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GOE 533 AIRFOIL (goe533-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: GOE 533 AIRFOIL (goe533-il)
Reynolds number: 500,000
Max Cl/Cd: 106.25 at α=7°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe533-il-500000.txt
Download as CSV file: xf-goe533-il-500000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.250  -0.2972   0.12664   0.12418  -0.0334   1.0000   0.0284
 -12.000  -0.2927   0.12353   0.12108  -0.0344   1.0000   0.0294
 -11.750  -0.3150   0.11568   0.11325  -0.0415   1.0000   0.0309
 -11.500  -0.3058   0.11308   0.11067  -0.0404   1.0000   0.0312
 -11.250  -0.2971   0.11090   0.10851  -0.0400   1.0000   0.0314
 -11.000  -0.2893   0.10866   0.10628  -0.0398   1.0000   0.0317
 -10.750  -0.2825   0.10638   0.10402  -0.0398   1.0000   0.0321
 -10.500  -0.2782   0.10379   0.10147  -0.0400   1.0000   0.0325
 -10.250  -0.2186   0.08679   0.08469  -0.0509   0.9956   0.0361
 -10.000  -0.1991   0.08391   0.08181  -0.0521   0.9878   0.0365
  -9.750  -0.1797   0.08082   0.07871  -0.0544   0.9792   0.0369
  -9.500  -0.1592   0.07689   0.07477  -0.0584   0.9694   0.0377
  -9.250  -0.2810   0.08334   0.08115  -0.0507   0.9953   0.0367
  -9.000  -0.2602   0.08049   0.07831  -0.0539   0.9857   0.0372
  -8.750  -0.2415   0.07675   0.07456  -0.0586   0.9731   0.0380
  -8.500  -0.2735   0.04832   0.04567  -0.1035   0.9361   0.0421
  -8.250  -0.2409   0.04601   0.04334  -0.1066   0.9103   0.0425
  -8.000  -0.2212   0.04397   0.04114  -0.1083   0.8703   0.0429
  -7.750  -0.2092   0.04234   0.03928  -0.1082   0.8262   0.0434
  -7.500  -0.1998   0.04031   0.03698  -0.1080   0.7895   0.0442
  -7.250  -0.2084   0.03422   0.02993  -0.1094   0.7628   0.0489
  -7.000  -0.1883   0.03248   0.02817  -0.1091   0.7427   0.0495
  -6.750  -0.1681   0.03112   0.02670  -0.1088   0.7264   0.0501
  -6.500  -0.1474   0.02982   0.02525  -0.1086   0.7136   0.0511
  -6.250  -0.1356   0.02281   0.01686  -0.1077   0.7042   0.0419
  -6.000  -0.1122   0.02058   0.01453  -0.1074   0.6949   0.0408
  -5.750  -0.0880   0.01898   0.01269  -0.1071   0.6860   0.0404
  -5.500  -0.0627   0.01772   0.01120  -0.1067   0.6781   0.0400
  -5.250  -0.0368   0.01670   0.01001  -0.1064   0.6705   0.0400
  -5.000  -0.0105   0.01590   0.00903  -0.1060   0.6635   0.0401
  -4.750   0.0163   0.01518   0.00821  -0.1057   0.6568   0.0403
  -4.500   0.0432   0.01467   0.00756  -0.1054   0.6503   0.0408
  -4.250   0.0705   0.01432   0.00710  -0.1051   0.6444   0.0413
  -4.000   0.0980   0.01396   0.00667  -0.1049   0.6383   0.0417
  -3.750   0.1241   0.01312   0.00578  -0.1045   0.6326   0.0422
  -3.500   0.1506   0.01258   0.00523  -0.1042   0.6271   0.0428
  -3.250   0.1777   0.01218   0.00483  -0.1040   0.6214   0.0436
  -3.000   0.2049   0.01189   0.00451  -0.1038   0.6159   0.0445
  -2.750   0.2322   0.01166   0.00423  -0.1036   0.6108   0.0455
  -2.500   0.2599   0.01141   0.00398  -0.1034   0.6052   0.0467
  -2.250   0.2876   0.01124   0.00377  -0.1032   0.5994   0.0480
  -2.000   0.3148   0.01098   0.00345  -0.1030   0.5939   0.0497
  -1.750   0.3426   0.01073   0.00322  -0.1029   0.5883   0.0519
  -1.500   0.3705   0.01058   0.00305  -0.1027   0.5826   0.0545
  -1.250   0.3982   0.01047   0.00287  -0.1026   0.5770   0.0588
  -1.000   0.4262   0.01025   0.00274  -0.1025   0.5711   0.0728
  -0.750   0.4521   0.00939   0.00260  -0.1026   0.5649   0.2901
  -0.500   0.4779   0.00897   0.00265  -0.1024   0.5588   0.4768
  -0.250   0.5055   0.00886   0.00267  -0.1022   0.5520   0.5207
   0.000   0.5326   0.00881   0.00268  -0.1019   0.5450   0.5568
   0.250   0.5598   0.00877   0.00273  -0.1016   0.5375   0.5969
   0.500   0.5868   0.00878   0.00277  -0.1012   0.5289   0.6297
   0.750   0.6139   0.00880   0.00283  -0.1008   0.5207   0.6585
   1.000   0.6406   0.00884   0.00289  -0.1004   0.5124   0.6902
   1.250   0.6673   0.00887   0.00295  -0.1000   0.5044   0.7171
   1.500   0.6940   0.00890   0.00298  -0.0996   0.4957   0.7340
   1.750   0.7209   0.00893   0.00302  -0.0993   0.4876   0.7493
   2.000   0.7473   0.00897   0.00306  -0.0988   0.4792   0.7668
   2.250   0.7734   0.00898   0.00312  -0.0984   0.4710   0.7881
   2.500   0.7982   0.00899   0.00318  -0.0976   0.4620   0.8186
   2.750   0.8239   0.00879   0.00324  -0.0968   0.4534   0.9158
   3.000   0.8603   0.00895   0.00331  -0.0987   0.4443   1.0000
   3.250   0.8879   0.00908   0.00341  -0.0986   0.4364   1.0000
   3.500   0.9143   0.00928   0.00352  -0.0984   0.4287   1.0000
   3.750   0.9415   0.00942   0.00365  -0.0983   0.4219   1.0000
   4.000   0.9680   0.00961   0.00378  -0.0980   0.4151   1.0000
   4.250   0.9944   0.00980   0.00393  -0.0977   0.4086   1.0000
   4.500   1.0210   0.00996   0.00407  -0.0975   0.4018   1.0000
   4.750   1.0467   0.01020   0.00424  -0.0971   0.3955   1.0000
   5.000   1.0734   0.01034   0.00440  -0.0969   0.3896   1.0000
   5.250   1.0993   0.01054   0.00458  -0.0966   0.3834   1.0000
   5.500   1.1246   0.01078   0.00477  -0.0962   0.3780   1.0000
   5.750   1.1510   0.01093   0.00495  -0.0959   0.3722   1.0000
   6.000   1.1760   0.01116   0.00515  -0.0955   0.3655   1.0000
   6.250   1.2014   0.01136   0.00535  -0.0951   0.3591   1.0000
   6.500   1.2267   0.01156   0.00555  -0.0947   0.3528   1.0000
   7.000   1.2761   0.01201   0.00600  -0.0937   0.3404   1.0000
   7.250   1.3001   0.01226   0.00624  -0.0931   0.3337   1.0000
   7.500   1.3242   0.01250   0.00650  -0.0925   0.3279   1.0000
   7.750   1.3484   0.01272   0.00674  -0.0920   0.3214   1.0000
   8.000   1.3706   0.01304   0.00703  -0.0911   0.3145   1.0000
   8.250   1.3947   0.01324   0.00729  -0.0906   0.3070   1.0000
   8.500   1.4158   0.01359   0.00760  -0.0895   0.2985   1.0000
   8.750   1.4384   0.01385   0.00789  -0.0888   0.2891   1.0000
   9.000   1.4591   0.01419   0.00823  -0.0877   0.2801   1.0000
   9.250   1.4786   0.01457   0.00860  -0.0864   0.2697   1.0000
   9.500   1.4980   0.01494   0.00897  -0.0852   0.2582   1.0000
   9.750   1.5140   0.01539   0.00940  -0.0834   0.2452   1.0000
  10.000   1.5266   0.01593   0.00989  -0.0810   0.2309   1.0000
  10.250   1.5374   0.01655   0.01046  -0.0784   0.2170   1.0000
  10.500   1.5470   0.01725   0.01111  -0.0758   0.2049   1.0000
  10.750   1.5551   0.01805   0.01186  -0.0731   0.1943   1.0000
  11.000   1.5646   0.01882   0.01263  -0.0708   0.1860   1.0000
  11.250   1.5731   0.01968   0.01349  -0.0684   0.1792   1.0000
  11.500   1.5820   0.02055   0.01439  -0.0663   0.1727   1.0000
  11.750   1.5879   0.02165   0.01549  -0.0640   0.1660   1.0000
  12.000   1.5963   0.02268   0.01655  -0.0621   0.1586   1.0000
  12.250   1.6009   0.02401   0.01790  -0.0601   0.1518   1.0000
  12.500   1.6082   0.02525   0.01918  -0.0585   0.1428   1.0000
  12.750   1.6112   0.02690   0.02081  -0.0568   0.1291   1.0000
  13.000   1.6043   0.02946   0.02325  -0.0549   0.1029   1.0000
  13.250   1.5900   0.03290   0.02658  -0.0532   0.0860   1.0000
  13.500   1.5822   0.03602   0.02970  -0.0521   0.0789   1.0000
  13.750   1.5765   0.03910   0.03283  -0.0514   0.0748   1.0000
  14.000   1.5700   0.04236   0.03615  -0.0509   0.0715   1.0000
  14.250   1.5692   0.04511   0.03900  -0.0505   0.0693   1.0000
  14.500   1.5652   0.04827   0.04223  -0.0503   0.0671   1.0000
  14.750   1.5584   0.05184   0.04587  -0.0502   0.0650   1.0000
  15.000   1.5495   0.05577   0.04987  -0.0504   0.0630   1.0000
  15.250   1.5460   0.05918   0.05338  -0.0506   0.0614   1.0000
  15.500   1.5448   0.06239   0.05669  -0.0509   0.0597   1.0000
  15.750   1.5407   0.06607   0.06046  -0.0514   0.0578   1.0000
  16.000   1.5343   0.07015   0.06461  -0.0521   0.0563   1.0000
  16.250   1.5241   0.07487   0.06940  -0.0531   0.0544   1.0000
  16.500   1.5201   0.07886   0.07348  -0.0541   0.0528   1.0000
  16.750   1.5202   0.08227   0.07700  -0.0549   0.0508   1.0000
  17.000   1.5159   0.08642   0.08122  -0.0560   0.0489   1.0000
  17.250   1.5074   0.09126   0.08612  -0.0575   0.0470   1.0000
  17.500   1.5022   0.09569   0.09064  -0.0589   0.0451   1.0000
  17.750   1.5004   0.09962   0.09466  -0.0602   0.0425   1.0000
  18.000   1.4925   0.10458   0.09966  -0.0619   0.0403   1.0000
  18.250   1.4879   0.10905   0.10422  -0.0636   0.0378   1.0000
  18.500   1.4822   0.11378   0.10901  -0.0654   0.0351   1.0000
  18.750   1.4729   0.11915   0.11442  -0.0676   0.0332   1.0000
  19.000   1.4691   0.12359   0.11893  -0.0695   0.0308   1.0000
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