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GOE 735 AIRFOIL (goe735-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: GOE 735 AIRFOIL (goe735-il)
Reynolds number: 500,000
Max Cl/Cd: 78.9 at α=8.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe735-il-500000-n5.txt
Download as CSV file: xf-goe735-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 735 AIRFOIL                                 
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -18.500  -0.9384   0.08211   0.07822  -0.0509   1.0000   0.0357
 -18.250  -0.9824   0.07230   0.06824  -0.0569   1.0000   0.0359
 -18.000  -1.0217   0.06319   0.05895  -0.0626   1.0000   0.0359
 -17.750  -1.0520   0.05538   0.05096  -0.0677   1.0000   0.0362
 -17.500  -1.0764   0.04943   0.04487  -0.0703   0.9868   0.0363
 -17.250  -1.0473   0.04361   0.03874  -0.0823   0.8921   0.0371
 -17.000  -1.0536   0.04030   0.03512  -0.0836   0.8444   0.0375
 -16.750  -1.0605   0.03757   0.03219  -0.0837   0.8233   0.0379
 -16.500  -1.0648   0.03523   0.02969  -0.0833   0.8084   0.0383
 -16.250  -1.0704   0.03300   0.02734  -0.0824   0.7963   0.0387
 -16.000  -1.0725   0.03121   0.02543  -0.0812   0.7858   0.0392
 -15.750  -1.0717   0.02969   0.02381  -0.0797   0.7773   0.0397
 -15.500  -1.0689   0.02840   0.02242  -0.0780   0.7683   0.0404
 -15.250  -1.0640   0.02728   0.02120  -0.0763   0.7610   0.0411
 -15.000  -1.0576   0.02628   0.02011  -0.0744   0.7535   0.0419
 -14.750  -1.0497   0.02541   0.01913  -0.0724   0.7463   0.0425
 -14.500  -1.0426   0.02451   0.01817  -0.0703   0.7400   0.0433
 -14.250  -1.0339   0.02371   0.01731  -0.0682   0.7331   0.0441
 -14.000  -1.0236   0.02301   0.01654  -0.0661   0.7268   0.0452
 -13.750  -1.0115   0.02239   0.01585  -0.0641   0.7208   0.0463
 -13.500  -0.9983   0.02181   0.01520  -0.0621   0.7146   0.0476
 -13.250  -0.9859   0.02122   0.01456  -0.0600   0.7084   0.0486
 -13.000  -0.9719   0.02071   0.01399  -0.0580   0.7023   0.0501
 -12.750  -0.9564   0.02022   0.01345  -0.0561   0.6967   0.0516
 -12.500  -0.9405   0.01977   0.01294  -0.0542   0.6903   0.0530
 -12.250  -0.9246   0.01933   0.01246  -0.0523   0.6840   0.0546
 -12.000  -0.9073   0.01893   0.01201  -0.0505   0.6778   0.0563
 -11.750  -0.8891   0.01856   0.01158  -0.0488   0.6707   0.0580
 -11.500  -0.8715   0.01820   0.01117  -0.0470   0.6642   0.0597
 -11.250  -0.8528   0.01787   0.01081  -0.0453   0.6578   0.0616
 -11.000  -0.8334   0.01759   0.01047  -0.0437   0.6497   0.0636
 -10.750  -0.8145   0.01732   0.01013  -0.0420   0.6423   0.0652
 -10.500  -0.7946   0.01705   0.00984  -0.0405   0.6348   0.0670
 -10.250  -0.7736   0.01680   0.00954  -0.0391   0.6265   0.0688
 -10.000  -0.7513   0.01657   0.00923  -0.0380   0.6185   0.0706
  -9.750  -0.7293   0.01630   0.00892  -0.0368   0.6087   0.0721
  -9.500  -0.7068   0.01607   0.00864  -0.0357   0.5999   0.0738
  -9.250  -0.6835   0.01586   0.00838  -0.0347   0.5902   0.0757
  -9.000  -0.6599   0.01568   0.00811  -0.0337   0.5814   0.0776
  -8.750  -0.6363   0.01546   0.00784  -0.0328   0.5724   0.0791
  -8.500  -0.6130   0.01526   0.00759  -0.0318   0.5629   0.0808
  -8.250  -0.5888   0.01506   0.00736  -0.0309   0.5540   0.0825
  -8.000  -0.5645   0.01490   0.00713  -0.0301   0.5453   0.0842
  -7.750  -0.5395   0.01475   0.00691  -0.0294   0.5382   0.0858
  -7.500  -0.5151   0.01456   0.00668  -0.0285   0.5303   0.0876
  -7.250  -0.4907   0.01440   0.00648  -0.0277   0.5227   0.0893
  -7.000  -0.4655   0.01424   0.00630  -0.0271   0.5158   0.0913
  -6.750  -0.4400   0.01413   0.00613  -0.0264   0.5086   0.0935
  -6.500  -0.4142   0.01403   0.00596  -0.0258   0.5028   0.0954
  -6.250  -0.3894   0.01383   0.00577  -0.0251   0.4970   0.0978
  -6.000  -0.3641   0.01369   0.00561  -0.0244   0.4906   0.0998
  -5.750  -0.3387   0.01359   0.00545  -0.0238   0.4844   0.1017
  -5.500  -0.3126   0.01346   0.00529  -0.0233   0.4791   0.1036
  -5.250  -0.2864   0.01336   0.00514  -0.0227   0.4736   0.1053
  -5.000  -0.2614   0.01321   0.00498  -0.0220   0.4685   0.1075
  -4.750  -0.2357   0.01309   0.00484  -0.0214   0.4639   0.1096
  -4.500  -0.2095   0.01297   0.00472  -0.0209   0.4590   0.1120
  -4.250  -0.1833   0.01289   0.00460  -0.0204   0.4536   0.1144
  -4.000  -0.1572   0.01283   0.00449  -0.0199   0.4485   0.1166
  -3.750  -0.1315   0.01271   0.00437  -0.0194   0.4444   0.1194
  -3.500  -0.1052   0.01261   0.00428  -0.0189   0.4404   0.1225
  -3.250  -0.0788   0.01254   0.00419  -0.0184   0.4360   0.1258
  -3.000  -0.0525   0.01250   0.00411  -0.0180   0.4315   0.1289
  -2.750  -0.0269   0.01243   0.00403  -0.0174   0.4271   0.1331
  -2.500  -0.0003   0.01235   0.00397  -0.0170   0.4233   0.1375
  -2.250   0.0263   0.01230   0.00391  -0.0166   0.4192   0.1415
  -2.000   0.0522   0.01223   0.00385  -0.0161   0.4153   0.1472
  -1.750   0.0782   0.01220   0.00381  -0.0156   0.4115   0.1536
  -1.500   0.1041   0.01216   0.00377  -0.0151   0.4081   0.1607
  -1.250   0.1304   0.01209   0.00374  -0.0147   0.4049   0.1693
  -1.000   0.1564   0.01202   0.00371  -0.0142   0.4012   0.1793
  -0.750   0.1821   0.01197   0.00369  -0.0137   0.3972   0.1922
  -0.500   0.2071   0.01191   0.00368  -0.0131   0.3934   0.2115
  -0.250   0.2316   0.01184   0.00368  -0.0125   0.3901   0.2375
   0.000   0.2568   0.01173   0.00368  -0.0119   0.3875   0.2671
   0.250   0.2815   0.01162   0.00369  -0.0112   0.3845   0.3009
   0.500   0.3057   0.01152   0.00371  -0.0105   0.3813   0.3375
   0.750   0.3293   0.01142   0.00373  -0.0097   0.3781   0.3771
   1.000   0.3518   0.01131   0.00375  -0.0087   0.3748   0.4218
   1.250   0.3713   0.01110   0.00378  -0.0071   0.3718   0.4962
   1.500   0.3889   0.01080   0.00381  -0.0051   0.3692   0.5898
   1.750   0.4064   0.01056   0.00385  -0.0029   0.3664   0.6646
   2.000   0.4230   0.01032   0.00394  -0.0005   0.3638   0.7546
   2.250   0.4481   0.01026   0.00409   0.0003   0.3608   0.8197
   2.500   0.4851   0.01036   0.00430  -0.0015   0.3577   0.8655
   2.750   0.5274   0.01057   0.00452  -0.0044   0.3545   0.8952
   3.000   0.5767   0.01079   0.00477  -0.0087   0.3517   0.9158
   3.250   0.6147   0.01101   0.00499  -0.0106   0.3487   0.9309
   3.500   0.6590   0.01129   0.00524  -0.0139   0.3452   0.9382
   3.750   0.6814   0.01151   0.00543  -0.0128   0.3424   0.9485
   4.000   0.7195   0.01178   0.00565  -0.0150   0.3395   0.9509
   4.250   0.7565   0.01204   0.00588  -0.0169   0.3369   0.9542
   4.500   0.7911   0.01225   0.00610  -0.0183   0.3347   0.9594
   4.750   0.8194   0.01246   0.00630  -0.0185   0.3324   0.9651
   5.000   0.8553   0.01266   0.00648  -0.0203   0.3295   0.9668
   5.250   0.8894   0.01287   0.00667  -0.0218   0.3267   0.9691
   5.500   0.9207   0.01310   0.00688  -0.0229   0.3239   0.9719
   5.750   0.9474   0.01336   0.00710  -0.0230   0.3214   0.9756
   6.000   0.9730   0.01357   0.00732  -0.0229   0.3194   0.9790
   6.250   1.0058   0.01374   0.00751  -0.0242   0.3172   0.9803
   6.500   1.0371   0.01393   0.00771  -0.0253   0.3148   0.9819
   6.750   1.0675   0.01415   0.00793  -0.0263   0.3121   0.9838
   7.000   1.0967   0.01440   0.00816  -0.0270   0.3095   0.9863
   7.250   1.1236   0.01469   0.00843  -0.0274   0.3069   0.9890
   7.500   1.1472   0.01504   0.00876  -0.0273   0.3041   0.9917
   7.750   1.1780   0.01523   0.00899  -0.0284   0.3018   0.9932
   8.000   1.2080   0.01545   0.00924  -0.0295   0.2993   0.9951
   8.250   1.2369   0.01572   0.00952  -0.0304   0.2967   0.9972
   8.500   1.2639   0.01602   0.00983  -0.0310   0.2939   0.9992
   8.750   1.2733   0.01634   0.01016  -0.0284   0.2920   1.0000
   9.000   1.2682   0.01676   0.01060  -0.0234   0.2903   1.0000
   9.250   1.2672   0.01732   0.01116  -0.0194   0.2883   1.0000
   9.500   1.2739   0.01780   0.01168  -0.0167   0.2868   1.0000
   9.750   1.2825   0.01830   0.01222  -0.0143   0.2849   1.0000
  10.000   1.2913   0.01886   0.01282  -0.0122   0.2829   1.0000
  10.250   1.3000   0.01949   0.01348  -0.0102   0.2805   1.0000
  10.500   1.3089   0.02018   0.01418  -0.0083   0.2784   1.0000
  10.750   1.3175   0.02094   0.01495  -0.0065   0.2763   1.0000
  11.000   1.3255   0.02178   0.01581  -0.0048   0.2743   1.0000
  11.250   1.3336   0.02268   0.01671  -0.0032   0.2721   1.0000
  11.500   1.3459   0.02340   0.01749  -0.0020   0.2705   1.0000
  11.750   1.3570   0.02421   0.01835  -0.0008   0.2684   1.0000
  12.000   1.3673   0.02511   0.01929   0.0003   0.2661   1.0000
  12.250   1.3761   0.02613   0.02035   0.0014   0.2635   1.0000
  12.500   1.3842   0.02723   0.02147   0.0025   0.2611   1.0000
  12.750   1.3903   0.02850   0.02275   0.0037   0.2586   1.0000
  13.000   1.3983   0.02968   0.02396   0.0046   0.2565   1.0000
  13.250   1.4081   0.03080   0.02514   0.0054   0.2545   1.0000
  13.500   1.4171   0.03200   0.02640   0.0061   0.2522   1.0000
  13.750   1.4242   0.03338   0.02783   0.0068   0.2497   1.0000
  14.000   1.4302   0.03490   0.02939   0.0074   0.2471   1.0000
  14.250   1.4345   0.03660   0.03111   0.0080   0.2444   1.0000
  14.500   1.4381   0.03842   0.03295   0.0085   0.2417   1.0000
  14.750   1.4457   0.03997   0.03457   0.0089   0.2393   1.0000
  15.000   1.4484   0.04202   0.03669   0.0091   0.2355   1.0000
  15.250   1.4493   0.04426   0.03896   0.0094   0.2319   1.0000
  15.500   1.4481   0.04671   0.04141   0.0096   0.2283   1.0000
  15.750   1.4494   0.04904   0.04382   0.0097   0.2246   1.0000
  16.000   1.4483   0.05163   0.04647   0.0097   0.2205   1.0000
  16.250   1.4425   0.05471   0.04957   0.0097   0.2157   1.0000
  16.500   1.4397   0.05754   0.05243   0.0096   0.2123   1.0000
  16.750   1.4374   0.06038   0.05534   0.0094   0.2082   1.0000
  17.000   1.4291   0.06389   0.05888   0.0092   0.2030   1.0000
  17.250   1.4217   0.06736   0.06237   0.0088   0.1991   1.0000
  17.500   1.4195   0.07030   0.06538   0.0085   0.1955   1.0000
  17.750   1.4134   0.07371   0.06884   0.0080   0.1915   1.0000
  18.000   1.4027   0.07768   0.07281   0.0075   0.1872   1.0000
  18.250   1.3998   0.08079   0.07598   0.0069   0.1836   1.0000
  18.500   1.3923   0.08450   0.07975   0.0063   0.1796   1.0000
  18.750   1.3865   0.08801   0.08328   0.0056   0.1759   1.0000
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