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Rhode St. Genese 32 (rhodesg32-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: Rhode St. Genese 32 (rhodesg32-il)
Reynolds number: 1,000,000
Max Cl/Cd: 107.96 at α=4.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-rhodesg32-il-1000000-n5.txt
Download as CSV file: xf-rhodesg32-il-1000000-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 =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -17.750  -1.1643   0.03198   0.02894  -0.1074   1.0000   0.0157
 -17.500  -1.1782   0.03005   0.02688  -0.1039   1.0000   0.0160
 -17.250  -1.1819   0.02847   0.02518  -0.1009   1.0000   0.0164
 -17.000  -1.1794   0.02707   0.02367  -0.0983   1.0000   0.0168
 -16.750  -1.1751   0.02575   0.02227  -0.0956   1.0000   0.0175
 -16.500  -1.1677   0.02466   0.02110  -0.0931   1.0000   0.0181
 -16.250  -1.1457   0.02352   0.01986  -0.0932   0.9986   0.0192
 -16.000  -1.1201   0.02247   0.01870  -0.0938   0.9954   0.0200
 -15.750  -1.0952   0.02164   0.01782  -0.0940   0.9910   0.0209
 -15.500  -1.0688   0.02091   0.01704  -0.0942   0.9866   0.0218
 -15.250  -1.0408   0.02019   0.01625  -0.0948   0.9831   0.0227
 -15.000  -1.0151   0.01948   0.01543  -0.0948   0.9771   0.0233
 -14.750  -0.9848   0.01881   0.01468  -0.0956   0.9731   0.0239
 -14.500  -0.9520   0.01831   0.01415  -0.0968   0.9682   0.0246
 -14.250  -0.9162   0.01785   0.01366  -0.0985   0.9615   0.0253
 -14.000  -0.8782   0.01740   0.01313  -0.1007   0.9520   0.0262
 -13.750  -0.8429   0.01687   0.01249  -0.1023   0.9397   0.0269
 -13.250  -0.7889   0.01598   0.01136  -0.1021   0.9172   0.0278
 -13.000  -0.7646   0.01562   0.01093  -0.1014   0.9069   0.0283
 -12.750  -0.7394   0.01542   0.01070  -0.1007   0.8987   0.0288
 -12.500  -0.7142   0.01524   0.01047  -0.1000   0.8923   0.0293
 -12.250  -0.6894   0.01499   0.01016  -0.0993   0.8860   0.0298
 -11.750  -0.6394   0.01449   0.00953  -0.0979   0.8741   0.0308
 -11.500  -0.6144   0.01425   0.00922  -0.0971   0.8669   0.0314
 -11.250  -0.5894   0.01399   0.00888  -0.0964   0.8593   0.0318
 -11.000  -0.5640   0.01378   0.00858  -0.0957   0.8519   0.0321
 -10.750  -0.5401   0.01334   0.00808  -0.0948   0.8455   0.0327
 -10.500  -0.5150   0.01304   0.00774  -0.0941   0.8385   0.0331
 -10.250  -0.4898   0.01280   0.00743  -0.0934   0.8312   0.0335
 -10.000  -0.4640   0.01256   0.00715  -0.0928   0.8233   0.0338
  -9.750  -0.4383   0.01239   0.00693  -0.0921   0.8136   0.0343
  -9.500  -0.4126   0.01218   0.00666  -0.0915   0.8032   0.0347
  -9.250  -0.3871   0.01195   0.00636  -0.0908   0.7923   0.0351
  -9.000  -0.3620   0.01172   0.00603  -0.0900   0.7781   0.0355
  -8.750  -0.3370   0.01150   0.00572  -0.0892   0.7623   0.0359
  -8.500  -0.3120   0.01129   0.00541  -0.0885   0.7454   0.0363
  -8.250  -0.2869   0.01112   0.00513  -0.0877   0.7265   0.0366
  -8.000  -0.2616   0.01095   0.00486  -0.0869   0.7096   0.0369
  -7.750  -0.2361   0.01083   0.00464  -0.0863   0.6922   0.0372
  -7.500  -0.2111   0.01065   0.00437  -0.0855   0.6731   0.0376
  -7.250  -0.1867   0.01044   0.00406  -0.0846   0.6524   0.0382
  -7.000  -0.1614   0.01033   0.00386  -0.0839   0.6332   0.0387
  -6.750  -0.1357   0.01022   0.00368  -0.0833   0.6163   0.0392
  -6.500  -0.1099   0.01014   0.00352  -0.0827   0.5973   0.0396
  -6.250  -0.0845   0.01010   0.00338  -0.0820   0.5727   0.0401
  -6.000  -0.0595   0.01009   0.00325  -0.0813   0.5410   0.0407
  -5.750  -0.0400   0.01048   0.00320  -0.0796   0.4303   0.0411
  -5.500  -0.0171   0.01067   0.00314  -0.0785   0.3720   0.0417
  -5.250   0.0085   0.01065   0.00303  -0.0779   0.3524   0.0422
  -4.750   0.0613   0.01059   0.00286  -0.0770   0.3336   0.0433
  -4.500   0.0880   0.01054   0.00276  -0.0766   0.3280   0.0436
  -4.000   0.1406   0.01031   0.00248  -0.0757   0.3194   0.0454
  -3.750   0.1674   0.01025   0.00241  -0.0754   0.3166   0.0462
  -3.500   0.1942   0.01020   0.00235  -0.0750   0.3138   0.0470
  -3.250   0.2210   0.01016   0.00229  -0.0746   0.3110   0.0479
  -3.000   0.2477   0.01013   0.00225  -0.0743   0.3084   0.0488
  -2.750   0.2745   0.01012   0.00222  -0.0739   0.3056   0.0497
  -2.500   0.3013   0.01011   0.00219  -0.0736   0.3036   0.0506
  -2.250   0.3284   0.01009   0.00217  -0.0733   0.3024   0.0511
  -2.000   0.3551   0.01003   0.00211  -0.0730   0.3012   0.0525
  -1.750   0.3819   0.01000   0.00208  -0.0727   0.2995   0.0542
  -1.500   0.4087   0.00998   0.00207  -0.0724   0.2972   0.0558
  -1.250   0.4353   0.00999   0.00207  -0.0721   0.2945   0.0574
  -1.000   0.4619   0.01000   0.00208  -0.0718   0.2922   0.0593
  -0.750   0.4884   0.01003   0.00210  -0.0714   0.2897   0.0608
  -0.500   0.5147   0.01005   0.00212  -0.0711   0.2875   0.0652
  -0.250   0.5414   0.01005   0.00215  -0.0708   0.2864   0.0704
   0.000   0.5673   0.00994   0.00218  -0.0704   0.2851   0.1220
   0.250   0.5938   0.00993   0.00224  -0.0702   0.2839   0.1450
   0.500   0.6203   0.00994   0.00229  -0.0699   0.2828   0.1576
   0.750   0.6467   0.00996   0.00234  -0.0696   0.2813   0.1706
   1.000   0.6728   0.00995   0.00240  -0.0693   0.2795   0.1962
   1.250   0.6880   0.00894   0.00255  -0.0673   0.2780   0.6413
   1.500   0.7011   0.00834   0.00269  -0.0640   0.2768   0.8860
   1.750   0.7837   0.00848   0.00292  -0.0761   0.2740   0.9841
   2.000   0.8257   0.00864   0.00306  -0.0794   0.2718   0.9978
   2.250   0.8597   0.00874   0.00314  -0.0808   0.2696   1.0000
   2.500   0.8836   0.00882   0.00322  -0.0801   0.2668   1.0000
   2.750   0.9072   0.00892   0.00331  -0.0793   0.2638   1.0000
   3.000   0.9306   0.00903   0.00340  -0.0784   0.2606   1.0000
   3.250   0.9536   0.00917   0.00350  -0.0776   0.2566   1.0000
   3.500   0.9775   0.00927   0.00361  -0.0768   0.2534   1.0000
   3.750   1.0011   0.00939   0.00372  -0.0761   0.2492   1.0000
   4.000   1.0240   0.00955   0.00383  -0.0752   0.2425   1.0000
   4.250   1.0472   0.00970   0.00396  -0.0745   0.2343   1.0000
   4.500   1.0575   0.01057   0.00444  -0.0715   0.1653   1.0000
   4.750   1.0750   0.01105   0.00482  -0.0698   0.1463   1.0000
   5.250   1.1160   0.01166   0.00537  -0.0674   0.1300   1.0000
   5.500   1.1368   0.01194   0.00562  -0.0663   0.1246   1.0000
   5.750   1.1576   0.01222   0.00588  -0.0652   0.1193   1.0000
   6.000   1.1787   0.01246   0.00613  -0.0641   0.1150   1.0000
   6.250   1.1991   0.01275   0.00640  -0.0630   0.1105   1.0000
   6.500   1.2189   0.01305   0.00668  -0.0618   0.1053   1.0000
   6.750   1.2392   0.01330   0.00694  -0.0607   0.1017   1.0000
   7.250   1.2635   0.01446   0.00785  -0.0556   0.0613   1.0000
   7.500   1.2766   0.01499   0.00834  -0.0534   0.0527   1.0000
   7.750   1.2920   0.01543   0.00879  -0.0515   0.0491   1.0000
   8.000   1.3068   0.01591   0.00928  -0.0497   0.0456   1.0000
   8.250   1.3234   0.01632   0.00971  -0.0482   0.0437   1.0000
   8.500   1.3400   0.01674   0.01015  -0.0467   0.0423   1.0000
   8.750   1.3558   0.01721   0.01064  -0.0452   0.0407   1.0000
   9.000   1.3703   0.01777   0.01122  -0.0436   0.0387   1.0000
   9.250   1.3846   0.01835   0.01182  -0.0421   0.0370   1.0000
   9.500   1.4004   0.01886   0.01237  -0.0408   0.0362   1.0000
   9.750   1.4154   0.01943   0.01297  -0.0395   0.0349   1.0000
  10.000   1.4296   0.02008   0.01365  -0.0382   0.0335   1.0000
  10.250   1.4424   0.02082   0.01441  -0.0368   0.0322   1.0000
  10.500   1.4547   0.02162   0.01524  -0.0355   0.0309   1.0000
  10.750   1.4684   0.02236   0.01602  -0.0343   0.0296   1.0000
  11.000   1.4809   0.02321   0.01690  -0.0332   0.0285   1.0000
  11.250   1.4916   0.02419   0.01791  -0.0320   0.0269   1.0000
  11.500   1.5019   0.02526   0.01901  -0.0308   0.0256   1.0000
  11.750   1.5126   0.02631   0.02012  -0.0298   0.0245   1.0000
  12.000   1.5217   0.02754   0.02138  -0.0287   0.0229   1.0000
  12.250   1.5293   0.02893   0.02279  -0.0277   0.0215   1.0000
  12.500   1.5367   0.03037   0.02429  -0.0268   0.0200   1.0000
  12.750   1.5425   0.03201   0.02597  -0.0260   0.0187   1.0000
  13.000   1.5469   0.03385   0.02786  -0.0252   0.0175   1.0000
  13.250   1.5508   0.03579   0.02985  -0.0246   0.0164   1.0000
  13.500   1.5528   0.03800   0.03212  -0.0241   0.0154   1.0000
  13.750   1.5532   0.04047   0.03465  -0.0237   0.0146   1.0000
  14.000   1.5540   0.04299   0.03725  -0.0235   0.0141   1.0000
  14.250   1.5531   0.04578   0.04013  -0.0234   0.0134   1.0000
  14.500   1.5500   0.04893   0.04336  -0.0235   0.0129   1.0000
  14.750   1.5458   0.05232   0.04682  -0.0238   0.0125   1.0000
  15.000   1.5396   0.05602   0.05062  -0.0242   0.0121   1.0000
  15.250   1.5309   0.06017   0.05486  -0.0249   0.0118   1.0000
  15.500   1.5234   0.06428   0.05907  -0.0257   0.0115   1.0000
  15.750   1.5142   0.06871   0.06359  -0.0266   0.0112   1.0000
  16.000   1.5038   0.07338   0.06837  -0.0277   0.0111   1.0000
  16.250   1.4924   0.07828   0.07337  -0.0289   0.0107   1.0000
  16.500   1.4811   0.08318   0.07836  -0.0302   0.0106   1.0000
  16.750   1.4694   0.08812   0.08339  -0.0315   0.0103   1.0000
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