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HQ 3.5/13 AIRFOIL (hq3513-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: HQ 3.5/13 AIRFOIL (hq3513-il)
Reynolds number: 1,000,000
Max Cl/Cd: 101.53 at α=6.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-hq3513-il-1000000-n5.txt
Download as CSV file: xf-hq3513-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: HQ 3.5/13 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
  ------ -------- --------- --------- -------- -------- --------
 -14.250  -0.6439   0.08302   0.08094  -0.0617   1.0000   0.0054
 -14.000  -0.7365   0.06114   0.05880  -0.0742   1.0000   0.0051
 -13.750  -0.7677   0.05022   0.04769  -0.0820   1.0000   0.0050
 -13.500  -0.7894   0.04347   0.04079  -0.0868   1.0000   0.0050
 -13.250  -0.8038   0.03810   0.03525  -0.0910   0.9991   0.0050
 -13.000  -0.8111   0.03203   0.02892  -0.0984   0.9842   0.0051
 -12.750  -0.7957   0.02859   0.02527  -0.1043   0.9754   0.0051
 -12.500  -0.7779   0.02567   0.02213  -0.1092   0.9635   0.0052
 -12.250  -0.7580   0.02394   0.02022  -0.1111   0.9509   0.0053
 -12.000  -0.7425   0.02246   0.01857  -0.1113   0.9350   0.0054
 -11.750  -0.7269   0.02138   0.01734  -0.1107   0.9213   0.0054
 -11.500  -0.7111   0.02040   0.01620  -0.1099   0.9100   0.0055
 -11.250  -0.6936   0.01955   0.01521  -0.1090   0.9002   0.0056
 -11.000  -0.6749   0.01874   0.01428  -0.1083   0.8916   0.0057
 -10.500  -0.6346   0.01726   0.01256  -0.1070   0.8767   0.0059
 -10.250  -0.6133   0.01659   0.01177  -0.1064   0.8696   0.0060
 -10.000  -0.5906   0.01600   0.01110  -0.1060   0.8632   0.0061
  -9.750  -0.5675   0.01547   0.01046  -0.1055   0.8568   0.0063
  -9.500  -0.5440   0.01493   0.00983  -0.1052   0.8511   0.0065
  -9.250  -0.5201   0.01439   0.00919  -0.1048   0.8449   0.0066
  -8.750  -0.4711   0.01341   0.00804  -0.1042   0.8335   0.0068
  -8.500  -0.4460   0.01299   0.00754  -0.1039   0.8276   0.0070
  -8.250  -0.4205   0.01261   0.00708  -0.1036   0.8221   0.0070
  -8.000  -0.3949   0.01219   0.00659  -0.1034   0.8161   0.0071
  -7.750  -0.3697   0.01172   0.00604  -0.1032   0.8104   0.0074
  -7.500  -0.3437   0.01134   0.00560  -0.1030   0.8049   0.0076
  -7.250  -0.3174   0.01101   0.00521  -0.1028   0.7989   0.0078
  -7.000  -0.2910   0.01072   0.00486  -0.1027   0.7934   0.0081
  -6.750  -0.2641   0.01043   0.00452  -0.1026   0.7879   0.0083
  -6.500  -0.2373   0.01019   0.00423  -0.1025   0.7820   0.0086
  -6.250  -0.2102   0.00996   0.00395  -0.1024   0.7767   0.0089
  -6.000  -0.1829   0.00974   0.00369  -0.1023   0.7711   0.0093
  -5.750  -0.1558   0.00953   0.00343  -0.1022   0.7657   0.0101
  -5.500  -0.1285   0.00929   0.00317  -0.1022   0.7604   0.0121
  -5.250  -0.1014   0.00902   0.00294  -0.1022   0.7548   0.0193
  -4.750  -0.0460   0.00874   0.00263  -0.1022   0.7444   0.0274
  -4.500  -0.0183   0.00859   0.00248  -0.1022   0.7387   0.0310
  -4.250   0.0095   0.00848   0.00234  -0.1022   0.7335   0.0340
  -4.000   0.0376   0.00837   0.00221  -0.1023   0.7278   0.0363
  -3.750   0.0653   0.00826   0.00209  -0.1023   0.7218   0.0400
  -3.500   0.0933   0.00816   0.00198  -0.1023   0.7154   0.0441
  -3.250   0.1209   0.00806   0.00187  -0.1022   0.7070   0.0500
  -3.000   0.1486   0.00799   0.00177  -0.1022   0.6974   0.0553
  -2.750   0.1760   0.00790   0.00167  -0.1022   0.6877   0.0653
  -2.250   0.2312   0.00765   0.00150  -0.1022   0.6712   0.1076
  -2.000   0.2586   0.00750   0.00142  -0.1022   0.6630   0.1406
  -1.750   0.2861   0.00731   0.00135  -0.1022   0.6567   0.1899
  -1.500   0.3137   0.00711   0.00129  -0.1023   0.6502   0.2418
  -1.250   0.3406   0.00683   0.00121  -0.1023   0.6428   0.3223
  -1.000   0.3676   0.00660   0.00117  -0.1024   0.6338   0.4011
  -0.750   0.3950   0.00646   0.00116  -0.1024   0.6264   0.4565
  -0.500   0.4221   0.00633   0.00118  -0.1023   0.6171   0.5209
  -0.250   0.4495   0.00628   0.00122  -0.1022   0.6072   0.5661
   0.000   0.4768   0.00630   0.00126  -0.1021   0.5964   0.5966
   0.250   0.5040   0.00636   0.00130  -0.1020   0.5823   0.6102
   0.500   0.5311   0.00644   0.00134  -0.1018   0.5678   0.6202
   0.750   0.5583   0.00653   0.00139  -0.1017   0.5546   0.6300
   1.000   0.5853   0.00663   0.00144  -0.1015   0.5401   0.6379
   1.250   0.6122   0.00675   0.00150  -0.1013   0.5234   0.6433
   1.500   0.6383   0.00690   0.00158  -0.1010   0.5026   0.6484
   1.750   0.6639   0.00711   0.00168  -0.1006   0.4783   0.6537
   2.000   0.6894   0.00732   0.00179  -0.1002   0.4544   0.6587
   2.250   0.7149   0.00751   0.00191  -0.0998   0.4333   0.6641
   2.500   0.7403   0.00772   0.00203  -0.0994   0.4115   0.6695
   2.750   0.7653   0.00796   0.00217  -0.0990   0.3883   0.6747
   3.000   0.7898   0.00822   0.00233  -0.0984   0.3636   0.6804
   3.250   0.8143   0.00848   0.00250  -0.0979   0.3382   0.6864
   3.500   0.8378   0.00879   0.00269  -0.0972   0.3094   0.6919
   3.750   0.8616   0.00908   0.00288  -0.0966   0.2885   0.6982
   4.250   0.9111   0.00950   0.00324  -0.0956   0.2633   0.7104
   4.500   0.9362   0.00969   0.00340  -0.0952   0.2554   0.7171
   4.750   0.9612   0.00986   0.00358  -0.0947   0.2479   0.7234
   5.000   0.9861   0.01004   0.00375  -0.0943   0.2416   0.7303
   5.250   1.0112   0.01019   0.00392  -0.0939   0.2364   0.7372
   5.500   1.0354   0.01039   0.00412  -0.0933   0.2300   0.7446
   5.750   1.0603   0.01054   0.00430  -0.0929   0.2252   0.7520
   6.000   1.0842   0.01073   0.00450  -0.0923   0.2185   0.7603
   6.250   1.1078   0.01093   0.00470  -0.0916   0.2113   0.7686
   6.500   1.1310   0.01114   0.00492  -0.0909   0.2038   0.7779
   6.750   1.1534   0.01137   0.00515  -0.0900   0.1939   0.7878
   7.000   1.1751   0.01162   0.00540  -0.0890   0.1854   0.7987
   7.250   1.1971   0.01182   0.00564  -0.0881   0.1774   0.8113
   7.500   1.2171   0.01209   0.00592  -0.0868   0.1667   0.8279
   8.000   1.2556   0.01256   0.00656  -0.0841   0.1404   1.0000
   8.250   1.2711   0.01300   0.00694  -0.0821   0.1274   1.0000
   8.500   1.2845   0.01355   0.00740  -0.0797   0.1109   1.0000
   8.750   1.2983   0.01411   0.00788  -0.0776   0.0972   1.0000
   9.000   1.3085   0.01486   0.00850  -0.0749   0.0779   1.0000
   9.250   1.3198   0.01558   0.00913  -0.0725   0.0624   1.0000
   9.500   1.3316   0.01631   0.00979  -0.0703   0.0502   1.0000
   9.750   1.3430   0.01708   0.01049  -0.0681   0.0390   1.0000
  10.000   1.3532   0.01794   0.01129  -0.0658   0.0281   1.0000
  10.250   1.3620   0.01892   0.01221  -0.0635   0.0176   1.0000
  10.500   1.3714   0.01990   0.01317  -0.0613   0.0104   1.0000
  10.750   1.3807   0.02092   0.01418  -0.0592   0.0048   1.0000
  11.000   1.3928   0.02178   0.01506  -0.0575   0.0041   1.0000
  11.250   1.4055   0.02262   0.01594  -0.0560   0.0036   1.0000
  11.500   1.4187   0.02344   0.01681  -0.0546   0.0035   1.0000
  11.750   1.4304   0.02439   0.01781  -0.0531   0.0032   1.0000
  12.000   1.4427   0.02533   0.01880  -0.0518   0.0032   1.0000
  12.250   1.4528   0.02644   0.01997  -0.0503   0.0029   1.0000
  12.500   1.4629   0.02758   0.02118  -0.0489   0.0028   1.0000
  12.750   1.4723   0.02880   0.02246  -0.0476   0.0027   1.0000
  13.000   1.4804   0.03017   0.02389  -0.0462   0.0026   1.0000
  13.250   1.4856   0.03182   0.02563  -0.0448   0.0024   1.0000
  13.500   1.4935   0.03327   0.02714  -0.0436   0.0023   1.0000
  13.750   1.5012   0.03479   0.02872  -0.0426   0.0023   1.0000
  14.000   1.5074   0.03649   0.03051  -0.0415   0.0022   1.0000
  14.250   1.5132   0.03826   0.03235  -0.0406   0.0022   1.0000
  14.500   1.5177   0.04023   0.03440  -0.0398   0.0021   1.0000
  14.750   1.5216   0.04233   0.03658  -0.0390   0.0021   1.0000
  15.000   1.5254   0.04450   0.03883  -0.0385   0.0021   1.0000
  15.250   1.5269   0.04699   0.04141  -0.0379   0.0020   1.0000
  15.500   1.5285   0.04958   0.04408  -0.0376   0.0020   1.0000
  15.750   1.5282   0.05246   0.04707  -0.0374   0.0019   1.0000
  16.000   1.5275   0.05550   0.05019  -0.0374   0.0019   1.0000
  16.250   1.5251   0.05885   0.05365  -0.0376   0.0019   1.0000
  16.500   1.5221   0.06241   0.05730  -0.0380   0.0018   1.0000
  16.750   1.5174   0.06633   0.06135  -0.0387   0.0018   1.0000
  17.000   1.5125   0.07042   0.06554  -0.0396   0.0018   1.0000
  17.250   1.5053   0.07498   0.07021  -0.0408   0.0018   1.0000
  17.500   1.4968   0.07991   0.07526  -0.0423   0.0018   1.0000
  17.750   1.4864   0.08534   0.08082  -0.0442   0.0017   1.0000
  18.000   1.4768   0.09077   0.08637  -0.0463   0.0017   1.0000
  18.250   1.4633   0.09705   0.09278  -0.0488   0.0017   1.0000
  18.500   1.4503   0.10341   0.09926  -0.0516   0.0017   1.0000
  18.750   1.4353   0.11029   0.10628  -0.0548   0.0017   1.0000
  19.000   1.4211   0.11710   0.11322  -0.0582   0.0017   1.0000
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