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Rhode St. Genese 32 (rhodesg32-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: Rhode St. Genese 32 (rhodesg32-il)
Reynolds number: 200,000
Max Cl/Cd: 64.93 at α=7.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-rhodesg32-il-200000-n5.txt
Download as CSV file: xf-rhodesg32-il-200000-n5.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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.250  -0.3477   0.10052   0.09669  -0.0420   1.0000   0.0362
 -12.000  -0.3621   0.09448   0.09070  -0.0449   1.0000   0.0370
 -11.750  -0.3735   0.08951   0.08578  -0.0467   1.0000   0.0376
 -11.500  -0.3729   0.08744   0.08376  -0.0462   1.0000   0.0378
 -11.250  -0.3692   0.08644   0.08281  -0.0448   1.0000   0.0384
 -11.000  -0.3647   0.08393   0.08034  -0.0459   0.9979   0.0392
 -10.750  -0.3543   0.07932   0.07573  -0.0511   0.9877   0.0402
 -10.500  -0.3515   0.07310   0.06951  -0.0583   0.9761   0.0409
 -10.250  -0.3561   0.06325   0.05960  -0.0719   0.9610   0.0414
 -10.000  -0.4098   0.03791   0.03296  -0.0916   0.9404   0.0438
  -9.750  -0.3884   0.03573   0.03061  -0.0926   0.9329   0.0444
  -9.500  -0.3619   0.03411   0.02886  -0.0938   0.9267   0.0450
  -9.250  -0.3403   0.03260   0.02720  -0.0939   0.9184   0.0458
  -9.000  -0.3153   0.03078   0.02513  -0.0947   0.9125   0.0469
  -8.750  -0.2980   0.02877   0.02279  -0.0939   0.9030   0.0478
  -8.250  -0.2561   0.02513   0.01843  -0.0927   0.8862   0.0493
  -8.000  -0.2321   0.02381   0.01675  -0.0922   0.8787   0.0503
  -7.750  -0.2102   0.02296   0.01557  -0.0911   0.8692   0.0511
  -7.500  -0.1865   0.02161   0.01405  -0.0905   0.8607   0.0519
  -7.250  -0.1627   0.02065   0.01299  -0.0898   0.8514   0.0526
  -7.000  -0.1379   0.01986   0.01209  -0.0892   0.8431   0.0532
  -6.750  -0.1128   0.01915   0.01125  -0.0885   0.8340   0.0539
  -6.500  -0.0881   0.01849   0.01048  -0.0878   0.8238   0.0547
  -6.250  -0.0621   0.01792   0.00978  -0.0872   0.8142   0.0558
  -6.000  -0.0371   0.01740   0.00916  -0.0865   0.8033   0.0571
  -5.750  -0.0115   0.01689   0.00853  -0.0858   0.7916   0.0582
  -5.500   0.0143   0.01639   0.00791  -0.0851   0.7785   0.0590
  -5.250   0.0403   0.01595   0.00735  -0.0844   0.7649   0.0598
  -5.000   0.0660   0.01558   0.00686  -0.0837   0.7497   0.0605
  -4.750   0.0908   0.01499   0.00623  -0.0829   0.7328   0.0615
  -4.500   0.1153   0.01456   0.00575  -0.0821   0.7135   0.0630
  -4.250   0.1400   0.01426   0.00539  -0.0812   0.6936   0.0648
  -4.000   0.1647   0.01402   0.00506  -0.0804   0.6747   0.0664
  -3.750   0.1892   0.01381   0.00475  -0.0795   0.6552   0.0678
  -3.500   0.2135   0.01365   0.00447  -0.0786   0.6341   0.0692
  -3.250   0.2376   0.01354   0.00424  -0.0777   0.6100   0.0705
  -3.000   0.2608   0.01345   0.00401  -0.0766   0.5818   0.0723
  -2.750   0.2831   0.01337   0.00380  -0.0754   0.5437   0.0753
  -2.500   0.3034   0.01350   0.00365  -0.0738   0.4875   0.0784
  -2.250   0.3232   0.01373   0.00358  -0.0722   0.4376   0.0814
  -2.000   0.3450   0.01386   0.00355  -0.0710   0.4103   0.0855
  -1.750   0.3678   0.01390   0.00355  -0.0700   0.3945   0.0938
  -1.500   0.3908   0.01387   0.00364  -0.0692   0.3840   0.1419
  -1.250   0.4142   0.01388   0.00368  -0.0683   0.3759   0.1782
  -1.000   0.4373   0.01380   0.00374  -0.0675   0.3700   0.2300
  -0.750   0.4591   0.01349   0.00382  -0.0665   0.3654   0.3599
  -0.500   0.4720   0.01256   0.00399  -0.0636   0.3616   0.6930
   0.000   0.5977   0.01272   0.00446  -0.0779   0.3527   1.0000
   0.250   0.6203   0.01289   0.00456  -0.0769   0.3502   1.0000
   0.500   0.6430   0.01306   0.00468  -0.0759   0.3479   1.0000
   0.750   0.6657   0.01326   0.00481  -0.0749   0.3455   1.0000
   1.000   0.6883   0.01347   0.00495  -0.0739   0.3429   1.0000
   1.250   0.7108   0.01371   0.00511  -0.0729   0.3402   1.0000
   1.500   0.7335   0.01396   0.00529  -0.0720   0.3374   1.0000
   1.750   0.7570   0.01413   0.00545  -0.0712   0.3344   1.0000
   2.000   0.7805   0.01433   0.00563  -0.0704   0.3318   1.0000
   2.250   0.8040   0.01453   0.00582  -0.0696   0.3296   1.0000
   2.500   0.8276   0.01476   0.00602  -0.0689   0.3273   1.0000
   2.750   0.8511   0.01500   0.00624  -0.0682   0.3252   1.0000
   3.000   0.8749   0.01527   0.00647  -0.0675   0.3234   1.0000
   3.250   0.8990   0.01556   0.00673  -0.0670   0.3217   1.0000
   3.500   0.9233   0.01581   0.00699  -0.0664   0.3201   1.0000
   3.750   0.9472   0.01602   0.00725  -0.0658   0.3182   1.0000
   4.000   0.9708   0.01623   0.00751  -0.0652   0.3156   1.0000
   4.250   0.9942   0.01645   0.00777  -0.0645   0.3127   1.0000
   4.500   1.0171   0.01668   0.00803  -0.0638   0.3095   1.0000
   4.750   1.0397   0.01696   0.00828  -0.0630   0.3060   1.0000
   5.000   1.0625   0.01724   0.00857  -0.0623   0.3026   1.0000
   5.250   1.0849   0.01743   0.00887  -0.0615   0.2993   1.0000
   5.500   1.1073   0.01765   0.00917  -0.0607   0.2960   1.0000
   5.750   1.1291   0.01788   0.00946  -0.0599   0.2925   1.0000
   6.000   1.1500   0.01815   0.00973  -0.0589   0.2885   1.0000
   6.250   1.1707   0.01837   0.01004  -0.0578   0.2838   1.0000
   6.500   1.1912   0.01856   0.01035  -0.0568   0.2786   1.0000
   6.750   1.2105   0.01879   0.01064  -0.0555   0.2736   1.0000
   7.000   1.2299   0.01903   0.01097  -0.0543   0.2682   1.0000
   7.250   1.2488   0.01925   0.01130  -0.0530   0.2613   1.0000
   7.500   1.2652   0.01950   0.01162  -0.0513   0.2547   1.0000
   7.750   1.2823   0.01975   0.01197  -0.0497   0.2443   1.0000
   8.000   1.2978   0.02004   0.01234  -0.0479   0.2258   1.0000
   8.250   1.2944   0.02093   0.01285  -0.0435   0.1738   1.0000
   8.500   1.2985   0.02205   0.01385  -0.0406   0.1567   1.0000
   8.750   1.3055   0.02309   0.01487  -0.0383   0.1460   1.0000
   9.000   1.3139   0.02407   0.01589  -0.0362   0.1381   1.0000
   9.250   1.3227   0.02505   0.01693  -0.0343   0.1308   1.0000
   9.500   1.3293   0.02619   0.01812  -0.0323   0.1219   1.0000
   9.750   1.3374   0.02730   0.01928  -0.0306   0.1127   1.0000
  10.000   1.3427   0.02862   0.02063  -0.0287   0.1022   1.0000
  10.250   1.3470   0.03006   0.02207  -0.0270   0.0841   1.0000
  10.500   1.3429   0.03219   0.02408  -0.0250   0.0685   1.0000
  10.750   1.3394   0.03441   0.02626  -0.0233   0.0625   1.0000
  11.000   1.3381   0.03660   0.02852  -0.0219   0.0592   1.0000
  11.250   1.3348   0.03910   0.03108  -0.0208   0.0564   1.0000
  11.500   1.3301   0.04187   0.03394  -0.0199   0.0544   1.0000
  11.750   1.3250   0.04486   0.03703  -0.0193   0.0525   1.0000
  12.000   1.3231   0.04766   0.03996  -0.0190   0.0509   1.0000
  12.250   1.3193   0.05081   0.04324  -0.0190   0.0495   1.0000
  12.500   1.3136   0.05433   0.04688  -0.0192   0.0481   1.0000
  12.750   1.3058   0.05826   0.05092  -0.0196   0.0468   1.0000
  13.000   1.2960   0.06265   0.05540  -0.0204   0.0457   1.0000
  13.250   1.2849   0.06733   0.06018  -0.0214   0.0447   1.0000
  13.500   1.2795   0.07139   0.06437  -0.0224   0.0436   1.0000
  13.750   1.2762   0.07527   0.06838  -0.0234   0.0424   1.0000
  14.000   1.2716   0.07936   0.07258  -0.0246   0.0412   1.0000
  14.250   1.2670   0.08349   0.07682  -0.0258   0.0400   1.0000
  14.500   1.2621   0.08771   0.08112  -0.0271   0.0389   1.0000
  14.750   1.2565   0.09204   0.08551  -0.0285   0.0378   1.0000
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