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Rhode St. Genese 32 (rhodesg32-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: Rhode St. Genese 32 (rhodesg32-il)
Reynolds number: 200,000
Max Cl/Cd: 64.28 at α=8.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-rhodesg32-il-200000.txt
Download as CSV file: xf-rhodesg32-il-200000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: Rhode St. Genese 32                             
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -10.250  -0.3529   0.09031   0.08695  -0.0333   1.0000   0.0723
 -10.000  -0.3705   0.08901   0.08572  -0.0305   1.0000   0.0733
  -9.750  -0.4006   0.07937   0.07600  -0.0550   0.9864   0.0779
  -9.500  -0.3798   0.07442   0.07111  -0.0555   0.9837   0.0791
  -9.250  -0.3518   0.07321   0.06992  -0.0531   0.9813   0.0806
  -9.000  -0.3293   0.07038   0.06707  -0.0557   0.9751   0.0834
  -8.750  -0.3231   0.06033   0.05670  -0.0720   0.9628   0.0914
  -8.500  -0.2929   0.05842   0.05485  -0.0726   0.9594   0.0932
  -8.250  -0.2596   0.05546   0.05182  -0.0766   0.9562   0.0978
  -8.000  -0.1706   0.03679   0.03327  -0.0848   0.9412   0.1100
  -7.750  -0.1655   0.03169   0.02787  -0.0882   0.9299   0.1188
  -7.500  -0.1354   0.02940   0.02560  -0.0894   0.9256   0.1224
  -7.250  -0.1264   0.02590   0.02176  -0.0904   0.9141   0.1329
  -7.000  -0.1262   0.03907   0.03462  -0.0927   0.9249   0.1351
  -6.750  -0.1093   0.03740   0.03258  -0.0924   0.9138   0.1477
  -6.500  -0.0928   0.02508   0.01871  -0.0919   0.9068   0.0862
  -6.250  -0.0706   0.02319   0.01652  -0.0907   0.8975   0.0854
  -6.000  -0.0386   0.02133   0.01431  -0.0912   0.8921   0.0847
  -5.750  -0.0166   0.02009   0.01282  -0.0897   0.8815   0.0843
  -5.500   0.0148   0.01889   0.01140  -0.0898   0.8751   0.0847
  -5.250   0.0380   0.01814   0.01053  -0.0885   0.8639   0.0861
  -5.000   0.0654   0.01738   0.00962  -0.0879   0.8546   0.0876
  -4.750   0.0927   0.01663   0.00874  -0.0871   0.8441   0.0886
  -4.500   0.1177   0.01601   0.00804  -0.0860   0.8321   0.0895
  -4.250   0.1445   0.01533   0.00729  -0.0853   0.8220   0.0906
  -4.000   0.1698   0.01458   0.00657  -0.0845   0.8109   0.0933
  -3.750   0.1944   0.01414   0.00616  -0.0835   0.7987   0.0963
  -3.500   0.2199   0.01373   0.00572  -0.0826   0.7865   0.0992
  -3.250   0.2456   0.01336   0.00530  -0.0817   0.7734   0.1020
  -3.000   0.2705   0.01296   0.00490  -0.0807   0.7587   0.1061
  -2.750   0.2953   0.01270   0.00463  -0.0797   0.7416   0.1128
  -2.500   0.3197   0.01246   0.00441  -0.0786   0.7219   0.1230
  -2.250   0.3439   0.01224   0.00418  -0.0775   0.6987   0.1447
  -2.000   0.3657   0.01182   0.00393  -0.0760   0.6704   0.2113
  -1.750   0.3797   0.01087   0.00383  -0.0734   0.6361   0.4849
  -1.500   0.4513   0.01022   0.00402  -0.0809   0.5533   0.9681
  -1.250   0.5062   0.01081   0.00400  -0.0866   0.4788   1.0000
  -1.000   0.5238   0.01116   0.00406  -0.0847   0.4546   1.0000
  -0.750   0.5433   0.01145   0.00414  -0.0831   0.4405   1.0000
  -0.500   0.5637   0.01175   0.00424  -0.0817   0.4311   1.0000
  -0.250   0.5855   0.01199   0.00436  -0.0805   0.4237   1.0000
   0.000   0.6074   0.01228   0.00450  -0.0793   0.4181   1.0000
   0.250   0.6304   0.01253   0.00464  -0.0784   0.4134   1.0000
   0.500   0.6538   0.01276   0.00480  -0.0776   0.4092   1.0000
   0.750   0.6775   0.01302   0.00498  -0.0768   0.4055   1.0000
   1.000   0.7016   0.01333   0.00517  -0.0761   0.4020   1.0000
   1.250   0.7258   0.01362   0.00539  -0.0754   0.3984   1.0000
   1.500   0.7496   0.01384   0.00560  -0.0747   0.3943   1.0000
   1.750   0.7737   0.01410   0.00581  -0.0740   0.3904   1.0000
   2.000   0.7981   0.01440   0.00604  -0.0734   0.3868   1.0000
   2.250   0.8239   0.01482   0.00635  -0.0732   0.3837   1.0000
   2.500   0.8483   0.01505   0.00662  -0.0726   0.3815   1.0000
   2.750   0.8731   0.01531   0.00691  -0.0721   0.3795   1.0000
   3.000   0.8981   0.01560   0.00722  -0.0716   0.3773   1.0000
   3.250   0.9230   0.01589   0.00752  -0.0712   0.3747   1.0000
   3.500   0.9482   0.01621   0.00783  -0.0708   0.3720   1.0000
   3.750   0.9740   0.01658   0.00818  -0.0706   0.3697   1.0000
   4.000   1.0012   0.01708   0.00863  -0.0708   0.3673   1.0000
   4.250   1.0251   0.01736   0.00900  -0.0702   0.3653   1.0000
   4.500   1.0483   0.01761   0.00936  -0.0695   0.3621   1.0000
   4.750   1.0716   0.01788   0.00967  -0.0688   0.3579   1.0000
   5.000   1.0961   0.01820   0.00995  -0.0684   0.3531   1.0000
   5.250   1.1205   0.01863   0.01039  -0.0680   0.3489   1.0000
   5.500   1.1424   0.01887   0.01077  -0.0671   0.3454   1.0000
   5.750   1.1651   0.01914   0.01111  -0.0664   0.3414   1.0000
   6.000   1.1890   0.01943   0.01140  -0.0660   0.3368   1.0000
   6.250   1.2125   0.01983   0.01183  -0.0655   0.3321   1.0000
   6.500   1.2321   0.02003   0.01219  -0.0642   0.3275   1.0000
   6.750   1.2533   0.02023   0.01245  -0.0633   0.3222   1.0000
   7.000   1.2777   0.02063   0.01279  -0.0630   0.3167   1.0000
   7.250   1.2933   0.02072   0.01312  -0.0610   0.3111   1.0000
   7.500   1.3117   0.02085   0.01332  -0.0596   0.3047   1.0000
   7.750   1.3305   0.02108   0.01359  -0.0583   0.2984   1.0000
   8.000   1.3427   0.02111   0.01380  -0.0557   0.2901   1.0000
   8.250   1.3567   0.02123   0.01395  -0.0536   0.2823   1.0000
   8.500   1.3667   0.02128   0.01420  -0.0507   0.2727   1.0000
   8.750   1.3737   0.02137   0.01442  -0.0472   0.2610   1.0000
   9.000   1.3803   0.02152   0.01469  -0.0439   0.2438   1.0000
   9.250   1.3821   0.02193   0.01502  -0.0402   0.2010   1.0000
   9.500   1.3708   0.02343   0.01615  -0.0354   0.1682   1.0000
   9.750   1.3647   0.02520   0.01781  -0.0319   0.1505   1.0000
  10.000   1.3613   0.02697   0.01956  -0.0289   0.1356   1.0000
  10.250   1.3581   0.02884   0.02142  -0.0263   0.1206   1.0000
  10.500   1.3551   0.03084   0.02340  -0.0241   0.1056   1.0000
  10.750   1.3522   0.03295   0.02549  -0.0221   0.0917   1.0000
  11.000   1.3497   0.03517   0.02770  -0.0206   0.0812   1.0000
  11.250   1.3461   0.03762   0.03016  -0.0192   0.0753   1.0000
  11.500   1.3387   0.04056   0.03311  -0.0181   0.0711   1.0000
  11.750   1.3323   0.04360   0.03622  -0.0173   0.0680   1.0000
  12.000   1.3253   0.04687   0.03957  -0.0168   0.0654   1.0000
  12.250   1.3152   0.05063   0.04338  -0.0166   0.0633   1.0000
  12.500   1.3033   0.05473   0.04751  -0.0166   0.0613   1.0000
  12.750   1.2984   0.05820   0.05108  -0.0167   0.0596   1.0000
  13.000   1.2939   0.06172   0.05470  -0.0170   0.0577   1.0000
  13.250   1.2885   0.06538   0.05843  -0.0174   0.0557   1.0000
  13.500   1.2847   0.06873   0.06178  -0.0176   0.0539   1.0000
  13.750   1.2867   0.07108   0.06408  -0.0169   0.0518   1.0000
  14.000   1.2876   0.07414   0.06728  -0.0173   0.0502   1.0000
  14.250   1.2891   0.07704   0.07026  -0.0176   0.0483   1.0000
  14.500   1.2943   0.07927   0.07248  -0.0175   0.0465   1.0000
  14.750   1.3107   0.07957   0.07266  -0.0156   0.0442   1.0000
  15.000   1.3104   0.08297   0.07624  -0.0165   0.0431   1.0000
  15.250   1.3133   0.08587   0.07928  -0.0170   0.0418   1.0000
  15.500   1.3163   0.08874   0.08225  -0.0175   0.0405   1.0000
  15.750   1.3215   0.09123   0.08477  -0.0179   0.0393   1.0000
  16.000   1.3406   0.09160   0.08504  -0.0163   0.0374   1.0000
  16.250   1.3334   0.09613   0.08981  -0.0181   0.0369   1.0000
  16.500   1.3258   0.10085   0.09474  -0.0201   0.0362   1.0000
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