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GOE 533 AIRFOIL (goe533-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: GOE 533 AIRFOIL (goe533-il)
Reynolds number: 500,000
Max Cl/Cd: 102.33 at α=6.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe533-il-500000-n5.txt
Download as CSV file: xf-goe533-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 533 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
  ------ -------- --------- --------- -------- -------- --------
 -11.750  -0.3239   0.10814   0.10567  -0.0408   1.0000   0.0193
 -11.500  -0.3183   0.10576   0.10330  -0.0414   1.0000   0.0195
 -10.500  -0.4937   0.03833   0.03531  -0.1025   0.9500   0.0230
 -10.250  -0.4673   0.03536   0.03213  -0.1088   0.9295   0.0232
 -10.000  -0.4490   0.03242   0.02888  -0.1125   0.9003   0.0235
  -9.750  -0.4356   0.03027   0.02642  -0.1132   0.8655   0.0237
  -9.500  -0.4221   0.02866   0.02450  -0.1129   0.8305   0.0239
  -9.250  -0.4092   0.02693   0.02242  -0.1122   0.7966   0.0242
  -9.000  -0.3938   0.02538   0.02052  -0.1115   0.7669   0.0245
  -8.750  -0.3763   0.02398   0.01880  -0.1109   0.7423   0.0250
  -8.500  -0.3570   0.02268   0.01718  -0.1104   0.7218   0.0254
  -8.250  -0.3365   0.02138   0.01556  -0.1099   0.7054   0.0258
  -8.000  -0.3145   0.02030   0.01420  -0.1094   0.6913   0.0261
  -7.750  -0.2911   0.01938   0.01303  -0.1090   0.6794   0.0264
  -7.500  -0.2667   0.01864   0.01208  -0.1086   0.6694   0.0266
  -7.250  -0.2427   0.01769   0.01097  -0.1083   0.6604   0.0268
  -7.000  -0.2176   0.01698   0.01015  -0.1080   0.6528   0.0271
  -6.750  -0.1919   0.01642   0.00952  -0.1078   0.6454   0.0274
  -6.250  -0.1394   0.01558   0.00852  -0.1073   0.6328   0.0281
  -6.000  -0.1129   0.01516   0.00803  -0.1071   0.6266   0.0286
  -5.500  -0.0597   0.01431   0.00701  -0.1066   0.6156   0.0293
  -5.250  -0.0328   0.01392   0.00655  -0.1064   0.6099   0.0297
  -5.000  -0.0061   0.01356   0.00611  -0.1061   0.6043   0.0300
  -4.750   0.0210   0.01322   0.00571  -0.1059   0.5993   0.0303
  -4.500   0.0483   0.01290   0.00534  -0.1057   0.5937   0.0307
  -4.250   0.0755   0.01263   0.00501  -0.1055   0.5885   0.0310
  -4.000   0.1025   0.01234   0.00467  -0.1053   0.5839   0.0313
  -3.750   0.1299   0.01198   0.00430  -0.1052   0.5792   0.0319
  -3.500   0.1574   0.01175   0.00406  -0.1050   0.5738   0.0326
  -3.250   0.1848   0.01157   0.00385  -0.1049   0.5686   0.0333
  -3.000   0.2126   0.01139   0.00364  -0.1048   0.5639   0.0340
  -2.750   0.2406   0.01120   0.00344  -0.1047   0.5588   0.0347
  -2.500   0.2683   0.01106   0.00325  -0.1045   0.5531   0.0354
  -2.250   0.2961   0.01094   0.00309  -0.1044   0.5477   0.0361
  -2.000   0.3241   0.01078   0.00292  -0.1043   0.5416   0.0369
  -1.750   0.3518   0.01065   0.00277  -0.1042   0.5355   0.0383
  -1.500   0.3797   0.01057   0.00266  -0.1041   0.5300   0.0397
  -1.250   0.4078   0.01049   0.00257  -0.1040   0.5235   0.0417
  -1.000   0.4355   0.01043   0.00247  -0.1038   0.5166   0.0448
  -0.750   0.4634   0.01035   0.00239  -0.1037   0.5093   0.0498
  -0.500   0.4908   0.01018   0.00233  -0.1036   0.5014   0.0848
  -0.250   0.5184   0.01006   0.00229  -0.1035   0.4934   0.1249
   0.000   0.5449   0.00976   0.00225  -0.1035   0.4832   0.2332
   0.250   0.5710   0.00934   0.00227  -0.1034   0.4724   0.4013
   0.500   0.5978   0.00930   0.00234  -0.1032   0.4624   0.4684
   0.750   0.6248   0.00930   0.00239  -0.1030   0.4535   0.5066
   1.000   0.6515   0.00928   0.00248  -0.1027   0.4456   0.5534
   1.250   0.6778   0.00927   0.00261  -0.1023   0.4371   0.6091
   1.500   0.7045   0.00934   0.00271  -0.1019   0.4295   0.6413
   1.750   0.7316   0.00943   0.00280  -0.1017   0.4218   0.6585
   2.000   0.7583   0.00955   0.00289  -0.1014   0.4152   0.6738
   2.250   0.7855   0.00963   0.00298  -0.1012   0.4086   0.6869
   2.500   0.8121   0.00976   0.00307  -0.1009   0.4014   0.6976
   2.750   0.8389   0.00986   0.00317  -0.1006   0.3941   0.7096
   3.000   0.8651   0.00997   0.00329  -0.1002   0.3864   0.7241
   3.250   0.8913   0.01007   0.00341  -0.0998   0.3799   0.7400
   3.500   0.9174   0.01016   0.00353  -0.0995   0.3731   0.7556
   3.750   0.9429   0.01029   0.00367  -0.0990   0.3669   0.7721
   4.000   0.9686   0.01034   0.00380  -0.0985   0.3622   0.7959
   4.250   0.9912   0.01026   0.00393  -0.0973   0.3571   0.8631
   4.500   1.0267   0.01036   0.00408  -0.0990   0.3507   1.0000
   4.750   1.0531   0.01052   0.00423  -0.0987   0.3454   1.0000
   5.000   1.0792   0.01071   0.00439  -0.0984   0.3396   1.0000
   5.250   1.1046   0.01093   0.00458  -0.0980   0.3341   1.0000
   5.500   1.1306   0.01111   0.00476  -0.0977   0.3294   1.0000
   5.750   1.1559   0.01132   0.00495  -0.0973   0.3220   1.0000
   6.000   1.1804   0.01157   0.00517  -0.0968   0.3144   1.0000
   6.250   1.2055   0.01179   0.00537  -0.0964   0.3071   1.0000
   6.500   1.2296   0.01205   0.00561  -0.0958   0.3010   1.0000
   6.750   1.2545   0.01226   0.00584  -0.0954   0.2949   1.0000
   7.000   1.2777   0.01256   0.00610  -0.0947   0.2858   1.0000
   7.250   1.3012   0.01283   0.00636  -0.0940   0.2764   1.0000
   7.500   1.3237   0.01315   0.00665  -0.0932   0.2675   1.0000
   7.750   1.3462   0.01346   0.00695  -0.0924   0.2578   1.0000
   8.000   1.3676   0.01381   0.00727  -0.0915   0.2470   1.0000
   8.250   1.3874   0.01424   0.00765  -0.0903   0.2333   1.0000
   8.500   1.4043   0.01481   0.00812  -0.0887   0.2144   1.0000
   8.750   1.4195   0.01542   0.00864  -0.0868   0.1983   1.0000
   9.000   1.4341   0.01593   0.00912  -0.0848   0.1885   1.0000
   9.250   1.4477   0.01646   0.00964  -0.0826   0.1813   1.0000
   9.500   1.4624   0.01695   0.01014  -0.0806   0.1760   1.0000
   9.750   1.4757   0.01751   0.01070  -0.0785   0.1711   1.0000
  10.000   1.4892   0.01807   0.01129  -0.0766   0.1671   1.0000
  10.250   1.5038   0.01860   0.01187  -0.0748   0.1636   1.0000
  10.500   1.5162   0.01925   0.01254  -0.0728   0.1592   1.0000
  10.750   1.5254   0.02010   0.01339  -0.0706   0.1540   1.0000
  11.000   1.5383   0.02078   0.01413  -0.0690   0.1487   1.0000
  11.250   1.5466   0.02176   0.01510  -0.0669   0.1410   1.0000
  11.500   1.5563   0.02272   0.01610  -0.0652   0.1335   1.0000
  11.750   1.5616   0.02401   0.01736  -0.0632   0.1198   1.0000
  12.000   1.5504   0.02657   0.01972  -0.0603   0.0893   1.0000
  12.250   1.5438   0.02907   0.02217  -0.0583   0.0773   1.0000
  12.500   1.5431   0.03129   0.02442  -0.0569   0.0718   1.0000
  12.750   1.5461   0.03331   0.02651  -0.0560   0.0686   1.0000
  13.000   1.5475   0.03557   0.02883  -0.0551   0.0654   1.0000
  13.250   1.5462   0.03820   0.03151  -0.0544   0.0623   1.0000
  13.500   1.5482   0.04056   0.03394  -0.0539   0.0603   1.0000
  13.750   1.5504   0.04297   0.03643  -0.0536   0.0585   1.0000
  14.000   1.5502   0.04567   0.03920  -0.0532   0.0565   1.0000
  14.250   1.5488   0.04856   0.04216  -0.0530   0.0548   1.0000
  14.500   1.5455   0.05175   0.04541  -0.0529   0.0531   1.0000
  14.750   1.5451   0.05469   0.04845  -0.0530   0.0519   1.0000
  15.000   1.5455   0.05759   0.05144  -0.0531   0.0507   1.0000
  15.250   1.5448   0.06071   0.05465  -0.0533   0.0493   1.0000
  15.500   1.5426   0.06410   0.05811  -0.0537   0.0478   1.0000
  15.750   1.5390   0.06775   0.06184  -0.0543   0.0464   1.0000
  16.000   1.5333   0.07180   0.06595  -0.0550   0.0449   1.0000
  16.250   1.5327   0.07522   0.06947  -0.0557   0.0436   1.0000
  16.500   1.5309   0.07888   0.07322  -0.0565   0.0420   1.0000
  16.750   1.5271   0.08288   0.07730  -0.0575   0.0402   1.0000
  17.000   1.5219   0.08716   0.08165  -0.0586   0.0387   1.0000
  17.250   1.5189   0.09118   0.08575  -0.0598   0.0370   1.0000
  17.500   1.5150   0.09537   0.09003  -0.0611   0.0348   1.0000
  17.750   1.5085   0.10003   0.09474  -0.0626   0.0328   1.0000
  18.000   1.5037   0.10445   0.09925  -0.0641   0.0302   1.0000
  18.250   1.4972   0.10923   0.10407  -0.0659   0.0274   1.0000
  18.500   1.4905   0.11407   0.10897  -0.0678   0.0248   1.0000
  18.750   1.4822   0.11924   0.11420  -0.0699   0.0224   1.0000
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