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HOBIESMO1.DAT (hobiesm-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: HOBIESMO1.DAT (hobiesm-il)
Reynolds number: 500,000
Max Cl/Cd: 101.89 at α=3.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-hobiesm-il-500000-n5.txt
Download as CSV file: xf-hobiesm-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: HOBIESMO1.DAT                                   
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -10.250  -0.4194   0.09630   0.09402  -0.0310   1.0000   0.0071
 -10.000  -0.4308   0.08954   0.08731  -0.0336   1.0000   0.0075
  -9.500  -0.6170   0.02867   0.02575  -0.0841   0.9919   0.0065
  -9.250  -0.5891   0.02533   0.02203  -0.0883   0.9865   0.0069
  -9.000  -0.5595   0.02261   0.01894  -0.0915   0.9821   0.0073
  -8.750  -0.5324   0.02062   0.01663  -0.0931   0.9754   0.0078
  -8.500  -0.5011   0.01902   0.01473  -0.0951   0.9710   0.0083
  -8.250  -0.4719   0.01738   0.01284  -0.0966   0.9649   0.0089
  -8.000  -0.4400   0.01673   0.01210  -0.0980   0.9590   0.0096
  -7.750  -0.4075   0.01620   0.01148  -0.0994   0.9528   0.0105
  -7.500  -0.3753   0.01552   0.01063  -0.1007   0.9451   0.0116
  -7.250  -0.3436   0.01476   0.00968  -0.1019   0.9365   0.0125
  -7.000  -0.3120   0.01422   0.00898  -0.1028   0.9272   0.0131
  -6.750  -0.2842   0.01303   0.00758  -0.1033   0.9157   0.0144
  -6.500  -0.2564   0.01251   0.00696  -0.1035   0.9045   0.0157
  -6.250  -0.2289   0.01207   0.00640  -0.1035   0.8938   0.0169
  -6.000  -0.2019   0.01163   0.00580  -0.1034   0.8837   0.0179
  -5.750  -0.1750   0.01127   0.00531  -0.1032   0.8736   0.0190
  -5.500  -0.1481   0.01098   0.00490  -0.1030   0.8640   0.0197
  -5.250  -0.1213   0.01058   0.00437  -0.1027   0.8550   0.0204
  -5.000  -0.0945   0.01017   0.00382  -0.1025   0.8459   0.0216
  -4.750  -0.0675   0.00986   0.00339  -0.1022   0.8373   0.0231
  -4.500  -0.0405   0.00961   0.00307  -0.1020   0.8290   0.0254
  -4.250  -0.0133   0.00939   0.00277  -0.1018   0.8202   0.0282
  -4.000   0.0138   0.00913   0.00248  -0.1016   0.8119   0.0375
  -3.750   0.0407   0.00883   0.00225  -0.1014   0.8032   0.0626
  -3.500   0.0679   0.00867   0.00208  -0.1012   0.7947   0.0796
  -3.250   0.0952   0.00857   0.00194  -0.1010   0.7862   0.0908
  -3.000   0.1225   0.00846   0.00182  -0.1009   0.7771   0.1016
  -2.750   0.1498   0.00836   0.00171  -0.1007   0.7683   0.1127
  -2.250   0.2043   0.00817   0.00151  -0.1003   0.7494   0.1400
  -2.000   0.2315   0.00808   0.00143  -0.1002   0.7398   0.1579
  -1.750   0.2587   0.00801   0.00135  -0.1000   0.7298   0.1752
  -1.500   0.2859   0.00794   0.00129  -0.0998   0.7189   0.1922
  -1.250   0.3131   0.00788   0.00125  -0.0996   0.7079   0.2139
  -1.000   0.3402   0.00783   0.00121  -0.0994   0.6965   0.2349
  -0.750   0.3672   0.00781   0.00119  -0.0992   0.6848   0.2559
  -0.500   0.3942   0.00779   0.00118  -0.0989   0.6723   0.2769
  -0.250   0.4212   0.00778   0.00118  -0.0987   0.6597   0.2997
   0.000   0.4480   0.00777   0.00119  -0.0985   0.6465   0.3258
   0.250   0.4748   0.00777   0.00121  -0.0982   0.6330   0.3518
   1.250   0.5803   0.00763   0.00144  -0.0971   0.5780   0.5426
   1.500   0.6031   0.00725   0.00157  -0.0961   0.5648   0.7278
   1.750   0.6381   0.00686   0.00163  -0.0974   0.5507   1.0000
   2.000   0.6647   0.00700   0.00170  -0.0971   0.5375   1.0000
   2.250   0.6912   0.00714   0.00179  -0.0968   0.5243   1.0000
   2.500   0.7176   0.00729   0.00191  -0.0965   0.5112   1.0000
   2.750   0.7440   0.00744   0.00202  -0.0961   0.4982   1.0000
   3.000   0.7703   0.00760   0.00215  -0.0958   0.4852   1.0000
   3.250   0.7959   0.00782   0.00230  -0.0954   0.4655   1.0000
   3.500   0.8212   0.00806   0.00246  -0.0949   0.4408   1.0000
   3.750   0.8462   0.00833   0.00263  -0.0944   0.4139   1.0000
   4.000   0.8708   0.00864   0.00284  -0.0938   0.3845   1.0000
   4.250   0.8930   0.00918   0.00311  -0.0929   0.3299   1.0000
   4.500   0.9136   0.00992   0.00352  -0.0918   0.2599   1.0000
   4.750   0.9325   0.01087   0.00404  -0.0906   0.1781   1.0000
   5.000   0.9441   0.01266   0.00507  -0.0883   0.0345   1.0000
   5.250   0.9676   0.01312   0.00550  -0.0876   0.0224   1.0000
   5.500   0.9912   0.01354   0.00592  -0.0869   0.0177   1.0000
   5.750   1.0146   0.01400   0.00643  -0.0861   0.0147   1.0000
   6.000   1.0380   0.01442   0.00692  -0.0854   0.0127   1.0000
   6.250   1.0604   0.01493   0.00745  -0.0846   0.0107   1.0000
   6.500   1.0815   0.01558   0.00817  -0.0834   0.0095   1.0000
   6.750   1.1031   0.01614   0.00880  -0.0824   0.0089   1.0000
   7.000   1.1238   0.01677   0.00950  -0.0813   0.0083   1.0000
   7.250   1.1436   0.01744   0.01024  -0.0801   0.0077   1.0000
   7.500   1.1627   0.01815   0.01104  -0.0787   0.0072   1.0000
   7.750   1.1813   0.01886   0.01179  -0.0774   0.0066   1.0000
   8.000   1.1932   0.02012   0.01315  -0.0750   0.0060   1.0000
   8.250   1.2100   0.02090   0.01400  -0.0734   0.0057   1.0000
   8.500   1.2249   0.02181   0.01500  -0.0715   0.0055   1.0000
   8.750   1.2372   0.02285   0.01615  -0.0693   0.0053   1.0000
   9.000   1.2477   0.02386   0.01726  -0.0667   0.0051   1.0000
   9.250   1.2571   0.02498   0.01848  -0.0640   0.0049   1.0000
   9.500   1.2659   0.02622   0.01984  -0.0615   0.0047   1.0000
   9.750   1.2749   0.02751   0.02126  -0.0591   0.0045   1.0000
  10.000   1.2841   0.02879   0.02264  -0.0569   0.0043   1.0000
  10.250   1.2922   0.03030   0.02429  -0.0548   0.0042   1.0000
  10.500   1.3003   0.03176   0.02586  -0.0528   0.0041   1.0000
  10.750   1.3074   0.03334   0.02756  -0.0509   0.0040   1.0000
  11.000   1.3134   0.03514   0.02950  -0.0491   0.0039   1.0000
  11.250   1.3180   0.03706   0.03156  -0.0474   0.0038   1.0000
  11.500   1.3210   0.03924   0.03389  -0.0458   0.0037   1.0000
  11.750   1.3209   0.04194   0.03677  -0.0442   0.0036   1.0000
  12.000   1.3178   0.04510   0.04014  -0.0427   0.0036   1.0000
  12.250   1.3113   0.04874   0.04402  -0.0415   0.0035   1.0000
  12.500   1.2984   0.05338   0.04894  -0.0406   0.0035   1.0000
  12.750   1.2891   0.05750   0.05327  -0.0404   0.0034   1.0000
  13.000   1.2794   0.06181   0.05780  -0.0406   0.0034   1.0000
  13.250   1.2695   0.06635   0.06255  -0.0414   0.0034   1.0000
  13.500   1.2540   0.07206   0.06847  -0.0430   0.0034   1.0000
  13.750   1.2436   0.07722   0.07382  -0.0448   0.0033   1.0000
  14.000   1.2243   0.08437   0.08117  -0.0479   0.0033   1.0000
  14.250   1.2068   0.09166   0.08865  -0.0514   0.0033   1.0000
  14.500   1.1879   0.09977   0.09695  -0.0558   0.0033   1.0000
  14.750   1.1674   0.10881   0.10615  -0.0611   0.0034   1.0000
  15.000   1.1480   0.11831   0.11581  -0.0668   0.0034   1.0000
  15.250   1.1265   0.12898   0.12662  -0.0734   0.0034   1.0000
  15.500   1.1062   0.14033   0.13810  -0.0804   0.0034   1.0000
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