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HQ 3.0/14 AIRFOIL (hq3014-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: HQ 3.0/14 AIRFOIL (hq3014-il)
Reynolds number: 200,000
Max Cl/Cd: 70.87 at α=5.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-hq3014-il-200000-n5.txt
Download as CSV file: xf-hq3014-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: HQ 3.0/14 AIRFOIL                               
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.750  -0.6582   0.05648   0.05216  -0.0796   1.0000   0.0149
 -12.500  -0.6819   0.05072   0.04622  -0.0827   1.0000   0.0149
 -12.250  -0.6990   0.04667   0.04204  -0.0839   1.0000   0.0150
 -12.000  -0.7185   0.04303   0.03823  -0.0839   1.0000   0.0149
 -11.750  -0.7335   0.04082   0.03595  -0.0823   1.0000   0.0150
 -11.500  -0.7498   0.03902   0.03408  -0.0799   0.9987   0.0151
 -11.250  -0.7370   0.03633   0.03119  -0.0833   0.9874   0.0154
 -11.000  -0.7189   0.03420   0.02883  -0.0857   0.9790   0.0159
 -10.750  -0.6981   0.03208   0.02647  -0.0879   0.9720   0.0165
 -10.500  -0.6774   0.03015   0.02426  -0.0893   0.9647   0.0175
 -10.250  -0.6548   0.02824   0.02207  -0.0907   0.9581   0.0184
 -10.000  -0.6310   0.02708   0.02082  -0.0916   0.9512   0.0191
  -9.750  -0.6063   0.02594   0.01956  -0.0925   0.9444   0.0200
  -9.500  -0.5810   0.02468   0.01809  -0.0933   0.9384   0.0212
  -9.250  -0.5580   0.02343   0.01662  -0.0933   0.9308   0.0227
  -8.750  -0.5081   0.02179   0.01481  -0.0939   0.9178   0.0261
  -8.500  -0.4819   0.02089   0.01375  -0.0942   0.9123   0.0287
  -8.250  -0.4576   0.02039   0.01321  -0.0941   0.9054   0.0312
  -8.000  -0.4319   0.01987   0.01253  -0.0941   0.8992   0.0345
  -7.750  -0.4068   0.01929   0.01191  -0.0941   0.8936   0.0372
  -7.500  -0.3828   0.01891   0.01145  -0.0937   0.8864   0.0404
  -7.250  -0.3567   0.01844   0.01087  -0.0936   0.8812   0.0439
  -7.000  -0.3329   0.01807   0.01048  -0.0932   0.8745   0.0474
  -6.750  -0.3075   0.01773   0.01003  -0.0929   0.8686   0.0512
  -6.500  -0.2825   0.01720   0.00941  -0.0926   0.8634   0.0543
  -6.250  -0.2593   0.01671   0.00892  -0.0920   0.8568   0.0573
  -6.000  -0.2339   0.01630   0.00842  -0.0917   0.8516   0.0608
  -5.750  -0.2089   0.01592   0.00795  -0.0913   0.8460   0.0640
  -5.500  -0.1852   0.01542   0.00744  -0.0908   0.8398   0.0675
  -5.250  -0.1594   0.01502   0.00699  -0.0905   0.8351   0.0722
  -5.000  -0.1342   0.01474   0.00662  -0.0901   0.8292   0.0774
  -4.750  -0.1093   0.01435   0.00626  -0.0898   0.8234   0.0854
  -4.500  -0.0828   0.01401   0.00589  -0.0896   0.8190   0.0959
  -4.250  -0.0579   0.01370   0.00561  -0.0893   0.8129   0.1104
  -4.000  -0.0323   0.01335   0.00532  -0.0890   0.8074   0.1342
  -3.750  -0.0064   0.01290   0.00503  -0.0889   0.8031   0.1812
  -3.500   0.0174   0.01245   0.00482  -0.0886   0.7967   0.2450
  -3.250   0.0416   0.01188   0.00456  -0.0883   0.7913   0.3275
  -3.000   0.0655   0.01138   0.00451  -0.0877   0.7867   0.4543
  -2.750   0.0910   0.01128   0.00453  -0.0872   0.7804   0.5079
  -2.500   0.1181   0.01123   0.00449  -0.0869   0.7751   0.5395
  -2.250   0.1453   0.01122   0.00447  -0.0866   0.7698   0.5646
  -2.000   0.1717   0.01123   0.00450  -0.0861   0.7633   0.5897
  -1.750   0.1991   0.01127   0.00451  -0.0857   0.7581   0.6172
  -1.500   0.2255   0.01131   0.00457  -0.0853   0.7519   0.6349
  -1.250   0.2529   0.01132   0.00454  -0.0850   0.7459   0.6459
  -1.000   0.2810   0.01133   0.00450  -0.0849   0.7411   0.6550
  -0.750   0.3077   0.01136   0.00451  -0.0846   0.7344   0.6649
  -0.500   0.3351   0.01138   0.00451  -0.0843   0.7289   0.6746
  -0.250   0.3624   0.01140   0.00452  -0.0841   0.7231   0.6843
   0.000   0.3895   0.01143   0.00453  -0.0839   0.7165   0.6926
   0.250   0.4175   0.01142   0.00447  -0.0838   0.7102   0.6984
   0.500   0.4438   0.01142   0.00447  -0.0834   0.7008   0.7041
   0.750   0.4711   0.01143   0.00441  -0.0832   0.6912   0.7110
   1.000   0.4979   0.01142   0.00439  -0.0828   0.6821   0.7166
   1.250   0.5245   0.01145   0.00442  -0.0825   0.6733   0.7235
   1.500   0.5519   0.01148   0.00442  -0.0823   0.6659   0.7297
   1.750   0.5781   0.01152   0.00448  -0.0819   0.6570   0.7363
   2.000   0.6052   0.01156   0.00449  -0.0817   0.6487   0.7436
   2.250   0.6309   0.01160   0.00457  -0.0812   0.6387   0.7502
   2.500   0.6572   0.01166   0.00462  -0.0809   0.6282   0.7581
   2.750   0.6826   0.01170   0.00467  -0.0803   0.6166   0.7649
   3.000   0.7081   0.01177   0.00472  -0.0798   0.6033   0.7734
   3.250   0.7327   0.01183   0.00479  -0.0791   0.5893   0.7807
   3.500   0.7577   0.01192   0.00487  -0.0785   0.5748   0.7896
   3.750   0.7819   0.01201   0.00496  -0.0777   0.5594   0.7981
   4.000   0.8057   0.01212   0.00507  -0.0769   0.5435   0.8076
   4.250   0.8289   0.01226   0.00520  -0.0760   0.5258   0.8179
   4.500   0.8512   0.01240   0.00533  -0.0749   0.5070   0.8288
   4.750   0.8729   0.01259   0.00550  -0.0737   0.4864   0.8414
   5.000   0.8938   0.01281   0.00568  -0.0724   0.4651   0.8562
   5.250   0.9145   0.01303   0.00588  -0.0711   0.4433   0.8756
   5.500   0.9367   0.01330   0.00614  -0.0701   0.4209   0.9078
   5.750   0.9660   0.01363   0.00644  -0.0709   0.3960   1.0000
   6.000   0.9854   0.01407   0.00676  -0.0696   0.3744   1.0000
   6.250   1.0048   0.01450   0.00711  -0.0684   0.3536   1.0000
   6.500   1.0229   0.01497   0.00750  -0.0670   0.3337   1.0000
   6.750   1.0402   0.01547   0.00791  -0.0654   0.3158   1.0000
   7.000   1.0569   0.01597   0.00834  -0.0637   0.3000   1.0000
   7.250   1.0727   0.01646   0.00879  -0.0619   0.2858   1.0000
   7.500   1.0881   0.01695   0.00925  -0.0600   0.2728   1.0000
   7.750   1.1034   0.01748   0.00975  -0.0582   0.2606   1.0000
   8.000   1.1184   0.01803   0.01027  -0.0564   0.2493   1.0000
   8.250   1.1326   0.01863   0.01084  -0.0545   0.2380   1.0000
   8.500   1.1480   0.01920   0.01142  -0.0529   0.2264   1.0000
   8.750   1.1629   0.01980   0.01203  -0.0513   0.2155   1.0000
   9.000   1.1767   0.02047   0.01269  -0.0495   0.2053   1.0000
   9.250   1.1895   0.02122   0.01341  -0.0478   0.1949   1.0000
   9.500   1.2036   0.02192   0.01413  -0.0463   0.1845   1.0000
   9.750   1.2165   0.02272   0.01494  -0.0447   0.1751   1.0000
  10.000   1.2281   0.02360   0.01581  -0.0430   0.1662   1.0000
  10.250   1.2420   0.02440   0.01666  -0.0417   0.1581   1.0000
  10.750   1.2662   0.02625   0.01858  -0.0388   0.1432   1.0000
  11.000   1.2765   0.02733   0.01968  -0.0374   0.1354   1.0000
  11.250   1.2872   0.02842   0.02079  -0.0361   0.1259   1.0000
  11.500   1.2979   0.02955   0.02195  -0.0348   0.1179   1.0000
  11.750   1.3056   0.03091   0.02330  -0.0334   0.1099   1.0000
  12.000   1.3155   0.03215   0.02458  -0.0323   0.1012   1.0000
  12.250   1.3234   0.03359   0.02604  -0.0311   0.0936   1.0000
  12.500   1.3299   0.03516   0.02762  -0.0300   0.0859   1.0000
  12.750   1.3376   0.03669   0.02922  -0.0290   0.0790   1.0000
  13.000   1.3422   0.03853   0.03106  -0.0280   0.0730   1.0000
  13.250   1.3493   0.04019   0.03280  -0.0271   0.0677   1.0000
  13.500   1.3534   0.04217   0.03482  -0.0263   0.0630   1.0000
  13.750   1.3580   0.04416   0.03687  -0.0256   0.0585   1.0000
  14.000   1.3623   0.04624   0.03904  -0.0250   0.0550   1.0000
  14.250   1.3637   0.04868   0.04153  -0.0245   0.0515   1.0000
  14.500   1.3674   0.05097   0.04392  -0.0242   0.0489   1.0000
  14.750   1.3704   0.05340   0.04647  -0.0240   0.0463   1.0000
  15.000   1.3711   0.05617   0.04933  -0.0239   0.0437   1.0000
  15.250   1.3697   0.05927   0.05250  -0.0240   0.0416   1.0000
  15.500   1.3715   0.06207   0.05544  -0.0242   0.0395   1.0000
  15.750   1.3715   0.06519   0.05868  -0.0246   0.0378   1.0000
  16.000   1.3692   0.06872   0.06231  -0.0253   0.0356   1.0000
  16.250   1.3649   0.07263   0.06632  -0.0262   0.0341   1.0000
  16.500   1.3623   0.07641   0.07023  -0.0271   0.0321   1.0000
  16.750   1.3589   0.08040   0.07437  -0.0283   0.0305   1.0000
  17.000   1.3524   0.08501   0.07907  -0.0298   0.0283   1.0000
  17.250   1.3435   0.09009   0.08427  -0.0317   0.0270   1.0000
  17.500   1.3378   0.09480   0.08913  -0.0335   0.0254   1.0000
  17.750   1.3302   0.09993   0.09442  -0.0357   0.0239   1.0000
  18.000   1.3186   0.10588   0.10048  -0.0384   0.0218   1.0000
  18.250   1.3075   0.11187   0.10660  -0.0412   0.0207   1.0000
  18.500   1.2974   0.11779   0.11267  -0.0441   0.0196   1.0000
  18.750   1.2857   0.12412   0.11915  -0.0474   0.0185   1.0000
  19.000   1.2733   0.13071   0.12587  -0.0509   0.0178   1.0000
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