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Rhode St. Genese 34 (rhodesg34-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: Rhode St. Genese 34 (rhodesg34-il)
Reynolds number: 500,000
Max Cl/Cd: 81.93 at α=5.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-rhodesg34-il-500000-n5.txt
Download as CSV file: xf-rhodesg34-il-500000-n5.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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.750  -0.4869   0.03687   0.03326  -0.1333   0.8800   0.0278
 -13.500  -0.5299   0.03256   0.02852  -0.1303   0.8614   0.0279
 -13.250  -0.5442   0.03012   0.02575  -0.1269   0.8506   0.0281
 -13.000  -0.5480   0.02790   0.02323  -0.1242   0.8426   0.0284
 -12.750  -0.5435   0.02615   0.02119  -0.1219   0.8359   0.0286
 -12.500  -0.5340   0.02467   0.01946  -0.1199   0.8303   0.0288
 -12.250  -0.5210   0.02341   0.01798  -0.1182   0.8255   0.0290
 -12.000  -0.5051   0.02236   0.01673  -0.1167   0.8211   0.0291
 -11.750  -0.4881   0.02133   0.01553  -0.1152   0.8170   0.0293
 -11.500  -0.4693   0.02047   0.01457  -0.1139   0.8127   0.0295
 -11.250  -0.4486   0.01981   0.01384  -0.1128   0.8086   0.0297
 -11.000  -0.4271   0.01921   0.01316  -0.1117   0.8045   0.0299
 -10.750  -0.4049   0.01868   0.01253  -0.1107   0.7999   0.0301
 -10.500  -0.3823   0.01815   0.01192  -0.1097   0.7961   0.0304
 -10.250  -0.3594   0.01761   0.01133  -0.1088   0.7917   0.0307
 -10.000  -0.3361   0.01710   0.01074  -0.1079   0.7878   0.0310
  -9.750  -0.3126   0.01659   0.01013  -0.1070   0.7837   0.0312
  -9.500  -0.2888   0.01611   0.00955  -0.1061   0.7793   0.0316
  -9.250  -0.2647   0.01563   0.00901  -0.1052   0.7743   0.0320
  -9.000  -0.2405   0.01520   0.00848  -0.1044   0.7685   0.0324
  -8.750  -0.2160   0.01481   0.00799  -0.1035   0.7624   0.0328
  -8.500  -0.1912   0.01442   0.00753  -0.1027   0.7558   0.0332
  -8.250  -0.1669   0.01397   0.00704  -0.1019   0.7494   0.0336
  -8.000  -0.1421   0.01361   0.00666  -0.1011   0.7427   0.0340
  -7.750  -0.1170   0.01330   0.00631  -0.1004   0.7342   0.0344
  -7.500  -0.0918   0.01302   0.00600  -0.0996   0.7260   0.0349
  -7.250  -0.0668   0.01274   0.00567  -0.0988   0.7139   0.0354
  -7.000  -0.0421   0.01249   0.00535  -0.0979   0.6978   0.0359
  -6.750  -0.0182   0.01228   0.00502  -0.0969   0.6788   0.0365
  -6.500   0.0055   0.01211   0.00473  -0.0958   0.6579   0.0372
  -6.250   0.0290   0.01199   0.00447  -0.0947   0.6374   0.0377
  -6.000   0.0523   0.01184   0.00424  -0.0936   0.6186   0.0385
  -5.750   0.0763   0.01177   0.00408  -0.0927   0.6007   0.0393
  -5.500   0.1006   0.01172   0.00395  -0.0917   0.5828   0.0404
  -5.250   0.1249   0.01165   0.00379  -0.0908   0.5640   0.0415
  -5.000   0.1487   0.01162   0.00365  -0.0898   0.5392   0.0426
  -4.750   0.1698   0.01166   0.00352  -0.0884   0.4946   0.0437
  -4.500   0.1888   0.01190   0.00350  -0.0866   0.4372   0.0449
  -4.250   0.2104   0.01204   0.00348  -0.0853   0.4053   0.0464
  -4.000   0.2339   0.01210   0.00343  -0.0843   0.3867   0.0480
  -3.750   0.2576   0.01211   0.00339  -0.0833   0.3735   0.0500
  -3.500   0.2823   0.01211   0.00335  -0.0826   0.3638   0.0524
  -3.000   0.3316   0.01210   0.00328  -0.0811   0.3499   0.0577
  -2.750   0.3566   0.01211   0.00326  -0.0804   0.3444   0.0607
  -2.500   0.3810   0.01211   0.00323  -0.0796   0.3394   0.0639
  -2.250   0.4057   0.01213   0.00323  -0.0789   0.3351   0.0680
  -2.000   0.4306   0.01209   0.00320  -0.0783   0.3318   0.0731
  -1.750   0.4552   0.01207   0.00319  -0.0776   0.3280   0.0816
  -1.500   0.4787   0.01197   0.00325  -0.0767   0.3242   0.1300
  -1.250   0.5028   0.01203   0.00332  -0.0759   0.3206   0.1476
  -1.000   0.5269   0.01211   0.00338  -0.0752   0.3172   0.1580
  -0.750   0.5518   0.01211   0.00342  -0.0746   0.3148   0.1685
  -0.500   0.5766   0.01214   0.00346  -0.0739   0.3118   0.1770
  -0.250   0.6009   0.01217   0.00352  -0.0732   0.3094   0.1883
   0.000   0.6245   0.01218   0.00360  -0.0724   0.3072   0.2114
   0.250   0.6467   0.01207   0.00370  -0.0714   0.3054   0.2908
   0.500   0.6629   0.01154   0.00384  -0.0695   0.3036   0.5340
   1.000   0.8013   0.01119   0.00456  -0.0873   0.2984   0.9996
   1.250   0.8240   0.01130   0.00466  -0.0863   0.2973   1.0000
   1.500   0.8449   0.01142   0.00475  -0.0850   0.2959   1.0000
   1.750   0.8658   0.01154   0.00486  -0.0837   0.2939   1.0000
   2.000   0.8864   0.01167   0.00497  -0.0823   0.2913   1.0000
   2.250   0.9067   0.01181   0.00509  -0.0809   0.2890   1.0000
   2.500   0.9266   0.01198   0.00522  -0.0794   0.2866   1.0000
   2.750   0.9462   0.01216   0.00536  -0.0779   0.2843   1.0000
   3.000   0.9654   0.01235   0.00553  -0.0764   0.2824   1.0000
   3.250   0.9853   0.01251   0.00569  -0.0749   0.2806   1.0000
   3.500   1.0049   0.01263   0.00582  -0.0734   0.2786   1.0000
   3.750   1.0236   0.01277   0.00597  -0.0718   0.2765   1.0000
   4.000   1.0422   0.01293   0.00612  -0.0701   0.2735   1.0000
   4.250   1.0604   0.01310   0.00630  -0.0685   0.2707   1.0000
   4.500   1.0787   0.01331   0.00648  -0.0669   0.2683   1.0000
   4.750   1.0968   0.01354   0.00670  -0.0653   0.2659   1.0000
   5.000   1.1165   0.01373   0.00691  -0.0640   0.2640   1.0000
   5.250   1.1369   0.01392   0.00712  -0.0629   0.2615   1.0000
   5.500   1.1569   0.01412   0.00735  -0.0618   0.2582   1.0000
   5.750   1.1760   0.01437   0.00759  -0.0605   0.2541   1.0000
   6.000   1.1940   0.01466   0.00786  -0.0592   0.2490   1.0000
   6.250   1.2141   0.01490   0.00813  -0.0582   0.2442   1.0000
   6.500   1.2325   0.01521   0.00842  -0.0570   0.2375   1.0000
   6.750   1.2507   0.01555   0.00876  -0.0558   0.2295   1.0000
   7.000   1.2663   0.01602   0.00916  -0.0543   0.2131   1.0000
   7.250   1.2589   0.01778   0.01048  -0.0500   0.1500   1.0000
   7.500   1.2685   0.01871   0.01134  -0.0480   0.1359   1.0000
   7.750   1.2817   0.01946   0.01208  -0.0466   0.1292   1.0000
   8.000   1.2960   0.02016   0.01279  -0.0453   0.1238   1.0000
   8.250   1.3091   0.02095   0.01357  -0.0440   0.1188   1.0000
   8.500   1.3231   0.02170   0.01433  -0.0428   0.1147   1.0000
   8.750   1.3369   0.02248   0.01514  -0.0417   0.1104   1.0000
   9.000   1.3492   0.02338   0.01605  -0.0406   0.1063   1.0000
   9.250   1.3625   0.02423   0.01692  -0.0395   0.1026   1.0000
   9.500   1.3752   0.02513   0.01784  -0.0385   0.0973   1.0000
   9.750   1.3861   0.02619   0.01892  -0.0374   0.0916   1.0000
  10.250   1.3879   0.02985   0.02241  -0.0340   0.0585   1.0000
  10.500   1.3933   0.03142   0.02402  -0.0328   0.0558   1.0000
  10.750   1.4000   0.03295   0.02560  -0.0318   0.0543   1.0000
  11.000   1.4067   0.03452   0.02724  -0.0309   0.0533   1.0000
  11.250   1.4120   0.03627   0.02906  -0.0301   0.0523   1.0000
  11.500   1.4161   0.03819   0.03105  -0.0294   0.0514   1.0000
  11.750   1.4185   0.04036   0.03330  -0.0288   0.0507   1.0000
  12.000   1.4192   0.04280   0.03581  -0.0282   0.0499   1.0000
  12.250   1.4179   0.04554   0.03864  -0.0278   0.0492   1.0000
  12.500   1.4159   0.04846   0.04165  -0.0276   0.0486   1.0000
  12.750   1.4176   0.05107   0.04435  -0.0276   0.0479   1.0000
  13.000   1.4169   0.05401   0.04739  -0.0276   0.0473   1.0000
  13.250   1.4137   0.05731   0.05079  -0.0278   0.0465   1.0000
  13.500   1.4083   0.06096   0.05454  -0.0281   0.0460   1.0000
  13.750   1.4009   0.06498   0.05867  -0.0286   0.0454   1.0000
  14.000   1.3914   0.06939   0.06318  -0.0293   0.0449   1.0000
  14.250   1.3801   0.07414   0.06804  -0.0301   0.0445   1.0000
  14.500   1.3690   0.07895   0.07296  -0.0311   0.0442   1.0000
  14.750   1.3557   0.08413   0.07824  -0.0322   0.0437   1.0000
  15.000   1.3436   0.08913   0.08333  -0.0333   0.0433   1.0000
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