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Rhode St. Genese 34 (rhodesg34-il) Xfoil prediction polar at RE=100,000 Ncrit=9


Details Polar file
Airfoil: Rhode St. Genese 34 (rhodesg34-il)
Reynolds number: 100,000
Max Cl/Cd: 43.8 at α=3°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-rhodesg34-il-100000.txt
Download as CSV file: xf-rhodesg34-il-100000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: Rhode St. Genese 34                             
  
 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  -0.3213   0.11368   0.10918  -0.0221   1.0000   0.1179
 -10.500  -0.3354   0.11247   0.10804  -0.0211   1.0000   0.1208
 -10.250  -0.3748   0.11232   0.10799  -0.0249   0.9978   0.1232
 -10.000  -0.3451   0.10660   0.10226  -0.0277   0.9937   0.1252
  -9.750  -0.3070   0.10263   0.09825  -0.0293   0.9885   0.1295
  -9.500  -0.3057   0.09969   0.09532  -0.0371   0.9805   0.1361
  -9.250  -0.3234   0.09560   0.09126  -0.0468   0.9693   0.1385
  -9.000  -0.2660   0.09141   0.08703  -0.0443   0.9662   0.1426
  -8.750  -0.2546   0.08829   0.08392  -0.0481   0.9573   0.1478
  -8.500  -0.2795   0.08369   0.07923  -0.0602   0.9422   0.1537
  -8.250  -0.2323   0.07989   0.07547  -0.0593   0.9397   0.1570
  -8.000  -0.2213   0.07736   0.07294  -0.0596   0.9292   0.1616
  -7.750  -0.2276   0.07294   0.06835  -0.0678   0.9168   0.1706
  -7.500  -0.1949   0.06975   0.06522  -0.0677   0.9107   0.1741
  -7.250  -0.1945   0.06684   0.06200  -0.0733   0.8988   0.1870
  -7.000  -0.1597   0.06318   0.05850  -0.0730   0.8933   0.1909
  -6.750  -0.1341   0.05958   0.05464  -0.0786   0.8860   0.2060
  -6.500  -0.1143   0.05696   0.05209  -0.0774   0.8761   0.2095
  -6.250  -0.0852   0.04383   0.03715  -0.0873   0.8707   0.1231
  -6.000  -0.0755   0.04181   0.03519  -0.0847   0.8584   0.1203
  -5.750  -0.0386   0.03673   0.02903  -0.0867   0.8543   0.1106
  -5.500  -0.0202   0.03507   0.02713  -0.0850   0.8445   0.1103
  -5.250   0.0196   0.03265   0.02438  -0.0867   0.8388   0.1098
  -5.000   0.0682   0.03026   0.02157  -0.0895   0.8351   0.1103
  -4.750   0.0852   0.02936   0.02056  -0.0873   0.8239   0.1124
  -4.500   0.1297   0.02799   0.01915  -0.0894   0.8187   0.1171
  -4.250   0.1576   0.02705   0.01805  -0.0886   0.8094   0.1206
  -4.000   0.1955   0.02573   0.01661  -0.0894   0.8018   0.1255
  -3.750   0.2281   0.02492   0.01581  -0.0893   0.7928   0.1337
  -3.500   0.2622   0.02382   0.01472  -0.0894   0.7833   0.1424
  -3.250   0.2886   0.02306   0.01395  -0.0882   0.7714   0.1547
  -3.000   0.3268   0.02169   0.01272  -0.0889   0.7628   0.1764
  -2.750   0.3469   0.02070   0.01198  -0.0867   0.7483   0.2116
  -2.500   0.3689   0.01929   0.01117  -0.0848   0.7341   0.3198
  -2.250   0.5227   0.01627   0.00984  -0.1058   0.7127   1.0000
  -2.000   0.5427   0.01589   0.00923  -0.1035   0.6890   1.0000
  -1.750   0.5649   0.01555   0.00858  -0.1016   0.6607   1.0000
  -1.500   0.5865   0.01543   0.00810  -0.0997   0.6277   1.0000
  -1.250   0.6069   0.01559   0.00788  -0.0979   0.5953   1.0000
  -1.000   0.6279   0.01586   0.00777  -0.0963   0.5693   1.0000
  -0.750   0.6472   0.01619   0.00785  -0.0946   0.5475   1.0000
  -0.500   0.6684   0.01651   0.00792  -0.0932   0.5316   1.0000
  -0.250   0.6904   0.01684   0.00803  -0.0921   0.5189   1.0000
   0.000   0.7121   0.01720   0.00824  -0.0910   0.5080   1.0000
   0.250   0.7369   0.01757   0.00836  -0.0904   0.4999   1.0000
   0.500   0.7587   0.01796   0.00868  -0.0894   0.4919   1.0000
   0.750   0.7835   0.01834   0.00890  -0.0889   0.4855   1.0000
   1.000   0.8077   0.01879   0.00924  -0.0883   0.4801   1.0000
   1.250   0.8307   0.01923   0.00964  -0.0876   0.4746   1.0000
   1.500   0.8557   0.01967   0.00996  -0.0871   0.4698   1.0000
   1.750   0.8832   0.02017   0.01030  -0.0872   0.4657   1.0000
   2.000   0.9038   0.02068   0.01087  -0.0861   0.4615   1.0000
   2.250   0.9266   0.02120   0.01139  -0.0854   0.4577   1.0000
   2.500   0.9509   0.02174   0.01191  -0.0850   0.4544   1.0000
   2.750   0.9766   0.02230   0.01241  -0.0849   0.4516   1.0000
   3.000   1.0043   0.02293   0.01295  -0.0851   0.4491   1.0000
   3.250   1.0247   0.02359   0.01370  -0.0841   0.4463   1.0000
   3.500   1.0439   0.02425   0.01446  -0.0829   0.4431   1.0000
   3.750   1.0647   0.02491   0.01518  -0.0821   0.4398   1.0000
   4.000   1.0874   0.02553   0.01583  -0.0815   0.4365   1.0000
   4.250   1.1134   0.02616   0.01640  -0.0815   0.4332   1.0000
   4.500   1.1372   0.02692   0.01715  -0.0811   0.4299   1.0000
   4.750   1.1513   0.02771   0.01813  -0.0793   0.4264   1.0000
   5.000   1.1690   0.02851   0.01904  -0.0780   0.4231   1.0000
   5.250   1.1888   0.02931   0.01992  -0.0772   0.4202   1.0000
   5.500   1.2116   0.03006   0.02070  -0.0767   0.4173   1.0000
   5.750   1.2417   0.03077   0.02133  -0.0775   0.4137   1.0000
   6.000   1.2504   0.03185   0.02263  -0.0750   0.4107   1.0000
   6.250   1.2595   0.03290   0.02387  -0.0726   0.4068   1.0000
   6.500   1.2791   0.03353   0.02455  -0.0717   0.4018   1.0000
   6.750   1.3148   0.03381   0.02469  -0.0731   0.3964   1.0000
   7.000   1.3193   0.03501   0.02610  -0.0701   0.3924   1.0000
   7.250   1.3246   0.03607   0.02734  -0.0673   0.3875   1.0000
   7.500   1.3512   0.03635   0.02761  -0.0673   0.3818   1.0000
   7.750   1.3839   0.03685   0.02803  -0.0684   0.3769   1.0000
   8.000   1.3751   0.03836   0.02984  -0.0637   0.3729   1.0000
   8.250   1.3799   0.03945   0.03109  -0.0610   0.3682   1.0000
   8.500   1.4126   0.03954   0.03116  -0.0618   0.3628   1.0000
   8.750   1.4349   0.04026   0.03191  -0.0615   0.3581   1.0000
   9.000   1.4146   0.04219   0.03412  -0.0556   0.3540   1.0000
   9.250   1.4207   0.04305   0.03509  -0.0531   0.3487   1.0000
   9.500   1.4872   0.04185   0.03370  -0.0582   0.3414   1.0000
   9.750   1.4479   0.04415   0.03632  -0.0498   0.3377   1.0000
  10.000   1.4220   0.04621   0.03856  -0.0438   0.3332   1.0000
  10.250   1.5229   0.04330   0.03541  -0.0526   0.3240   1.0000
  10.500   1.4682   0.04615   0.03857  -0.0428   0.3208   1.0000
  10.750   1.4171   0.04995   0.04260  -0.0358   0.3164   1.0000
  11.000   1.4921   0.04680   0.03936  -0.0395   0.3088   1.0000
  11.250   1.4705   0.04909   0.04181  -0.0353   0.3039   1.0000
  11.500   1.0447   0.09995   0.09293  -0.0336   0.2723   1.0000
  11.750   1.1013   0.09363   0.08672  -0.0309   0.2731   1.0000
  12.000   1.1565   0.08740   0.08059  -0.0283   0.2732   1.0000
  12.250   1.2219   0.08026   0.07355  -0.0259   0.2729   1.0000
  12.500   1.3186   0.06998   0.06336  -0.0237   0.2720   1.0000
  13.000   1.3112   0.07487   0.06841  -0.0232   0.2577   1.0000
  13.750   0.9738   0.14399   0.13738  -0.0465   0.2100   1.0000
  14.000   0.9994   0.14228   0.13576  -0.0454   0.2047   1.0000
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