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Rhode St. Genese 30 (rhodesg30-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: Rhode St. Genese 30 (rhodesg30-il)
Reynolds number: 200,000
Max Cl/Cd: 66.32 at α=5.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-rhodesg30-il-200000-n5.txt
Download as CSV file: xf-rhodesg30-il-200000-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 =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.750  -0.4664   0.10138   0.09762  -0.0298   1.0000   0.0117
 -12.500  -0.4690   0.09700   0.09326  -0.0315   1.0000   0.0116
 -12.250  -0.4782   0.09120   0.08748  -0.0341   1.0000   0.0115
 -12.000  -0.4875   0.08571   0.08200  -0.0366   1.0000   0.0114
 -11.750  -0.5014   0.07954   0.07585  -0.0397   1.0000   0.0112
 -11.500  -0.5147   0.07389   0.07023  -0.0426   1.0000   0.0111
 -11.250  -0.5354   0.06743   0.06381  -0.0461   1.0000   0.0110
 -11.000  -0.5625   0.06136   0.05784  -0.0493   1.0000   0.0108
 -10.750  -0.5970   0.05055   0.04692  -0.0567   1.0000   0.0106
 -10.500  -0.6143   0.04302   0.03908  -0.0589   1.0000   0.0104
 -10.250  -0.6216   0.03957   0.03540  -0.0573   1.0000   0.0104
 -10.000  -0.6154   0.03648   0.03203  -0.0571   0.9980   0.0104
  -9.750  -0.5907   0.03341   0.02863  -0.0597   0.9922   0.0105
  -9.500  -0.5641   0.03107   0.02599  -0.0616   0.9870   0.0107
  -9.250  -0.5377   0.02920   0.02391  -0.0629   0.9815   0.0108
  -9.000  -0.5091   0.02761   0.02212  -0.0643   0.9769   0.0110
  -8.750  -0.4813   0.02626   0.02059  -0.0652   0.9717   0.0111
  -8.500  -0.4521   0.02498   0.01908  -0.0662   0.9668   0.0116
  -8.250  -0.4212   0.02366   0.01762  -0.0678   0.9634   0.0122
  -8.000  -0.3951   0.02249   0.01627  -0.0681   0.9570   0.0129
  -7.750  -0.3635   0.02154   0.01513  -0.0693   0.9525   0.0133
  -7.500  -0.3308   0.02069   0.01410  -0.0704   0.9476   0.0137
  -7.250  -0.3009   0.01995   0.01318  -0.0709   0.9402   0.0141
  -7.000  -0.2662   0.01917   0.01220  -0.0723   0.9349   0.0146
  -6.750  -0.2373   0.01849   0.01133  -0.0724   0.9265   0.0151
  -6.500  -0.2046   0.01768   0.01032  -0.0733   0.9203   0.0160
  -6.250  -0.1773   0.01657   0.00899  -0.0731   0.9117   0.0181
  -6.000  -0.1449   0.01663   0.00908  -0.0739   0.9048   0.0209
  -5.750  -0.1176   0.01620   0.00855  -0.0735   0.8954   0.0342
  -5.500  -0.0880   0.01566   0.00779  -0.0735   0.8871   0.0392
  -5.250  -0.0599   0.01596   0.00804  -0.0734   0.8769   0.0425
  -5.000  -0.0326   0.01600   0.00797  -0.0730   0.8671   0.0449
  -4.750  -0.0046   0.01610   0.00791  -0.0728   0.8576   0.0475
  -4.500   0.0211   0.01595   0.00784  -0.0725   0.8463   0.0514
  -4.250   0.0471   0.01579   0.00760  -0.0720   0.8344   0.0537
  -4.000   0.0735   0.01581   0.00752  -0.0714   0.8211   0.0563
  -3.750   0.0996   0.01561   0.00720  -0.0709   0.8065   0.0579
  -3.500   0.1256   0.01505   0.00655  -0.0703   0.7924   0.0581
  -3.250   0.1518   0.01460   0.00604  -0.0698   0.7796   0.0582
  -3.000   0.1779   0.01419   0.00557  -0.0692   0.7661   0.0583
  -2.750   0.2037   0.01378   0.00512  -0.0686   0.7517   0.0585
  -2.500   0.2293   0.01342   0.00470  -0.0680   0.7361   0.0588
  -2.250   0.2546   0.01310   0.00433  -0.0673   0.7190   0.0593
  -2.000   0.2798   0.01284   0.00401  -0.0666   0.7003   0.0599
  -1.750   0.3048   0.01264   0.00374  -0.0659   0.6803   0.0605
  -1.500   0.3298   0.01250   0.00351  -0.0652   0.6588   0.0613
  -1.250   0.3547   0.01241   0.00333  -0.0645   0.6359   0.0622
  -1.000   0.3794   0.01236   0.00318  -0.0638   0.6116   0.0633
  -0.750   0.4039   0.01237   0.00307  -0.0630   0.5839   0.0654
  -0.500   0.4280   0.01242   0.00299  -0.0622   0.5503   0.0674
  -0.250   0.4513   0.01255   0.00293  -0.0612   0.5107   0.0692
   0.000   0.4744   0.01273   0.00291  -0.0602   0.4734   0.0704
   0.500   0.5220   0.01307   0.00299  -0.0587   0.4275   0.0754
   0.750   0.5463   0.01320   0.00308  -0.0580   0.4136   0.0816
   1.000   0.5699   0.01313   0.00324  -0.0574   0.4020   0.1766
   1.500   0.6500   0.01168   0.00377  -0.0630   0.3805   1.0000
   1.750   0.6735   0.01193   0.00393  -0.0622   0.3742   1.0000
   2.000   0.6979   0.01213   0.00410  -0.0616   0.3685   1.0000
   2.250   0.7220   0.01236   0.00430  -0.0609   0.3627   1.0000
   2.500   0.7458   0.01262   0.00450  -0.0602   0.3565   1.0000
   2.750   0.7697   0.01283   0.00470  -0.0595   0.3464   1.0000
   3.000   0.7933   0.01307   0.00491  -0.0588   0.3360   1.0000
   3.250   0.8166   0.01334   0.00513  -0.0581   0.3270   1.0000
   3.500   0.8411   0.01353   0.00535  -0.0575   0.3191   1.0000
   3.750   0.8646   0.01380   0.00560  -0.0568   0.3115   1.0000
   4.000   0.8890   0.01398   0.00585  -0.0563   0.3030   1.0000
   4.250   0.9124   0.01424   0.00611  -0.0556   0.2950   1.0000
   4.500   0.9368   0.01443   0.00638  -0.0551   0.2855   1.0000
   4.750   0.9606   0.01466   0.00667  -0.0544   0.2756   1.0000
   5.000   0.9840   0.01490   0.00695  -0.0538   0.2627   1.0000
   5.250   1.0067   0.01518   0.00722  -0.0530   0.2376   1.0000
   5.500   1.0199   0.01622   0.00775  -0.0511   0.1526   1.0000
   5.750   1.0367   0.01713   0.00851  -0.0496   0.1199   1.0000
   6.000   1.0548   0.01789   0.00919  -0.0483   0.0908   1.0000
   6.500   1.0868   0.01962   0.01073  -0.0452   0.0550   1.0000
   6.750   1.1043   0.02029   0.01150  -0.0437   0.0522   1.0000
   7.000   1.1204   0.02103   0.01233  -0.0421   0.0500   1.0000
   7.250   1.1342   0.02188   0.01327  -0.0402   0.0478   1.0000
   7.500   1.1464   0.02276   0.01425  -0.0381   0.0455   1.0000
   7.750   1.1600   0.02343   0.01506  -0.0362   0.0435   1.0000
   8.000   1.1711   0.02423   0.01597  -0.0339   0.0411   1.0000
   8.250   1.1804   0.02514   0.01699  -0.0316   0.0388   1.0000
   8.500   1.1862   0.02631   0.01822  -0.0290   0.0365   1.0000
   8.750   1.1853   0.02796   0.01995  -0.0260   0.0344   1.0000
   9.000   1.1983   0.02877   0.02090  -0.0245   0.0328   1.0000
   9.250   1.2077   0.02986   0.02212  -0.0229   0.0307   1.0000
   9.500   1.2155   0.03109   0.02347  -0.0213   0.0284   1.0000
   9.750   1.2208   0.03257   0.02502  -0.0198   0.0264   1.0000
  10.000   1.2207   0.03456   0.02707  -0.0181   0.0247   1.0000
  10.250   1.2288   0.03600   0.02868  -0.0170   0.0229   1.0000
  10.500   1.2333   0.03781   0.03063  -0.0159   0.0210   1.0000
  10.750   1.2388   0.03958   0.03249  -0.0152   0.0192   1.0000
  11.000   1.2418   0.04168   0.03466  -0.0147   0.0180   1.0000
  11.250   1.2423   0.04416   0.03725  -0.0142   0.0169   1.0000
  11.500   1.2433   0.04670   0.03994  -0.0138   0.0159   1.0000
  11.750   1.2431   0.04950   0.04286  -0.0137   0.0150   1.0000
  12.000   1.2430   0.05238   0.04586  -0.0139   0.0143   1.0000
  12.250   1.2414   0.05553   0.04913  -0.0143   0.0138   1.0000
  12.500   1.2399   0.05884   0.05254  -0.0151   0.0131   1.0000
  12.750   1.2359   0.06253   0.05633  -0.0158   0.0128   1.0000
  13.000   1.2288   0.06679   0.06066  -0.0169   0.0122   1.0000
  13.250   1.2256   0.07062   0.06465  -0.0178   0.0119   1.0000
  13.500   1.2221   0.07460   0.06880  -0.0189   0.0116   1.0000
  13.750   1.2182   0.07879   0.07316  -0.0202   0.0112   1.0000
  14.000   1.2135   0.08327   0.07779  -0.0219   0.0107   1.0000
  14.250   1.2086   0.08786   0.08253  -0.0238   0.0104   1.0000
  14.500   1.2025   0.09272   0.08753  -0.0257   0.0101   1.0000
  14.750   1.1957   0.09784   0.09280  -0.0280   0.0099   1.0000
  15.000   1.1885   0.10312   0.09822  -0.0303   0.0098   1.0000
  15.250   1.1802   0.10875   0.10397  -0.0330   0.0095   1.0000
  15.500   1.1718   0.11447   0.10984  -0.0358   0.0094   1.0000
  15.750   1.1623   0.12055   0.11605  -0.0389   0.0092   1.0000
  16.000   1.1521   0.12693   0.12260  -0.0421   0.0093   1.0000
  16.250   1.1417   0.13351   0.12931  -0.0456   0.0091   1.0000
  16.500   1.1303   0.14054   0.13647  -0.0495   0.0090   1.0000
  16.750   1.1160   0.14855   0.14466  -0.0540   0.0091   1.0000
  17.000   1.0978   0.15809   0.15437  -0.0594   0.0091   1.0000
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