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HOBIE (hobie-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: HOBIE (hobie-il)
Reynolds number: 1,000,000
Max Cl/Cd: 102.74 at α=4.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-hobie-il-1000000-n5.txt
Download as CSV file: xf-hobie-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: HOBIE                                           
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -12.250  -0.5532   0.09882   0.09699  -0.0309   1.0000   0.0059
 -12.000  -0.5560   0.09441   0.09258  -0.0330   1.0000   0.0060
 -11.500  -0.8225   0.02822   0.02558  -0.0867   0.9983   0.0048
 -11.250  -0.7979   0.02483   0.02191  -0.0905   0.9959   0.0050
 -11.000  -0.7716   0.02267   0.01953  -0.0928   0.9939   0.0052
 -10.750  -0.7454   0.02098   0.01763  -0.0944   0.9914   0.0053
 -10.500  -0.7172   0.01958   0.01606  -0.0959   0.9891   0.0055
 -10.250  -0.6872   0.01840   0.01471  -0.0974   0.9871   0.0056
 -10.000  -0.6589   0.01699   0.01313  -0.0988   0.9845   0.0059
  -9.750  -0.6306   0.01598   0.01200  -0.0997   0.9811   0.0062
  -9.500  -0.5996   0.01513   0.01103  -0.1010   0.9785   0.0065
  -9.250  -0.5692   0.01437   0.01016  -0.1020   0.9753   0.0068
  -9.000  -0.5402   0.01370   0.00936  -0.1027   0.9708   0.0071
  -8.750  -0.5090   0.01309   0.00864  -0.1037   0.9675   0.0074
  -8.500  -0.4804   0.01244   0.00789  -0.1042   0.9621   0.0078
  -8.250  -0.4498   0.01184   0.00721  -0.1051   0.9568   0.0084
  -8.000  -0.4208   0.01137   0.00667  -0.1055   0.9488   0.0090
  -7.750  -0.3914   0.01096   0.00615  -0.1059   0.9391   0.0097
  -7.500  -0.3631   0.01052   0.00561  -0.1060   0.9255   0.0104
  -7.250  -0.3359   0.01014   0.00513  -0.1059   0.9083   0.0113
  -7.000  -0.3093   0.00985   0.00472  -0.1056   0.8893   0.0123
  -6.750  -0.2832   0.00956   0.00431  -0.1052   0.8706   0.0136
  -6.500  -0.2570   0.00928   0.00394  -0.1048   0.8534   0.0155
  -6.250  -0.2307   0.00901   0.00359  -0.1045   0.8384   0.0183
  -6.000  -0.2043   0.00879   0.00329  -0.1042   0.8229   0.0218
  -5.750  -0.1778   0.00865   0.00313  -0.1038   0.8056   0.0276
  -5.500  -0.1509   0.00869   0.00317  -0.1035   0.7881   0.0342
  -5.250  -0.1238   0.00871   0.00312  -0.1032   0.7728   0.0372
  -5.000  -0.0966   0.00873   0.00305  -0.1029   0.7583   0.0388
  -4.750  -0.0693   0.00878   0.00303  -0.1027   0.7447   0.0395
  -4.500  -0.0419   0.00882   0.00301  -0.1025   0.7327   0.0399
  -4.250  -0.0150   0.00856   0.00266  -0.1022   0.7211   0.0414
  -4.000   0.0123   0.00843   0.00247  -0.1020   0.7101   0.0430
  -3.750   0.0396   0.00838   0.00237  -0.1019   0.6992   0.0446
  -3.500   0.0672   0.00830   0.00225  -0.1017   0.6891   0.0456
  -3.250   0.0947   0.00817   0.00207  -0.1015   0.6806   0.0462
  -3.000   0.1221   0.00807   0.00189  -0.1013   0.6708   0.0468
  -2.750   0.1495   0.00799   0.00175  -0.1012   0.6580   0.0478
  -2.500   0.1766   0.00792   0.00160  -0.1009   0.6407   0.0486
  -2.250   0.2036   0.00789   0.00148  -0.1006   0.6208   0.0496
  -2.000   0.2306   0.00789   0.00138  -0.1004   0.5991   0.0506
  -1.750   0.2575   0.00791   0.00130  -0.1001   0.5782   0.0514
  -1.500   0.2846   0.00794   0.00126  -0.0999   0.5589   0.0521
  -1.250   0.3116   0.00798   0.00122  -0.0996   0.5398   0.0526
  -1.000   0.3386   0.00803   0.00119  -0.0994   0.5205   0.0528
  -0.750   0.3655   0.00807   0.00114  -0.0992   0.5008   0.0537
  -0.500   0.3924   0.00811   0.00110  -0.0989   0.4806   0.0549
  -0.250   0.4193   0.00817   0.00108  -0.0987   0.4592   0.0559
   0.000   0.4463   0.00823   0.00107  -0.0984   0.4424   0.0570
   0.250   0.4735   0.00827   0.00107  -0.0982   0.4314   0.0581
   0.500   0.5007   0.00832   0.00108  -0.0980   0.4220   0.0592
   0.750   0.5280   0.00836   0.00110  -0.0979   0.4132   0.0605
   1.000   0.5550   0.00844   0.00114  -0.0976   0.4010   0.0622
   1.250   0.5820   0.00850   0.00119  -0.0974   0.3900   0.0644
   1.750   0.6359   0.00834   0.00130  -0.0972   0.3684   0.1965
   2.000   0.6626   0.00840   0.00139  -0.0969   0.3503   0.2339
   2.250   0.6882   0.00859   0.00150  -0.0966   0.3198   0.2530
   2.500   0.7132   0.00886   0.00166  -0.0961   0.2822   0.2705
   2.750   0.7363   0.00925   0.00195  -0.0954   0.2219   0.3395
   3.000   0.7627   0.00935   0.00209  -0.0951   0.2145   0.3683
   3.250   0.7890   0.00944   0.00224  -0.0949   0.2081   0.3991
   3.500   0.8154   0.00938   0.00240  -0.0947   0.2048   0.4858
   3.750   0.8400   0.00908   0.00262  -0.0942   0.2013   0.6978
   4.000   0.8690   0.00864   0.00279  -0.0944   0.1973   1.0000
   4.250   0.8953   0.00881   0.00296  -0.0941   0.1921   1.0000
   4.500   0.9215   0.00900   0.00312  -0.0938   0.1822   1.0000
   4.750   0.9473   0.00922   0.00329  -0.0934   0.1676   1.0000
   5.000   0.9654   0.01028   0.00385  -0.0920   0.0723   1.0000
   5.250   0.9901   0.01061   0.00414  -0.0914   0.0613   1.0000
   5.500   1.0152   0.01089   0.00440  -0.0909   0.0547   1.0000
   5.750   1.0406   0.01112   0.00464  -0.0905   0.0508   1.0000
   6.000   1.0650   0.01145   0.00494  -0.0899   0.0422   1.0000
   6.250   1.0896   0.01176   0.00522  -0.0894   0.0343   1.0000
   6.500   1.1130   0.01218   0.00557  -0.0887   0.0241   1.0000
   6.750   1.1368   0.01254   0.00591  -0.0880   0.0190   1.0000
   7.000   1.1603   0.01293   0.00629  -0.0873   0.0158   1.0000
   7.250   1.1839   0.01330   0.00665  -0.0866   0.0137   1.0000
   7.500   1.2070   0.01369   0.00706  -0.0859   0.0119   1.0000
   7.750   1.2300   0.01408   0.00747  -0.0852   0.0107   1.0000
   8.000   1.2524   0.01452   0.00791  -0.0843   0.0096   1.0000
   8.250   1.2750   0.01491   0.00835  -0.0835   0.0089   1.0000
   8.500   1.2970   0.01535   0.00882  -0.0826   0.0082   1.0000
   8.750   1.3180   0.01586   0.00934  -0.0816   0.0075   1.0000
   9.000   1.3391   0.01632   0.00985  -0.0806   0.0070   1.0000
   9.250   1.3599   0.01679   0.01036  -0.0795   0.0066   1.0000
   9.500   1.3798   0.01731   0.01092  -0.0783   0.0062   1.0000
   9.750   1.3988   0.01787   0.01153  -0.0770   0.0059   1.0000
  10.000   1.4158   0.01856   0.01226  -0.0754   0.0055   1.0000
  10.250   1.4334   0.01914   0.01290  -0.0739   0.0054   1.0000
  10.500   1.4499   0.01974   0.01357  -0.0723   0.0051   1.0000
  10.750   1.4635   0.02037   0.01425  -0.0701   0.0049   1.0000
  11.000   1.4755   0.02103   0.01497  -0.0677   0.0048   1.0000
  11.250   1.4874   0.02169   0.01569  -0.0654   0.0046   1.0000
  11.500   1.4981   0.02245   0.01650  -0.0630   0.0044   1.0000
  11.750   1.5071   0.02334   0.01747  -0.0606   0.0042   1.0000
  12.000   1.5129   0.02448   0.01868  -0.0579   0.0040   1.0000
  12.250   1.5211   0.02551   0.01980  -0.0557   0.0040   1.0000
  12.500   1.5288   0.02662   0.02100  -0.0537   0.0039   1.0000
  12.750   1.5351   0.02790   0.02236  -0.0516   0.0038   1.0000
  13.000   1.5413   0.02926   0.02381  -0.0498   0.0037   1.0000
  13.250   1.5460   0.03082   0.02546  -0.0481   0.0036   1.0000
  13.500   1.5507   0.03247   0.02720  -0.0466   0.0035   1.0000
  13.750   1.5542   0.03432   0.02915  -0.0453   0.0034   1.0000
  14.000   1.5564   0.03639   0.03132  -0.0441   0.0034   1.0000
  14.250   1.5593   0.03850   0.03352  -0.0432   0.0033   1.0000
  14.500   1.5602   0.04092   0.03605  -0.0425   0.0032   1.0000
  14.750   1.5599   0.04357   0.03880  -0.0420   0.0032   1.0000
  15.000   1.5587   0.04646   0.04179  -0.0417   0.0032   1.0000
  15.250   1.5572   0.04949   0.04493  -0.0417   0.0031   1.0000
  15.500   1.5537   0.05292   0.04846  -0.0419   0.0030   1.0000
  15.750   1.5501   0.05652   0.05219  -0.0424   0.0030   1.0000
  16.000   1.5439   0.06065   0.05644  -0.0433   0.0030   1.0000
  16.250   1.5365   0.06516   0.06107  -0.0445   0.0029   1.0000
  16.500   1.5268   0.07024   0.06628  -0.0461   0.0029   1.0000
  16.750   1.5159   0.07572   0.07188  -0.0481   0.0028   1.0000
  17.000   1.5037   0.08164   0.07794  -0.0505   0.0028   1.0000
  17.250   1.4896   0.08814   0.08457  -0.0533   0.0028   1.0000
  17.500   1.4772   0.09446   0.09103  -0.0562   0.0028   1.0000
  17.750   1.4642   0.10107   0.09777  -0.0593   0.0028   1.0000
  18.000   1.4499   0.10815   0.10498  -0.0628   0.0028   1.0000
  18.250   1.4348   0.11554   0.11251  -0.0666   0.0028   1.0000
  18.500   1.4203   0.12302   0.12012  -0.0706   0.0028   1.0000
  18.750   1.4062   0.13063   0.12786  -0.0749   0.0028   1.0000
  19.000   1.3912   0.13862   0.13598  -0.0795   0.0027   1.0000
  19.250   1.3765   0.14675   0.14424  -0.0843   0.0027   1.0000
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