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HOBIESMO1.DAT (hobiesm-il) Xfoil prediction polar at RE=50,000 Ncrit=5


Details Polar file
Airfoil: HOBIESMO1.DAT (hobiesm-il)
Reynolds number: 50,000
Max Cl/Cd: 41.46 at α=6.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-hobiesm-il-50000-n5.txt
Download as CSV file: xf-hobiesm-il-50000-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 =     0.050 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
  -8.750  -0.3683   0.09789   0.09094  -0.0346   1.0000   0.0599
  -8.500  -0.3689   0.09457   0.08771  -0.0353   1.0000   0.0594
  -8.250  -0.3711   0.09131   0.08455  -0.0359   1.0000   0.0585
  -8.000  -0.3758   0.08817   0.08152  -0.0362   1.0000   0.0577
  -7.750  -0.3822   0.08502   0.07850  -0.0365   1.0000   0.0569
  -7.500  -0.3866   0.08138   0.07498  -0.0379   1.0000   0.0562
  -7.250  -0.3907   0.07745   0.07116  -0.0398   1.0000   0.0556
  -7.000  -0.3939   0.07318   0.06697  -0.0422   1.0000   0.0550
  -6.750  -0.3960   0.06821   0.06206  -0.0455   1.0000   0.0543
  -6.500  -0.3953   0.06257   0.05640  -0.0493   1.0000   0.0539
  -6.250  -0.3910   0.05597   0.04965  -0.0540   1.0000   0.0536
  -6.000  -0.3821   0.05218   0.04573  -0.0555   1.0000   0.0549
  -5.750  -0.3699   0.04859   0.04194  -0.0574   1.0000   0.0578
  -5.500  -0.3522   0.04292   0.03575  -0.0615   1.0000   0.0609
  -5.250  -0.3295   0.03725   0.02927  -0.0649   1.0000   0.0629
  -5.000  -0.3060   0.03329   0.02461  -0.0665   1.0000   0.0650
  -4.750  -0.2854   0.03150   0.02262  -0.0664   1.0000   0.0680
  -4.500  -0.2622   0.02948   0.02017  -0.0665   1.0000   0.0726
  -4.250  -0.2380   0.02792   0.01825  -0.0666   0.9995   0.0804
  -4.000  -0.2005   0.02674   0.01680  -0.0693   0.9928   0.0957
  -3.750  -0.1630   0.02551   0.01515  -0.0716   0.9859   0.1182
  -3.500  -0.1268   0.02502   0.01460  -0.0740   0.9782   0.1482
  -3.250  -0.0897   0.02459   0.01405  -0.0763   0.9706   0.1777
  -3.000  -0.0552   0.02416   0.01342  -0.0780   0.9620   0.2033
  -2.750  -0.0174   0.02372   0.01283  -0.0801   0.9548   0.2245
  -2.500   0.0175   0.02336   0.01230  -0.0817   0.9459   0.2473
  -2.250   0.0541   0.02301   0.01183  -0.0836   0.9378   0.2714
  -2.000   0.0918   0.02269   0.01143  -0.0856   0.9298   0.3021
  -1.750   0.1256   0.02239   0.01115  -0.0869   0.9205   0.3351
  -1.500   0.1658   0.02203   0.01086  -0.0894   0.9137   0.3809
  -1.250   0.1977   0.02172   0.01067  -0.0903   0.9037   0.4323
  -1.000   0.2316   0.02128   0.01052  -0.0914   0.8950   0.5039
  -0.750   0.2637   0.02052   0.01037  -0.0918   0.8872   0.6403
  -0.500   0.3007   0.01988   0.01007  -0.0929   0.8769   1.0000
  -0.250   0.3355   0.02002   0.00994  -0.0942   0.8672   1.0000
   0.000   0.3722   0.02012   0.00981  -0.0957   0.8583   1.0000
   0.250   0.4018   0.02030   0.00983  -0.0960   0.8466   1.0000
   0.500   0.4321   0.02048   0.00987  -0.0964   0.8354   1.0000
   0.750   0.4635   0.02063   0.00991  -0.0969   0.8247   1.0000
   1.000   0.4977   0.02070   0.00990  -0.0977   0.8154   1.0000
   1.250   0.5253   0.02091   0.01004  -0.0975   0.8030   1.0000
   1.500   0.5531   0.02111   0.01020  -0.0973   0.7908   1.0000
   1.750   0.5810   0.02131   0.01038  -0.0971   0.7787   1.0000
   2.000   0.6092   0.02149   0.01058  -0.0969   0.7668   1.0000
   2.250   0.6376   0.02166   0.01075  -0.0966   0.7550   1.0000
   2.500   0.6664   0.02180   0.01091  -0.0964   0.7433   1.0000
   2.750   0.6948   0.02194   0.01113  -0.0961   0.7314   1.0000
   3.000   0.7210   0.02217   0.01141  -0.0955   0.7182   1.0000
   3.250   0.7471   0.02240   0.01171  -0.0948   0.7049   1.0000
   3.500   0.7732   0.02263   0.01203  -0.0942   0.6914   1.0000
   3.750   0.7992   0.02286   0.01241  -0.0935   0.6778   1.0000
   4.000   0.8253   0.02309   0.01276  -0.0928   0.6639   1.0000
   4.250   0.8512   0.02333   0.01314  -0.0920   0.6498   1.0000
   4.500   0.8771   0.02358   0.01353  -0.0912   0.6354   1.0000
   4.750   0.9030   0.02384   0.01401  -0.0904   0.6208   1.0000
   5.000   0.9288   0.02411   0.01446  -0.0896   0.6059   1.0000
   5.250   0.9541   0.02442   0.01497  -0.0887   0.5907   1.0000
   5.500   0.9778   0.02484   0.01564  -0.0876   0.5744   1.0000
   5.750   0.9998   0.02480   0.01572  -0.0854   0.5467   1.0000
   6.000   1.0133   0.02446   0.01522  -0.0813   0.4922   1.0000
   6.250   1.0258   0.02474   0.01551  -0.0780   0.4380   1.0000
   6.500   1.0343   0.02542   0.01596  -0.0743   0.3600   1.0000
   6.750   1.0308   0.02750   0.01692  -0.0699   0.2013   1.0000
   7.000   1.0234   0.03103   0.01921  -0.0666   0.0803   1.0000
   7.250   1.0292   0.03329   0.02135  -0.0641   0.0654   1.0000
   7.500   1.0328   0.03549   0.02357  -0.0615   0.0575   1.0000
   7.750   1.0382   0.03733   0.02557  -0.0590   0.0515   1.0000
   8.000   1.0412   0.03941   0.02777  -0.0566   0.0477   1.0000
   8.250   1.0421   0.04180   0.03025  -0.0543   0.0456   1.0000
   8.500   1.0495   0.04380   0.03244  -0.0522   0.0439   1.0000
   8.750   1.0612   0.04571   0.03458  -0.0504   0.0421   1.0000
   9.000   1.0778   0.04758   0.03672  -0.0488   0.0391   1.0000
   9.250   1.0977   0.04966   0.03889  -0.0476   0.0358   1.0000
   9.500   1.1444   0.05283   0.04214  -0.0481   0.0334   1.0000
   9.750   1.1703   0.05582   0.04554  -0.0475   0.0327   1.0000
  10.000   1.1863   0.05905   0.04917  -0.0464   0.0322   1.0000
  10.250   1.1932   0.06230   0.05281  -0.0446   0.0319   1.0000
  10.500   1.1933   0.06556   0.05643  -0.0427   0.0315   1.0000
  10.750   1.1883   0.06894   0.06015  -0.0408   0.0311   1.0000
  11.000   1.1799   0.07253   0.06406  -0.0394   0.0307   1.0000
  11.250   1.1683   0.07644   0.06828  -0.0385   0.0305   1.0000
  11.500   1.1552   0.08071   0.07282  -0.0383   0.0304   1.0000
  11.750   1.1400   0.08544   0.07781  -0.0389   0.0304   1.0000
  12.000   1.1235   0.09064   0.08325  -0.0403   0.0304   1.0000
  12.250   1.1058   0.09642   0.08924  -0.0425   0.0306   1.0000
  12.500   1.0878   0.10275   0.09576  -0.0456   0.0309   1.0000
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