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GOE 723 AIRFOIL (goe723-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: GOE 723 AIRFOIL (goe723-il)
Reynolds number: 500,000
Max Cl/Cd: 114.05 at α=5.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe723-il-500000.txt
Download as CSV file: xf-goe723-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 723 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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -10.500  -0.2617   0.09750   0.09525  -0.0445   1.0000   0.0336
 -10.250  -0.2566   0.09549   0.09326  -0.0435   1.0000   0.0338
 -10.000  -0.2537   0.09340   0.09121  -0.0425   1.0000   0.0341
  -9.750  -0.2448   0.09023   0.08805  -0.0438   0.9991   0.0346
  -9.500  -0.2313   0.08620   0.08402  -0.0470   0.9970   0.0353
  -9.250  -0.2201   0.08165   0.07946  -0.0506   0.9937   0.0363
  -9.000  -0.2135   0.07640   0.07420  -0.0547   0.9889   0.0376
  -8.750  -0.3243   0.08645   0.08418  -0.0434   0.9992   0.0354
  -8.500  -0.3064   0.08181   0.07954  -0.0495   0.9955   0.0365
  -8.250  -0.3242   0.06308   0.06081  -0.0743   0.9752   0.0396
  -8.000  -0.3034   0.06112   0.05885  -0.0766   0.9641   0.0399
  -7.750  -0.2799   0.05799   0.05571  -0.0816   0.9527   0.0404
  -7.500  -0.2481   0.05367   0.05134  -0.0901   0.9428   0.0413
  -7.250  -0.2287   0.03356   0.03002  -0.1200   0.9167   0.0471
  -7.000  -0.1971   0.03151   0.02796  -0.1224   0.9018   0.0479
  -6.750  -0.1719   0.02991   0.02622  -0.1235   0.8841   0.0490
  -6.500  -0.1510   0.02838   0.02448  -0.1235   0.8665   0.0507
  -6.250  -0.1391   0.02629   0.02167  -0.1225   0.8488   0.0555
  -6.000  -0.1173   0.02455   0.01996  -0.1221   0.8352   0.0566
  -5.750  -0.0953   0.02346   0.01879  -0.1216   0.8225   0.0581
  -5.500  -0.0733   0.02257   0.01770  -0.1208   0.8105   0.0606
  -5.250  -0.0574   0.01836   0.01244  -0.1180   0.7990   0.0473
  -5.000  -0.0336   0.01627   0.00994  -0.1165   0.7888   0.0398
  -4.750  -0.0083   0.01580   0.00930  -0.1158   0.7793   0.0395
  -4.500   0.0170   0.01526   0.00867  -0.1152   0.7699   0.0393
  -4.250   0.0423   0.01467   0.00795  -0.1145   0.7614   0.0392
  -4.000   0.0674   0.01399   0.00720  -0.1139   0.7525   0.0392
  -3.750   0.0922   0.01320   0.00631  -0.1132   0.7449   0.0394
  -3.500   0.1165   0.01239   0.00549  -0.1124   0.7368   0.0399
  -3.250   0.1413   0.01188   0.00493  -0.1117   0.7296   0.0404
  -3.000   0.1664   0.01148   0.00451  -0.1110   0.7222   0.0408
  -2.750   0.1917   0.01115   0.00414  -0.1104   0.7149   0.0413
  -2.500   0.2173   0.01088   0.00383  -0.1098   0.7083   0.0419
  -2.250   0.2430   0.01063   0.00355  -0.1092   0.7011   0.0427
  -1.750   0.2950   0.01025   0.00309  -0.1081   0.6878   0.0444
  -1.500   0.3213   0.01011   0.00289  -0.1076   0.6812   0.0454
  -1.250   0.3473   0.00994   0.00269  -0.1070   0.6741   0.0473
  -1.000   0.3732   0.00978   0.00249  -0.1064   0.6660   0.0501
  -0.750   0.3996   0.00970   0.00235  -0.1059   0.6587   0.0534
  -0.500   0.4257   0.00952   0.00223  -0.1053   0.6516   0.0674
  -0.250   0.4482   0.00880   0.00218  -0.1046   0.6458   0.2860
   0.000   0.4740   0.00865   0.00224  -0.1041   0.6394   0.3611
   0.250   0.5000   0.00858   0.00227  -0.1036   0.6332   0.4046
   0.500   0.5262   0.00857   0.00231  -0.1031   0.6273   0.4407
   0.750   0.5523   0.00851   0.00235  -0.1026   0.6210   0.4714
   1.000   0.5783   0.00848   0.00239  -0.1021   0.6151   0.5055
   1.250   0.6042   0.00847   0.00245  -0.1015   0.6092   0.5410
   1.500   0.6292   0.00837   0.00252  -0.1008   0.6027   0.5925
   1.750   0.6523   0.00820   0.00257  -0.0997   0.5971   0.6723
   2.000   0.7476   0.00766   0.00267  -0.1146   0.5878   1.0000
   2.250   0.7728   0.00778   0.00269  -0.1139   0.5785   1.0000
   2.500   0.7983   0.00784   0.00273  -0.1133   0.5685   1.0000
   2.750   0.8237   0.00796   0.00279  -0.1126   0.5608   1.0000
   3.000   0.8495   0.00804   0.00286  -0.1121   0.5526   1.0000
   3.250   0.8745   0.00817   0.00294  -0.1114   0.5436   1.0000
   3.500   0.8995   0.00828   0.00301  -0.1106   0.5331   1.0000
   3.750   0.9245   0.00839   0.00311  -0.1099   0.5227   1.0000
   4.000   0.9490   0.00855   0.00321  -0.1091   0.5134   1.0000
   4.250   0.9741   0.00866   0.00333  -0.1085   0.5031   1.0000
   4.500   0.9984   0.00881   0.00345  -0.1076   0.4914   1.0000
   4.750   1.0221   0.00898   0.00358  -0.1067   0.4777   1.0000
   5.000   1.0455   0.00917   0.00372  -0.1057   0.4628   1.0000
   5.250   1.0686   0.00937   0.00388  -0.1047   0.4466   1.0000
   5.500   1.0909   0.00961   0.00406  -0.1036   0.4264   1.0000
   5.750   1.1120   0.00992   0.00428  -0.1022   0.4041   1.0000
   6.000   1.1324   0.01027   0.00453  -0.1008   0.3791   1.0000
   6.250   1.1510   0.01072   0.00484  -0.0990   0.3509   1.0000
   6.500   1.1682   0.01125   0.00522  -0.0971   0.3190   1.0000
   6.750   1.1832   0.01191   0.00567  -0.0947   0.2790   1.0000
   7.000   1.1895   0.01306   0.00637  -0.0911   0.2010   1.0000
   7.250   1.1841   0.01485   0.00757  -0.0856   0.1069   1.0000
   7.500   1.1965   0.01559   0.00821  -0.0830   0.0869   1.0000
   7.750   1.2092   0.01619   0.00875  -0.0803   0.0767   1.0000
   8.000   1.2227   0.01669   0.00925  -0.0777   0.0720   1.0000
   8.250   1.2344   0.01729   0.00984  -0.0750   0.0682   1.0000
   8.500   1.2471   0.01788   0.01045  -0.0725   0.0654   1.0000
   8.750   1.2608   0.01844   0.01106  -0.0702   0.0635   1.0000
   9.000   1.2732   0.01909   0.01176  -0.0679   0.0614   1.0000
   9.250   1.2835   0.01989   0.01257  -0.0654   0.0593   1.0000
   9.500   1.2886   0.02101   0.01373  -0.0625   0.0570   1.0000
   9.750   1.3005   0.02181   0.01460  -0.0605   0.0557   1.0000
  10.000   1.3124   0.02265   0.01550  -0.0587   0.0545   1.0000
  10.250   1.3233   0.02360   0.01652  -0.0569   0.0530   1.0000
  10.500   1.3330   0.02467   0.01763  -0.0551   0.0515   1.0000
  10.750   1.3402   0.02599   0.01899  -0.0533   0.0502   1.0000
  11.000   1.3414   0.02783   0.02087  -0.0511   0.0486   1.0000
  11.250   1.3463   0.02947   0.02259  -0.0494   0.0474   1.0000
  11.500   1.3589   0.03056   0.02375  -0.0484   0.0463   1.0000
  11.750   1.3688   0.03188   0.02515  -0.0473   0.0450   1.0000
  12.000   1.3778   0.03332   0.02664  -0.0463   0.0437   1.0000
  12.250   1.3859   0.03487   0.02823  -0.0453   0.0424   1.0000
  12.500   1.3887   0.03692   0.03030  -0.0441   0.0412   1.0000
  12.750   1.3901   0.03912   0.03256  -0.0428   0.0400   1.0000
  13.000   1.4016   0.04046   0.03401  -0.0422   0.0387   1.0000
  13.250   1.4098   0.04214   0.03576  -0.0415   0.0375   1.0000
  13.500   1.4174   0.04389   0.03756  -0.0409   0.0363   1.0000
  13.750   1.4231   0.04585   0.03955  -0.0403   0.0351   1.0000
  14.000   1.4205   0.04857   0.04229  -0.0393   0.0340   1.0000
  14.250   1.4285   0.05044   0.04427  -0.0389   0.0331   1.0000
  14.500   1.4350   0.05245   0.04638  -0.0385   0.0319   1.0000
  14.750   1.4410   0.05456   0.04856  -0.0383   0.0308   1.0000
  15.000   1.4471   0.05674   0.05077  -0.0382   0.0297   1.0000
  15.250   1.4469   0.05955   0.05360  -0.0379   0.0289   1.0000
  15.500   1.4474   0.06229   0.05643  -0.0375   0.0281   1.0000
  15.750   1.4515   0.06476   0.05902  -0.0375   0.0272   1.0000
  16.000   1.4546   0.06737   0.06171  -0.0375   0.0265   1.0000
  16.250   1.4568   0.07016   0.06457  -0.0376   0.0257   1.0000
  16.500   1.4587   0.07302   0.06748  -0.0378   0.0251   1.0000
  16.750   1.4584   0.07611   0.07061  -0.0381   0.0244   1.0000
  17.000   1.4553   0.07943   0.07397  -0.0381   0.0238   1.0000
  17.250   1.4564   0.08252   0.07720  -0.0385   0.0232   1.0000
  17.500   1.4564   0.08571   0.08051  -0.0388   0.0227   1.0000
  17.750   1.4561   0.08904   0.08392  -0.0394   0.0221   1.0000
  18.000   1.4557   0.09236   0.08733  -0.0401   0.0216   1.0000
  18.250   1.4543   0.09585   0.09089  -0.0408   0.0212   1.0000
  18.500   1.4525   0.09939   0.09450  -0.0416   0.0208   1.0000
  18.750   1.4499   0.10304   0.09818  -0.0424   0.0204   1.0000
  19.000   1.4459   0.10667   0.10187  -0.0430   0.0199   1.0000
  19.250   1.4430   0.11052   0.10585  -0.0441   0.0196   1.0000
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