  -0.0358   0.0934   1.0000
   7.000   0.9267   0.01307   0.00617  -0.0350   0.0763   1.0000
   7.250   0.9488   0.01353   0.00658  -0.0342   0.0646   1.0000
   7.500   0.9711   0.01397   0.00699  -0.0334   0.0567   1.0000
   7.750   0.9927   0.01446   0.00743  -0.0326   0.0486   1.0000
   8.000   1.0151   0.01485   0.00783  -0.0319   0.0442   1.0000
   8.250   1.0365   0.01531   0.00827  -0.0310   0.0398   1.0000
   8.500   1.0580   0.01574   0.00873  -0.0301   0.0369   1.0000
   8.750   1.0798   0.01613   0.00917  -0.0293   0.0351   1.0000
   9.000   1.1006   0.01657   0.00963  -0.0284   0.0329   1.0000
   9.250   1.1203   0.01708   0.01014  -0.0273   0.0303   1.0000
   9.500   1.1397   0.01758   0.01067  -0.0262   0.0285   1.0000
   9.750   1.1595   0.01801   0.01116  -0.0251   0.0270   1.0000
  10.000   1.1780   0.01848   0.01168  -0.0238   0.0250   1.0000
  10.250   1.1936   0.01901   0.01222  -0.0221   0.0226   1.0000
  10.500   1.2087   0.01956   0.01279  -0.0203   0.0206   1.0000
  10.750   1.2235   0.02012   0.01339  -0.0186   0.0187   1.0000
  11.000   1.2368   0.02079   0.01406  -0.0168   0.0164   1.0000
  11.250   1.2502   0.02147   0.01479  -0.0150   0.0146   1.0000
  11.500   1.2620   0.02227   0.01562  -0.0132   0.0123   1.0000
  11.750   1.2716   0.02325   0.01661  -0.0113   0.0083   1.0000
  12.000   1.2792   0.02440   0.01780  -0.0093   0.0060   1.0000
  12.250   1.2870   0.02559   0.01905  -0.0075   0.0053   1.0000
  12.500   1.2956   0.02676   0.02029  -0.0060   0.0050   1.0000
  12.750   1.3022   0.02814   0.02176  -0.0044   0.0046   1.0000
  13.000   1.3089   0.02956   0.02327  -0.0030   0.0043   1.0000
  13.250   1.3155   0.03104   0.02486  -0.0018   0.0041   1.0000
  13.500   1.3220   0.03259   0.02650  -0.0007   0.0041   1.0000
  13.750   1.3264   0.03438   0.02841   0.0003   0.0039   1.0000
  14.000   1.3295   0.03636   0.03051   0.0011   0.0038   1.0000
  14.250   1.3323   0.03845   0.03272   0.0018   0.0037   1.0000
  14.500   1.3338   0.04075   0.03514   0.0023   0.0036   1.0000
  14.750   1.3324   0.04346   0.03798   0.0025   0.0034   1.0000
  15.000   1.3322   0.04614   0.04079   0.0026   0.0034   1.0000
  15.250   1.3288   0.04931   0.04408   0.0023   0.0033   1.0000
  15.500   1.3239   0.05283   0.04773   0.0017   0.0033   1.0000
  15.750   1.3153   0.05703   0.05208   0.0007   0.0032   1.0000
  16.000   1.3056   0.06166   0.05686  -0.0008   0.0031   1.0000
  16.250   1.2989   0.06610   0.06143  -0.0025   0.0032   1.0000
  16.500   1.2855   0.07184   0.06734  -0.0050   0.0031   1.0000
  16.750   1.2693   0.07842   0.07407  -0.0082   0.0031   1.0000
  17.000   1.2572   0.08452   0.08032  -0.0113   0.0031   1.0000
  17.250   1.2408   0.09172   0.08768  -0.0150   0.0031   1.0000
  17.500   1.2165   0.10076   0.09690  -0.0200   0.0030   1.0000
  17.750   1.1999   0.10844   0.10472  -0.0241   0.0031   1.0000
  18.000   1.1832   0.11631   0.11272  -0.0285   0.0031   1.0000
  18.250   1.1622   0.12520   0.12176  -0.0335   0.0031   1.0000
  18.500   1.1399   0.13461   0.13131  -0.0389   0.0032   1.0000
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