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Rhode St. Genese 30 (rhodesg30-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: Rhode St. Genese 30 (rhodesg30-il)
Reynolds number: 1,000,000
Max Cl/Cd: 105.36 at α=3.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-rhodesg30-il-1000000.txt
Download as CSV file: xf-rhodesg30-il-1000000.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 =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.500  -0.3692   0.12396   0.12235  -0.0220   1.0000   0.0126
 -14.250  -0.3764   0.11771   0.11610  -0.0242   1.0000   0.0126
 -10.750  -0.6869   0.02640   0.02288  -0.0658   0.9934   0.0090
 -10.500  -0.6641   0.02348   0.01975  -0.0667   0.9889   0.0085
 -10.250  -0.6359   0.02157   0.01764  -0.0679   0.9856   0.0085
 -10.000  -0.6053   0.02006   0.01596  -0.0693   0.9829   0.0087
  -9.750  -0.5780   0.01883   0.01459  -0.0697   0.9768   0.0088
  -9.500  -0.5461   0.01769   0.01333  -0.0710   0.9728   0.0090
  -9.250  -0.5147   0.01672   0.01225  -0.0720   0.9685   0.0091
  -9.000  -0.4839   0.01612   0.01153  -0.0727   0.9614   0.0094
  -8.750  -0.4524   0.01523   0.01054  -0.0737   0.9548   0.0095
  -8.500  -0.4234   0.01474   0.00995  -0.0739   0.9456   0.0096
  -8.250  -0.3972   0.01386   0.00899  -0.0737   0.9363   0.0097
  -8.000  -0.3736   0.01280   0.00785  -0.0730   0.9269   0.0099
  -7.750  -0.3508   0.01190   0.00686  -0.0721   0.9177   0.0102
  -7.500  -0.3259   0.01133   0.00620  -0.0714   0.9091   0.0106
  -7.250  -0.3008   0.01088   0.00565  -0.0707   0.9001   0.0109
  -7.000  -0.2754   0.01046   0.00516  -0.0700   0.8920   0.0113
  -6.750  -0.2494   0.01016   0.00479  -0.0694   0.8839   0.0117
  -6.500  -0.2230   0.00991   0.00448  -0.0689   0.8764   0.0122
  -6.250  -0.1966   0.00970   0.00421  -0.0684   0.8681   0.0125
  -6.000  -0.1704   0.00945   0.00387  -0.0678   0.8595   0.0130
  -5.750  -0.1447   0.00912   0.00343  -0.0672   0.8508   0.0137
  -5.500  -0.1191   0.00875   0.00295  -0.0665   0.8406   0.0148
  -5.250  -0.0932   0.00850   0.00260  -0.0659   0.8295   0.0158
  -5.000  -0.0673   0.00826   0.00230  -0.0653   0.8171   0.0192
  -4.750  -0.0406   0.00822   0.00237  -0.0649   0.8039   0.0359
  -4.500  -0.0117   0.00857   0.00275  -0.0648   0.7904   0.0393
  -4.250   0.0187   0.00931   0.00350  -0.0650   0.7761   0.0404
  -4.000   0.0441   0.00904   0.00318  -0.0645   0.7608   0.0424
  -3.750   0.0715   0.00921   0.00333  -0.0642   0.7444   0.0436
  -3.500   0.0983   0.00928   0.00336  -0.0639   0.7268   0.0447
  -3.250   0.1249   0.00934   0.00336  -0.0635   0.7084   0.0459
  -3.000   0.1516   0.00950   0.00344  -0.0631   0.6890   0.0473
  -2.750   0.1777   0.00948   0.00334  -0.0626   0.6691   0.0479
  -2.500   0.2052   0.01002   0.00378  -0.0624   0.6465   0.0489
  -2.250   0.2305   0.00975   0.00343  -0.0618   0.6241   0.0488
  -2.000   0.2548   0.00922   0.00282  -0.0610   0.5997   0.0492
  -1.750   0.2778   0.00880   0.00227  -0.0600   0.5655   0.0504
  -1.500   0.3013   0.00881   0.00209  -0.0592   0.5103   0.0514
  -1.250   0.3237   0.00905   0.00205  -0.0581   0.4393   0.0521
  -1.000   0.3484   0.00916   0.00201  -0.0575   0.4044   0.0529
  -0.750   0.3740   0.00920   0.00197  -0.0571   0.3842   0.0535
  -0.500   0.4000   0.00923   0.00194  -0.0567   0.3703   0.0541
  -0.250   0.4265   0.00923   0.00190  -0.0563   0.3606   0.0546
   0.000   0.4529   0.00924   0.00188  -0.0560   0.3523   0.0550
   0.250   0.4795   0.00924   0.00187  -0.0558   0.3457   0.0556
   0.500   0.5060   0.00927   0.00188  -0.0555   0.3390   0.0561
   0.750   0.5327   0.00928   0.00188  -0.0552   0.3322   0.0567
   1.000   0.5591   0.00934   0.00191  -0.0549   0.3263   0.0575
   1.250   0.5861   0.00935   0.00194  -0.0547   0.3222   0.0585
   1.500   0.6127   0.00938   0.00196  -0.0545   0.3162   0.0601
   1.750   0.6390   0.00944   0.00200  -0.0542   0.3110   0.0640
   2.000   0.6660   0.00945   0.00205  -0.0540   0.3076   0.0696
   2.250   0.6918   0.00931   0.00214  -0.0537   0.3026   0.1804
   2.500   0.7585   0.00764   0.00247  -0.0631   0.2931   1.0000
   2.750   0.7832   0.00774   0.00255  -0.0625   0.2873   1.0000
   3.000   0.8073   0.00789   0.00266  -0.0618   0.2804   1.0000
   3.250   0.8323   0.00798   0.00275  -0.0613   0.2731   1.0000
   3.500   0.8566   0.00813   0.00286  -0.0606   0.2622   1.0000
   3.750   0.8798   0.00836   0.00298  -0.0598   0.2383   1.0000
   4.000   0.8920   0.00949   0.00357  -0.0572   0.1343   1.0000
   4.250   0.9099   0.01021   0.00403  -0.0556   0.0874   1.0000
   4.500   0.9279   0.01096   0.00453  -0.0540   0.0452   1.0000
   4.750   0.9511   0.01124   0.00483  -0.0532   0.0417   1.0000
   5.000   0.9744   0.01151   0.00513  -0.0524   0.0402   1.0000
   5.250   0.9974   0.01181   0.00545  -0.0516   0.0384   1.0000
   5.500   1.0198   0.01217   0.00582  -0.0507   0.0365   1.0000
   5.750   1.0414   0.01260   0.00628  -0.0497   0.0341   1.0000
   6.000   1.0621   0.01309   0.00685  -0.0486   0.0324   1.0000
   6.250   1.0853   0.01335   0.00713  -0.0479   0.0318   1.0000
   6.500   1.1079   0.01365   0.00746  -0.0472   0.0309   1.0000
   6.750   1.1301   0.01398   0.00782  -0.0464   0.0297   1.0000
   7.000   1.1517   0.01435   0.00821  -0.0455   0.0285   1.0000
   7.250   1.1725   0.01476   0.00864  -0.0445   0.0272   1.0000
   7.500   1.1877   0.01558   0.00952  -0.0427   0.0250   1.0000
   7.750   1.2088   0.01593   0.00991  -0.0418   0.0243   1.0000
   8.000   1.2316   0.01614   0.01013  -0.0412   0.0233   1.0000
   8.250   1.2527   0.01645   0.01047  -0.0403   0.0221   1.0000
   8.500   1.2739   0.01674   0.01075  -0.0395   0.0208   1.0000
   8.750   1.2887   0.01743   0.01145  -0.0377   0.0190   1.0000
   9.000   1.3080   0.01778   0.01185  -0.0366   0.0181   1.0000
   9.250   1.3276   0.01805   0.01214  -0.0355   0.0169   1.0000
   9.500   1.3445   0.01840   0.01247  -0.0340   0.0157   1.0000
   9.750   1.3533   0.01913   0.01322  -0.0312   0.0143   1.0000
  10.000   1.3665   0.01967   0.01382  -0.0292   0.0137   1.0000
  10.250   1.3800   0.02023   0.01442  -0.0274   0.0129   1.0000
  10.500   1.3928   0.02083   0.01507  -0.0256   0.0122   1.0000
  10.750   1.4028   0.02162   0.01588  -0.0235   0.0115   1.0000
  11.000   1.4030   0.02304   0.01739  -0.0205   0.0106   1.0000
  11.250   1.4156   0.02378   0.01818  -0.0191   0.0103   1.0000
  11.500   1.4237   0.02484   0.01932  -0.0174   0.0100   1.0000
  11.750   1.4315   0.02598   0.02053  -0.0158   0.0095   1.0000
  12.000   1.4390   0.02720   0.02181  -0.0144   0.0091   1.0000
  12.250   1.4442   0.02867   0.02336  -0.0131   0.0089   1.0000
  12.500   1.4452   0.03058   0.02534  -0.0117   0.0083   1.0000
  12.750   1.4394   0.03324   0.02812  -0.0103   0.0080   1.0000
  13.000   1.4351   0.03599   0.03098  -0.0095   0.0079   1.0000
  13.250   1.4342   0.03858   0.03368  -0.0092   0.0077   1.0000
  13.500   1.4334   0.04131   0.03652  -0.0091   0.0076   1.0000
  13.750   1.4326   0.04417   0.03949  -0.0093   0.0075   1.0000
  14.000   1.4290   0.04748   0.04290  -0.0097   0.0074   1.0000
  14.250   1.4260   0.05087   0.04640  -0.0103   0.0072   1.0000
  14.500   1.4215   0.05458   0.05022  -0.0112   0.0071   1.0000
  14.750   1.4153   0.05866   0.05440  -0.0123   0.0069   1.0000
  15.000   1.4087   0.06295   0.05881  -0.0137   0.0068   1.0000
  15.250   1.3994   0.06776   0.06372  -0.0154   0.0067   1.0000
  15.500   1.3886   0.07288   0.06896  -0.0172   0.0066   1.0000
  15.750   1.3810   0.07764   0.07381  -0.0190   0.0065   1.0000
  16.000   1.3667   0.08342   0.07972  -0.0211   0.0066   1.0000
  16.250   1.3578   0.08848   0.08488  -0.0232   0.0065   1.0000
  16.500   1.3490   0.09362   0.09009  -0.0253   0.0064   1.0000
  16.750   1.3359   0.09948   0.09606  -0.0277   0.0063   1.0000
  17.000   1.3258   0.10495   0.10161  -0.0301   0.0062   1.0000
  17.250   1.3135   0.11088   0.10765  -0.0328   0.0062   1.0000
  17.500   1.3042   0.11642   0.11327  -0.0353   0.0061   1.0000
  17.750   1.2902   0.12288   0.11983  -0.0384   0.0060   1.0000
  18.000   1.2810   0.12860   0.12564  -0.0413   0.0060   1.0000
  18.250   1.2694   0.13490   0.13204  -0.0445   0.0059   1.0000
  18.500   1.2555   0.14180   0.13905  -0.0481   0.0058   1.0000
  18.750   1.2410   0.14893   0.14629  -0.0520   0.0057   1.0000
  19.000   1.2326   0.15504   0.15250  -0.0555   0.0057   1.0000
  19.250   1.2152   0.16329   0.16089  -0.0602   0.0057   1.0000
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