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Rhode St. Genese 30 (rhodesg30-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: Rhode St. Genese 30 (rhodesg30-il)
Reynolds number: 500,000
Max Cl/Cd: 84.62 at α=3.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-rhodesg30-il-500000-n5.txt
Download as CSV file: xf-rhodesg30-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: Rhode St. Genese 30                             
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -12.750  -0.5227   0.08801   0.08553  -0.0346   1.0000   0.0059
 -12.500  -0.5411   0.08047   0.07797  -0.0388   1.0000   0.0059
 -12.250  -0.5591   0.07366   0.07116  -0.0426   1.0000   0.0058
 -12.000  -0.5829   0.06600   0.06348  -0.0473   1.0000   0.0057
 -11.750  -0.6153   0.05788   0.05537  -0.0528   1.0000   0.0055
 -11.500  -0.6568   0.04389   0.04115  -0.0637   1.0000   0.0051
 -11.250  -0.6691   0.03924   0.03627  -0.0639   1.0000   0.0052
 -11.000  -0.6517   0.03481   0.03150  -0.0681   0.9926   0.0053
 -10.750  -0.6309   0.03152   0.02789  -0.0708   0.9857   0.0054
 -10.500  -0.6096   0.02903   0.02512  -0.0722   0.9783   0.0056
 -10.250  -0.5848   0.02684   0.02267  -0.0736   0.9727   0.0057
 -10.000  -0.5590   0.02490   0.02051  -0.0747   0.9667   0.0058
  -9.750  -0.5319   0.02318   0.01857  -0.0758   0.9613   0.0058
  -9.500  -0.5044   0.02168   0.01689  -0.0766   0.9539   0.0059
  -9.250  -0.4753   0.02037   0.01544  -0.0776   0.9474   0.0060
  -9.000  -0.4470   0.01925   0.01417  -0.0781   0.9383   0.0062
  -8.750  -0.4194   0.01829   0.01307  -0.0785   0.9292   0.0063
  -8.500  -0.3944   0.01709   0.01175  -0.0784   0.9200   0.0065
  -8.250  -0.3705   0.01620   0.01076  -0.0779   0.9109   0.0067
  -8.000  -0.3452   0.01554   0.00999  -0.0775   0.9028   0.0069
  -7.750  -0.3204   0.01501   0.00939  -0.0769   0.8936   0.0071
  -7.500  -0.2949   0.01459   0.00887  -0.0764   0.8850   0.0074
  -7.250  -0.2692   0.01425   0.00844  -0.0758   0.8762   0.0077
  -7.000  -0.2433   0.01390   0.00800  -0.0753   0.8682   0.0084
  -6.750  -0.2172   0.01360   0.00758  -0.0748   0.8599   0.0087
  -6.500  -0.1911   0.01340   0.00730  -0.0743   0.8504   0.0091
  -6.250  -0.1651   0.01307   0.00685  -0.0738   0.8407   0.0096
  -6.000  -0.1393   0.01267   0.00633  -0.0732   0.8300   0.0101
  -5.750  -0.1137   0.01220   0.00574  -0.0726   0.8184   0.0107
  -5.500  -0.0881   0.01172   0.00514  -0.0720   0.8060   0.0114
  -5.250  -0.0632   0.01113   0.00439  -0.0713   0.7934   0.0127
  -5.000  -0.0383   0.01061   0.00370  -0.0705   0.7797   0.0140
  -4.750  -0.0130   0.01028   0.00324  -0.0698   0.7641   0.0154
  -4.500   0.0130   0.01021   0.00321  -0.0693   0.7461   0.0324
  -4.250   0.0398   0.01040   0.00333  -0.0688   0.7257   0.0379
  -4.000   0.0666   0.01058   0.00337  -0.0684   0.7054   0.0400
  -3.750   0.0934   0.01079   0.00357  -0.0681   0.6859   0.0418
  -3.500   0.1197   0.01090   0.00360  -0.0677   0.6668   0.0431
  -3.250   0.1459   0.01098   0.00359  -0.0672   0.6483   0.0445
  -3.000   0.1722   0.01107   0.00361  -0.0668   0.6297   0.0458
  -2.750   0.1985   0.01116   0.00360  -0.0664   0.6098   0.0466
  -2.500   0.2239   0.01108   0.00342  -0.0658   0.5879   0.0468
  -2.250   0.2491   0.01100   0.00324  -0.0652   0.5610   0.0469
  -2.000   0.2730   0.01085   0.00295  -0.0644   0.5251   0.0473
  -1.750   0.2959   0.01078   0.00268  -0.0635   0.4763   0.0477
  -1.500   0.3192   0.01079   0.00251  -0.0627   0.4357   0.0483
  -1.250   0.3438   0.01080   0.00240  -0.0621   0.4097   0.0489
  -1.000   0.3691   0.01081   0.00234  -0.0616   0.3918   0.0495
  -0.750   0.3947   0.01082   0.00229  -0.0612   0.3781   0.0503
  -0.500   0.4205   0.01084   0.00227  -0.0607   0.3658   0.0509
  -0.250   0.4463   0.01088   0.00226  -0.0604   0.3546   0.0517
   0.000   0.4723   0.01092   0.00226  -0.0600   0.3455   0.0525
   0.250   0.4985   0.01095   0.00227  -0.0597   0.3396   0.0535
   0.500   0.5250   0.01097   0.00229  -0.0594   0.3351   0.0545
   0.750   0.5513   0.01101   0.00233  -0.0591   0.3306   0.0560
   1.000   0.5774   0.01109   0.00240  -0.0588   0.3251   0.0571
   1.250   0.6036   0.01114   0.00244  -0.0585   0.3173   0.0582
   1.500   0.6294   0.01124   0.00249  -0.0582   0.3107   0.0602
   1.750   0.6559   0.01127   0.00256  -0.0579   0.3058   0.0628
   2.000   0.6819   0.01135   0.00264  -0.0576   0.2993   0.0669
   2.500   0.7165   0.00968   0.00302  -0.0539   0.2914   0.8334
   3.000   0.8105   0.00985   0.00340  -0.0626   0.2747   1.0000
   3.250   0.8346   0.01003   0.00353  -0.0619   0.2640   1.0000
   3.500   0.8589   0.01020   0.00367  -0.0613   0.2520   1.0000
   3.750   0.8826   0.01043   0.00384  -0.0607   0.2316   1.0000
   4.000   0.8965   0.01152   0.00439  -0.0586   0.1372   1.0000
   4.250   0.9178   0.01199   0.00477  -0.0576   0.1154   1.0000
   4.500   0.9395   0.01244   0.00513  -0.0567   0.0963   1.0000
   4.750   0.9577   0.01322   0.00566  -0.0552   0.0521   1.0000
   5.000   0.9801   0.01359   0.00604  -0.0544   0.0453   1.0000
   5.250   1.0030   0.01391   0.00640  -0.0537   0.0430   1.0000
   5.500   1.0255   0.01427   0.00679  -0.0529   0.0409   1.0000
   5.750   1.0475   0.01466   0.00721  -0.0520   0.0392   1.0000
   6.000   1.0693   0.01506   0.00766  -0.0512   0.0381   1.0000
   6.250   1.0905   0.01549   0.00814  -0.0502   0.0369   1.0000
   6.500   1.1103   0.01602   0.00874  -0.0491   0.0351   1.0000
   6.750   1.1315   0.01641   0.00917  -0.0482   0.0337   1.0000
   7.000   1.1528   0.01676   0.00958  -0.0473   0.0326   1.0000
   7.250   1.1733   0.01716   0.01003  -0.0464   0.0312   1.0000
   7.500   1.1932   0.01759   0.01052  -0.0453   0.0297   1.0000
   7.750   1.2120   0.01807   0.01103  -0.0442   0.0281   1.0000
   8.000   1.2286   0.01867   0.01166  -0.0427   0.0262   1.0000
   8.250   1.2440   0.01927   0.01233  -0.0409   0.0248   1.0000
   8.500   1.2630   0.01957   0.01268  -0.0398   0.0235   1.0000
   8.750   1.2800   0.01995   0.01312  -0.0383   0.0211   1.0000
   9.000   1.2952   0.02043   0.01361  -0.0366   0.0182   1.0000
   9.250   1.3084   0.02104   0.01422  -0.0347   0.0154   1.0000
   9.500   1.3200   0.02175   0.01491  -0.0327   0.0127   1.0000
   9.750   1.3302   0.02258   0.01579  -0.0306   0.0111   1.0000
  10.000   1.3387   0.02352   0.01678  -0.0285   0.0098   1.0000
  10.250   1.3456   0.02462   0.01795  -0.0264   0.0089   1.0000
  10.500   1.3528   0.02575   0.01916  -0.0244   0.0083   1.0000
  10.750   1.3592   0.02698   0.02050  -0.0226   0.0078   1.0000
  11.000   1.3648   0.02835   0.02197  -0.0209   0.0074   1.0000
  11.250   1.3692   0.02988   0.02359  -0.0193   0.0070   1.0000
  11.500   1.3724   0.03160   0.02540  -0.0179   0.0067   1.0000
  11.750   1.3724   0.03369   0.02759  -0.0166   0.0063   1.0000
  12.000   1.3714   0.03604   0.03005  -0.0156   0.0060   1.0000
  12.250   1.3714   0.03842   0.03255  -0.0149   0.0060   1.0000
  12.500   1.3723   0.04085   0.03511  -0.0145   0.0056   1.0000
  12.750   1.3708   0.04367   0.03805  -0.0144   0.0056   1.0000
  13.000   1.3685   0.04673   0.04123  -0.0145   0.0053   1.0000
  13.250   1.3669   0.04983   0.04445  -0.0149   0.0051   1.0000
  13.500   1.3606   0.05367   0.04842  -0.0156   0.0051   1.0000
  13.750   1.3555   0.05754   0.05241  -0.0165   0.0050   1.0000
  14.000   1.3486   0.06185   0.05685  -0.0178   0.0048   1.0000
  14.250   1.3437   0.06598   0.06109  -0.0191   0.0046   1.0000
  14.500   1.3349   0.07088   0.06612  -0.0209   0.0046   1.0000
  14.750   1.3259   0.07595   0.07130  -0.0228   0.0045   1.0000
  15.000   1.3170   0.08106   0.07652  -0.0248   0.0045   1.0000
  15.250   1.3035   0.08706   0.08263  -0.0272   0.0043   1.0000
  15.500   1.2936   0.09252   0.08821  -0.0295   0.0043   1.0000
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