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Rhode St. Genese 32 (rhodesg32-il) Xfoil prediction polar at RE=100,000 Ncrit=9


Details Polar file
Airfoil: Rhode St. Genese 32 (rhodesg32-il)
Reynolds number: 100,000
Max Cl/Cd: 45.24 at α=3.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-rhodesg32-il-100000.txt
Download as CSV file: xf-rhodesg32-il-100000.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 =     0.100 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -10.750  -0.3100   0.10110   0.09611  -0.0353   1.0000   0.1264
 -10.500  -0.3416   0.10080   0.09598  -0.0364   1.0000   0.1298
 -10.250  -0.3811   0.10096   0.09632  -0.0350   1.0000   0.1303
 -10.000  -0.3544   0.09554   0.09089  -0.0323   1.0000   0.1328
  -9.750  -0.3464   0.09325   0.08862  -0.0292   1.0000   0.1355
  -9.500  -0.3562   0.09185   0.08730  -0.0264   1.0000   0.1382
  -9.250  -0.3756   0.09080   0.08635  -0.0236   1.0000   0.1406
  -9.000  -0.4041   0.09010   0.08576  -0.0204   1.0000   0.1423
  -8.750  -0.4437   0.08910   0.08486  -0.0212   1.0000   0.1446
  -8.500  -0.4789   0.08625   0.08198  -0.0252   1.0000   0.1464
  -8.250  -0.4645   0.08332   0.07917  -0.0193   1.0000   0.1481
  -8.000  -0.4561   0.08149   0.07738  -0.0157   0.9995   0.1516
  -7.750  -0.4336   0.07530   0.07100  -0.0296   0.9888   0.1634
  -7.500  -0.4002   0.07220   0.06793  -0.0299   0.9834   0.1685
  -7.250  -0.3778   0.06710   0.06262  -0.0391   0.9730   0.1803
  -7.000  -0.3483   0.06421   0.05975  -0.0403   0.9660   0.1869
  -6.750  -0.3202   0.06022   0.05563  -0.0456   0.9576   0.1999
  -6.500  -0.2970   0.05688   0.05211  -0.0496   0.9476   0.2144
  -6.250  -0.2607   0.05358   0.04865  -0.0545   0.9411   0.2308
  -6.000  -0.2386   0.05119   0.04629  -0.0541   0.9313   0.2377
  -5.750  -0.2017   0.04833   0.04325  -0.0585   0.9252   0.2658
  -5.500  -0.1626   0.03574   0.02848  -0.0658   0.9152   0.1280
  -5.250  -0.1178   0.03270   0.02502  -0.0690   0.9096   0.1243
  -5.000  -0.0882   0.03094   0.02293  -0.0692   0.8987   0.1245
  -4.750  -0.0366   0.02864   0.02021  -0.0729   0.8932   0.1240
  -4.500  -0.0056   0.02726   0.01855  -0.0730   0.8823   0.1243
  -4.250   0.0445   0.02578   0.01679  -0.0763   0.8775   0.1274
  -4.000   0.0752   0.02499   0.01577  -0.0762   0.8675   0.1303
  -3.750   0.1190   0.02354   0.01434  -0.0784   0.8614   0.1337
  -3.500   0.1498   0.02274   0.01355  -0.0783   0.8513   0.1378
  -3.250   0.1922   0.02181   0.01251  -0.0799   0.8440   0.1456
  -3.000   0.2196   0.02096   0.01184  -0.0792   0.8321   0.1536
  -2.750   0.2559   0.01992   0.01086  -0.0797   0.8228   0.1654
  -2.500   0.2862   0.01894   0.01003  -0.0791   0.8108   0.1860
  -2.250   0.4107   0.01502   0.00877  -0.0954   0.7990   1.0000
  -2.000   0.4350   0.01472   0.00824  -0.0938   0.7806   1.0000
  -1.750   0.4606   0.01439   0.00768  -0.0924   0.7603   1.0000
  -1.500   0.4811   0.01420   0.00731  -0.0902   0.7327   1.0000
  -1.250   0.5040   0.01401   0.00688  -0.0883   0.6996   1.0000
  -1.000   0.5265   0.01397   0.00650  -0.0865   0.6591   1.0000
  -0.750   0.5472   0.01415   0.00630  -0.0845   0.6158   1.0000
  -0.500   0.5682   0.01446   0.00625  -0.0829   0.5812   1.0000
  -0.250   0.5898   0.01481   0.00633  -0.0815   0.5555   1.0000
   0.000   0.6123   0.01516   0.00644  -0.0804   0.5374   1.0000
   0.250   0.6355   0.01551   0.00658  -0.0794   0.5237   1.0000
   0.500   0.6597   0.01587   0.00673  -0.0787   0.5133   1.0000
   0.750   0.6833   0.01623   0.00699  -0.0780   0.5037   1.0000
   1.000   0.7086   0.01662   0.00721  -0.0775   0.4968   1.0000
   1.250   0.7329   0.01701   0.00756  -0.0769   0.4902   1.0000
   1.500   0.7584   0.01741   0.00787  -0.0765   0.4850   1.0000
   1.750   0.7847   0.01786   0.00821  -0.0763   0.4809   1.0000
   2.000   0.8089   0.01830   0.00868  -0.0758   0.4765   1.0000
   2.250   0.8340   0.01876   0.00915  -0.0755   0.4727   1.0000
   2.500   0.8598   0.01923   0.00957  -0.0752   0.4690   1.0000
   2.750   0.8868   0.01975   0.00998  -0.0752   0.4654   1.0000
   3.000   0.9089   0.02023   0.01058  -0.0744   0.4609   1.0000
   3.250   0.9324   0.02071   0.01110  -0.0738   0.4562   1.0000
   3.500   0.9582   0.02118   0.01151  -0.0735   0.4516   1.0000
   3.750   0.9826   0.02173   0.01209  -0.0731   0.4474   1.0000
   4.000   1.0041   0.02227   0.01275  -0.0723   0.4429   1.0000
   4.250   1.0278   0.02282   0.01336  -0.0718   0.4390   1.0000
   4.500   1.0531   0.02340   0.01398  -0.0716   0.4360   1.0000
   4.750   1.0797   0.02407   0.01465  -0.0716   0.4336   1.0000
   5.000   1.1004   0.02479   0.01554  -0.0708   0.4307   1.0000
   5.250   1.1204   0.02549   0.01644  -0.0698   0.4270   1.0000
   5.500   1.1424   0.02619   0.01726  -0.0692   0.4235   1.0000
   5.750   1.1682   0.02674   0.01781  -0.0690   0.4188   1.0000
   6.000   1.1875   0.02741   0.01862  -0.0679   0.4128   1.0000
   6.250   1.2086   0.02785   0.01915  -0.0669   0.4051   1.0000
   6.500   1.2319   0.02835   0.01965  -0.0664   0.3975   1.0000
   6.750   1.2503   0.02879   0.02022  -0.0650   0.3892   1.0000
   7.000   1.2746   0.02923   0.02067  -0.0646   0.3815   1.0000
   7.250   1.2909   0.02972   0.02133  -0.0629   0.3732   1.0000
   7.500   1.3167   0.03013   0.02172  -0.0628   0.3655   1.0000
   7.750   1.3298   0.03067   0.02251  -0.0607   0.3572   1.0000
   8.000   1.3540   0.03093   0.02275  -0.0602   0.3481   1.0000
   8.250   1.3683   0.03118   0.02315  -0.0581   0.3377   1.0000
   8.500   1.3829   0.03148   0.02359  -0.0562   0.3274   1.0000
   8.750   1.4043   0.03134   0.02340  -0.0551   0.3157   1.0000
   9.000   1.4097   0.03145   0.02373  -0.0517   0.3038   1.0000
   9.250   1.4140   0.03156   0.02402  -0.0482   0.2915   1.0000
   9.500   1.4159   0.03152   0.02412  -0.0442   0.2783   1.0000
   9.750   1.4095   0.03158   0.02433  -0.0390   0.2643   1.0000
  10.000   1.3992   0.03203   0.02499  -0.0338   0.2463   1.0000
  10.250   1.3888   0.03278   0.02584  -0.0293   0.2176   1.0000
  10.500   1.3734   0.03424   0.02700  -0.0252   0.1889   1.0000
  10.750   1.3522   0.03703   0.02946  -0.0217   0.1715   1.0000
  11.000   1.3302   0.04057   0.03280  -0.0189   0.1578   1.0000
  11.250   1.3119   0.04426   0.03640  -0.0169   0.1456   1.0000
  11.500   1.2980   0.04790   0.04004  -0.0155   0.1341   1.0000
  11.750   1.2888   0.05126   0.04337  -0.0145   0.1243   1.0000
  12.000   1.2859   0.05405   0.04600  -0.0135   0.1159   1.0000
  12.250   1.2813   0.05725   0.04937  -0.0132   0.1089   1.0000
  12.500   1.2848   0.05954   0.05153  -0.0125   0.1025   1.0000
  12.750   1.2825   0.06268   0.05486  -0.0125   0.0973   1.0000
  13.000   1.2864   0.06502   0.05712  -0.0122   0.0924   1.0000
  13.250   1.2887   0.06781   0.06004  -0.0120   0.0880   1.0000
  13.500   1.2904   0.07062   0.06295  -0.0121   0.0841   1.0000
  13.750   1.3018   0.07223   0.06441  -0.0115   0.0800   1.0000
  14.000   1.3006   0.07569   0.06812  -0.0118   0.0773   1.0000
  14.250   1.3015   0.07882   0.07138  -0.0121   0.0744   1.0000
  14.500   1.3167   0.08012   0.07254  -0.0115   0.0711   1.0000
  14.750   1.3182   0.08350   0.07609  -0.0117   0.0690   1.0000
  15.000   1.3124   0.08784   0.08069  -0.0126   0.0676   1.0000
  15.250   1.3057   0.09238   0.08546  -0.0137   0.0663   1.0000
  15.500   1.2972   0.09723   0.09051  -0.0153   0.0652   1.0000
  15.750   1.2884   0.10218   0.09563  -0.0170   0.0641   1.0000
  16.000   1.2844   0.10647   0.10003  -0.0184   0.0628   1.0000
  16.250   1.2928   0.10942   0.10295  -0.0184   0.0609   1.0000
  16.500   1.2677   0.11710   0.11091  -0.0223   0.0609   1.0000
  16.750   1.2423   0.12536   0.11940  -0.0268   0.0609   1.0000
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