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Rhode St. Genese 32 (rhodesg32-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: Rhode St. Genese 32 (rhodesg32-il)
Reynolds number: 500,000
Max Cl/Cd: 89.68 at α=5.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-rhodesg32-il-500000-n5.txt
Download as CSV file: xf-rhodesg32-il-500000-n5.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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.250  -0.8739   0.03426   0.03108  -0.0884   0.9975   0.0273
 -14.000  -0.8574   0.03164   0.02822  -0.0902   0.9900   0.0279
 -13.750  -0.8229   0.03216   0.02882  -0.0908   0.9863   0.0282
 -13.500  -0.7901   0.03229   0.02897  -0.0917   0.9817   0.0285
 -13.250  -0.7575   0.03243   0.02912  -0.0924   0.9754   0.0289
 -13.000  -0.7267   0.03175   0.02837  -0.0940   0.9695   0.0293
 -12.750  -0.6997   0.03021   0.02665  -0.0958   0.9621   0.0300
 -12.500  -0.6831   0.02647   0.02241  -0.0978   0.9524   0.0313
 -12.250  -0.6602   0.02387   0.01936  -0.0992   0.9442   0.0322
 -12.000  -0.6303   0.02346   0.01892  -0.0999   0.9354   0.0327
 -11.750  -0.5990   0.02328   0.01870  -0.1007   0.9281   0.0331
 -11.500  -0.5726   0.02298   0.01835  -0.1006   0.9193   0.0334
 -11.000  -0.5234   0.02207   0.01723  -0.0998   0.9039   0.0344
 -10.750  -0.5007   0.02132   0.01630  -0.0991   0.8956   0.0350
 -10.500  -0.4800   0.02045   0.01525  -0.0981   0.8871   0.0357
 -10.000  -0.4368   0.01861   0.01299  -0.0962   0.8726   0.0369
  -9.750  -0.4135   0.01799   0.01217  -0.0953   0.8649   0.0374
  -9.500  -0.3908   0.01724   0.01134  -0.0945   0.8571   0.0379
  -9.250  -0.3666   0.01680   0.01082  -0.0937   0.8487   0.0383
  -9.000  -0.3421   0.01637   0.01033  -0.0930   0.8406   0.0387
  -8.750  -0.3173   0.01597   0.00984  -0.0923   0.8330   0.0391
  -8.500  -0.2924   0.01554   0.00934  -0.0916   0.8249   0.0396
  -8.250  -0.2675   0.01515   0.00884  -0.0909   0.8154   0.0401
  -8.000  -0.2427   0.01474   0.00833  -0.0901   0.8031   0.0406
  -7.750  -0.2178   0.01436   0.00785  -0.0894   0.7898   0.0413
  -7.500  -0.1926   0.01401   0.00738  -0.0886   0.7770   0.0420
  -7.250  -0.1675   0.01367   0.00692  -0.0879   0.7631   0.0426
  -7.000  -0.1425   0.01336   0.00648  -0.0871   0.7477   0.0430
  -6.750  -0.1175   0.01308   0.00608  -0.0863   0.7305   0.0434
  -6.500  -0.0929   0.01272   0.00561  -0.0855   0.7136   0.0439
  -6.250  -0.0687   0.01236   0.00516  -0.0847   0.6953   0.0445
  -6.000  -0.0442   0.01215   0.00486  -0.0839   0.6755   0.0451
  -5.750  -0.0194   0.01199   0.00461  -0.0831   0.6566   0.0458
  -5.500   0.0053   0.01188   0.00440  -0.0823   0.6361   0.0465
  -5.250   0.0299   0.01178   0.00419  -0.0815   0.6135   0.0473
  -5.000   0.0542   0.01170   0.00399  -0.0806   0.5877   0.0482
  -4.750   0.0778   0.01165   0.00378  -0.0796   0.5529   0.0489
  -4.500   0.1001   0.01171   0.00361  -0.0784   0.4997   0.0496
  -4.250   0.1197   0.01203   0.00355  -0.0768   0.4153   0.0503
  -4.000   0.1430   0.01213   0.00346  -0.0759   0.3797   0.0508
  -3.750   0.1677   0.01210   0.00334  -0.0752   0.3627   0.0515
  -3.500   0.1922   0.01196   0.00314  -0.0744   0.3523   0.0527
  -3.250   0.2178   0.01188   0.00304  -0.0739   0.3450   0.0541
  -2.750   0.2693   0.01180   0.00289  -0.0729   0.3349   0.0567
  -2.500   0.2953   0.01176   0.00283  -0.0724   0.3313   0.0580
  -2.250   0.3212   0.01174   0.00279  -0.0719   0.3278   0.0592
  -2.000   0.3471   0.01175   0.00276  -0.0715   0.3247   0.0603
  -1.500   0.3987   0.01170   0.00270  -0.0705   0.3199   0.0653
  -1.250   0.4248   0.01169   0.00269  -0.0701   0.3181   0.0682
  -1.000   0.4510   0.01169   0.00269  -0.0697   0.3163   0.0713
  -0.750   0.4768   0.01167   0.00270  -0.0692   0.3140   0.0794
  -0.500   0.5017   0.01157   0.00276  -0.0687   0.3113   0.1377
  -0.250   0.5271   0.01159   0.00282  -0.0682   0.3086   0.1608
   0.250   0.5764   0.01151   0.00299  -0.0671   0.3048   0.2533
   0.500   0.5914   0.01056   0.00314  -0.0650   0.3033   0.6336
   0.750   0.6549   0.00997   0.00343  -0.0724   0.3004   0.9689
   1.000   0.7098   0.01014   0.00356  -0.0784   0.2979   0.9979
   1.250   0.7386   0.01027   0.00366  -0.0787   0.2960   1.0000
   1.500   0.7615   0.01039   0.00376  -0.0777   0.2940   1.0000
   1.750   0.7844   0.01052   0.00386  -0.0768   0.2923   1.0000
   2.000   0.8072   0.01067   0.00399  -0.0758   0.2909   1.0000
   2.250   0.8301   0.01082   0.00411  -0.0748   0.2895   1.0000
   2.500   0.8527   0.01098   0.00426  -0.0739   0.2880   1.0000
   2.750   0.8756   0.01115   0.00441  -0.0730   0.2867   1.0000
   3.000   0.8994   0.01125   0.00454  -0.0722   0.2852   1.0000
   3.250   0.9233   0.01134   0.00464  -0.0715   0.2823   1.0000
   3.500   0.9468   0.01145   0.00476  -0.0708   0.2786   1.0000
   3.750   0.9699   0.01160   0.00490  -0.0699   0.2755   1.0000
   4.000   0.9926   0.01176   0.00505  -0.0691   0.2730   1.0000
   4.250   1.0155   0.01192   0.00521  -0.0682   0.2700   1.0000
   4.500   1.0393   0.01204   0.00536  -0.0676   0.2669   1.0000
   4.750   1.0626   0.01217   0.00552  -0.0668   0.2635   1.0000
   5.000   1.0853   0.01233   0.00568  -0.0660   0.2591   1.0000
   5.250   1.1079   0.01250   0.00585  -0.0652   0.2538   1.0000
   5.500   1.1304   0.01266   0.00601  -0.0644   0.2442   1.0000
   5.750   1.1524   0.01285   0.00620  -0.0635   0.2346   1.0000
   6.000   1.1617   0.01373   0.00666  -0.0607   0.1655   1.0000
   6.250   1.1758   0.01436   0.00720  -0.0586   0.1491   1.0000
   6.500   1.1921   0.01478   0.00760  -0.0568   0.1411   1.0000
   6.750   1.2075   0.01523   0.00804  -0.0548   0.1340   1.0000
   7.000   1.2245   0.01560   0.00843  -0.0532   0.1283   1.0000
   7.250   1.2404   0.01605   0.00888  -0.0514   0.1226   1.0000
   7.500   1.2570   0.01646   0.00931  -0.0499   0.1179   1.0000
   7.750   1.2738   0.01688   0.00975  -0.0484   0.1126   1.0000
   8.000   1.2883   0.01744   0.01029  -0.0466   0.1055   1.0000
   8.250   1.3039   0.01794   0.01079  -0.0451   0.0958   1.0000
   8.500   1.3074   0.01915   0.01176  -0.0420   0.0617   1.0000
   8.750   1.3164   0.02006   0.01263  -0.0398   0.0548   1.0000
   9.000   1.3284   0.02080   0.01342  -0.0381   0.0511   1.0000
   9.250   1.3401   0.02159   0.01425  -0.0364   0.0486   1.0000
   9.500   1.3503   0.02250   0.01520  -0.0347   0.0464   1.0000
   9.750   1.3597   0.02349   0.01623  -0.0330   0.0443   1.0000
  10.000   1.3723   0.02429   0.01710  -0.0317   0.0430   1.0000
  10.250   1.3830   0.02524   0.01812  -0.0303   0.0416   1.0000
  10.500   1.3922   0.02634   0.01928  -0.0289   0.0400   1.0000
  10.750   1.3998   0.02759   0.02058  -0.0275   0.0386   1.0000
  11.000   1.4050   0.02908   0.02212  -0.0261   0.0371   1.0000
  11.250   1.4139   0.03034   0.02346  -0.0251   0.0362   1.0000
  11.500   1.4220   0.03170   0.02490  -0.0241   0.0349   1.0000
  11.750   1.4279   0.03331   0.02658  -0.0232   0.0336   1.0000
  12.000   1.4323   0.03513   0.02845  -0.0224   0.0323   1.0000
  12.250   1.4344   0.03722   0.03061  -0.0216   0.0312   1.0000
  12.500   1.4378   0.03929   0.03276  -0.0211   0.0303   1.0000
  12.750   1.4415   0.04141   0.03497  -0.0208   0.0290   1.0000
  13.000   1.4428   0.04387   0.03751  -0.0205   0.0278   1.0000
  13.250   1.4419   0.04665   0.04036  -0.0204   0.0268   1.0000
  13.500   1.4386   0.04985   0.04365  -0.0206   0.0259   1.0000
  13.750   1.4377   0.05286   0.04676  -0.0208   0.0249   1.0000
  14.000   1.4340   0.05631   0.05031  -0.0213   0.0240   1.0000
  14.250   1.4289   0.06008   0.05417  -0.0219   0.0232   1.0000
  14.500   1.4219   0.06420   0.05839  -0.0228   0.0223   1.0000
  14.750   1.4130   0.06870   0.06297  -0.0239   0.0217   1.0000
  15.000   1.4053   0.07314   0.06752  -0.0250   0.0211   1.0000
  15.250   1.3975   0.07767   0.07216  -0.0263   0.0204   1.0000
  15.500   1.3892   0.08231   0.07689  -0.0277   0.0197   1.0000
  15.750   1.3811   0.08693   0.08160  -0.0290   0.0190   1.0000
  16.000   1.3729   0.09159   0.08632  -0.0305   0.0183   1.0000
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