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GOE 534 AIRFOIL (goe534-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 534 AIRFOIL (goe534-il)
Reynolds number: 1,000,000
Max Cl/Cd: 110.2 at α=7.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe534-il-1000000-n5.txt
Download as CSV file: xf-goe534-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 534 AIRFOIL                                 
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -15.750  -0.7596   0.08875   0.08600  -0.0480   1.0000   0.0235
 -15.500  -0.7758   0.08259   0.07977  -0.0519   1.0000   0.0237
 -15.250  -0.7933   0.07640   0.07351  -0.0559   1.0000   0.0238
 -15.000  -0.8150   0.06977   0.06679  -0.0603   1.0000   0.0239
 -14.750  -0.8418   0.06280   0.05974  -0.0650   1.0000   0.0240
 -14.500  -0.8804   0.05493   0.05177  -0.0706   1.0000   0.0239
 -14.250  -0.9428   0.04611   0.04284  -0.0755   1.0000   0.0239
 -14.000  -0.9988   0.03505   0.03157  -0.0854   1.0000   0.0238
 -13.750  -1.0011   0.02895   0.02527  -0.0915   1.0000   0.0239
 -13.500  -0.9795   0.02503   0.02116  -0.0969   0.9992   0.0241
 -13.250  -0.9484   0.02326   0.01927  -0.1000   0.9971   0.0243
 -13.000  -0.9161   0.02194   0.01786  -0.1025   0.9938   0.0244
 -12.750  -0.8866   0.02063   0.01646  -0.1044   0.9889   0.0247
 -12.500  -0.8562   0.01937   0.01513  -0.1062   0.9830   0.0250
 -12.250  -0.8268   0.01843   0.01412  -0.1073   0.9760   0.0253
 -11.750  -0.7528   0.01679   0.01235  -0.1119   0.9565   0.0259
 -11.500  -0.7059   0.01603   0.01149  -0.1160   0.9298   0.0262
 -11.250  -0.6743   0.01557   0.01080  -0.1167   0.8757   0.0265
 -11.000  -0.6513   0.01523   0.01026  -0.1157   0.8369   0.0268
 -10.750  -0.6275   0.01488   0.00976  -0.1148   0.8109   0.0271
 -10.500  -0.6027   0.01454   0.00930  -0.1141   0.7927   0.0274
 -10.250  -0.5776   0.01420   0.00885  -0.1134   0.7776   0.0276
 -10.000  -0.5520   0.01388   0.00843  -0.1128   0.7641   0.0278
  -9.750  -0.5260   0.01354   0.00802  -0.1122   0.7537   0.0280
  -9.500  -0.5005   0.01311   0.00750  -0.1116   0.7434   0.0284
  -9.250  -0.4744   0.01273   0.00706  -0.1110   0.7341   0.0288
  -9.000  -0.4480   0.01241   0.00667  -0.1105   0.7244   0.0292
  -8.750  -0.4214   0.01210   0.00630  -0.1099   0.7165   0.0296
  -8.500  -0.3944   0.01182   0.00596  -0.1094   0.7082   0.0300
  -8.250  -0.3676   0.01158   0.00566  -0.1089   0.6986   0.0304
  -8.000  -0.3402   0.01134   0.00536  -0.1084   0.6902   0.0309
  -7.750  -0.3129   0.01113   0.00509  -0.1079   0.6808   0.0314
  -7.500  -0.2855   0.01091   0.00482  -0.1074   0.6717   0.0320
  -7.250  -0.2584   0.01067   0.00452  -0.1069   0.6597   0.0329
  -7.000  -0.2310   0.01046   0.00426  -0.1064   0.6472   0.0337
  -6.750  -0.2037   0.01029   0.00402  -0.1059   0.6339   0.0347
  -6.500  -0.1764   0.01014   0.00380  -0.1053   0.6168   0.0359
  -6.250  -0.1495   0.00997   0.00355  -0.1047   0.5955   0.0385
  -5.750  -0.0956   0.00971   0.00326  -0.1037   0.5546   0.0586
  -5.500  -0.0679   0.00971   0.00320  -0.1032   0.5379   0.0626
  -5.000  -0.0119   0.00969   0.00305  -0.1022   0.5117   0.0666
  -4.750   0.0160   0.00967   0.00300  -0.1018   0.5007   0.0686
  -4.500   0.0442   0.00964   0.00294  -0.1014   0.4907   0.0700
  -4.250   0.0722   0.00963   0.00287  -0.1010   0.4810   0.0712
  -4.000   0.1003   0.00962   0.00280  -0.1005   0.4695   0.0721
  -3.750   0.1284   0.00963   0.00275  -0.1001   0.4581   0.0729
  -3.500   0.1564   0.00961   0.00267  -0.0997   0.4481   0.0736
  -3.250   0.1843   0.00954   0.00257  -0.0993   0.4407   0.0746
  -3.000   0.2125   0.00948   0.00249  -0.0989   0.4330   0.0755
  -2.750   0.2404   0.00947   0.00244  -0.0985   0.4250   0.0765
  -2.500   0.2687   0.00944   0.00239  -0.0981   0.4193   0.0777
  -2.250   0.2969   0.00942   0.00234  -0.0977   0.4124   0.0787
  -2.000   0.3248   0.00943   0.00230  -0.0973   0.4045   0.0794
  -1.750   0.3531   0.00941   0.00226  -0.0970   0.3981   0.0801
  -1.500   0.3811   0.00941   0.00223  -0.0966   0.3907   0.0808
  -1.250   0.4091   0.00942   0.00221  -0.0962   0.3845   0.0818
  -1.000   0.4372   0.00938   0.00216  -0.0958   0.3786   0.0834
  -0.750   0.4651   0.00939   0.00214  -0.0954   0.3712   0.0845
  -0.500   0.4929   0.00940   0.00213  -0.0950   0.3642   0.0854
  -0.250   0.5208   0.00942   0.00212  -0.0946   0.3561   0.0865
   0.000   0.5484   0.00946   0.00213  -0.0942   0.3487   0.0876
   0.250   0.5764   0.00948   0.00214  -0.0938   0.3423   0.0889
   0.500   0.6040   0.00954   0.00216  -0.0934   0.3342   0.0901
   0.750   0.6316   0.00958   0.00218  -0.0930   0.3264   0.0931
   1.000   0.6588   0.00965   0.00222  -0.0925   0.3168   0.0972
   1.250   0.6862   0.00967   0.00226  -0.0921   0.3095   0.1074
   1.500   0.7129   0.00960   0.00230  -0.0916   0.3013   0.1591
   1.750   0.7396   0.00958   0.00237  -0.0912   0.2934   0.2037
   2.000   0.7664   0.00963   0.00246  -0.0907   0.2839   0.2323
   2.250   0.7931   0.00970   0.00256  -0.0902   0.2758   0.2563
   2.500   0.8198   0.00977   0.00267  -0.0897   0.2678   0.2818
   2.750   0.8464   0.00989   0.00278  -0.0892   0.2601   0.2994
   3.250   0.8993   0.01014   0.00303  -0.0881   0.2449   0.3304
   3.500   0.9259   0.01025   0.00316  -0.0877   0.2387   0.3459
   3.750   0.9519   0.01041   0.00331  -0.0871   0.2314   0.3617
   4.000   0.9784   0.01054   0.00345  -0.0866   0.2263   0.3749
   4.250   1.0048   0.01065   0.00359  -0.0860   0.2217   0.3892
   4.500   1.0307   0.01081   0.00375  -0.0855   0.2166   0.4038
   4.750   1.0566   0.01097   0.00392  -0.0849   0.2119   0.4164
   5.000   1.0828   0.01109   0.00407  -0.0844   0.2084   0.4305
   5.250   1.1086   0.01124   0.00423  -0.0838   0.2048   0.4426
   5.500   1.1341   0.01141   0.00441  -0.0832   0.2008   0.4571
   5.750   1.1592   0.01159   0.00461  -0.0825   0.1966   0.4733
   6.000   1.1849   0.01171   0.00478  -0.0819   0.1938   0.4900
   6.250   1.2102   0.01186   0.00496  -0.0813   0.1906   0.5050
   6.500   1.2349   0.01204   0.00516  -0.0806   0.1870   0.5198
   6.750   1.2590   0.01224   0.00539  -0.0798   0.1827   0.5386
   7.250   1.3068   0.01242   0.00582  -0.0782   0.1770   0.6488
   7.750   1.3753   0.01248   0.00643  -0.0811   0.1671   1.0000
   8.000   1.3992   0.01271   0.00665  -0.0803   0.1633   1.0000
   8.250   1.4219   0.01301   0.00691  -0.0794   0.1581   1.0000
   8.500   1.4441   0.01332   0.00720  -0.0784   0.1538   1.0000
   8.750   1.4671   0.01357   0.00745  -0.0775   0.1507   1.0000
   9.000   1.4891   0.01386   0.00773  -0.0764   0.1470   1.0000
   9.250   1.5099   0.01421   0.00805  -0.0752   0.1429   1.0000
   9.500   1.5310   0.01452   0.00836  -0.0741   0.1393   1.0000
   9.750   1.5515   0.01484   0.00868  -0.0728   0.1359   1.0000
  10.000   1.5704   0.01523   0.00905  -0.0714   0.1317   1.0000
  10.250   1.5880   0.01560   0.00942  -0.0696   0.1285   1.0000
  10.500   1.6048   0.01593   0.00977  -0.0678   0.1259   1.0000
  10.750   1.6202   0.01632   0.01016  -0.0657   0.1229   1.0000
  11.000   1.6346   0.01678   0.01061  -0.0636   0.1197   1.0000
  11.250   1.6494   0.01724   0.01109  -0.0617   0.1170   1.0000
  11.500   1.6646   0.01770   0.01157  -0.0599   0.1145   1.0000
  11.750   1.6788   0.01823   0.01211  -0.0580   0.1119   1.0000
  12.000   1.6916   0.01886   0.01274  -0.0561   0.1091   1.0000
  12.250   1.7040   0.01954   0.01344  -0.0543   0.1063   1.0000
  12.500   1.7178   0.02019   0.01412  -0.0527   0.1044   1.0000
  12.750   1.7301   0.02095   0.01491  -0.0512   0.1021   1.0000
  13.000   1.7412   0.02184   0.01583  -0.0497   0.0999   1.0000
  13.250   1.7509   0.02290   0.01691  -0.0482   0.0975   1.0000
  13.500   1.7623   0.02390   0.01796  -0.0470   0.0958   1.0000
  13.750   1.7734   0.02499   0.01909  -0.0460   0.0942   1.0000
  14.000   1.7821   0.02633   0.02046  -0.0450   0.0916   1.0000
  14.250   1.7891   0.02788   0.02204  -0.0441   0.0893   1.0000
  14.500   1.7952   0.02956   0.02376  -0.0433   0.0868   1.0000
  14.750   1.8024   0.03121   0.02546  -0.0426   0.0848   1.0000
  15.000   1.8066   0.03318   0.02747  -0.0420   0.0823   1.0000
  15.250   1.8072   0.03553   0.02985  -0.0415   0.0796   1.0000
  15.500   1.8099   0.03774   0.03212  -0.0411   0.0780   1.0000
  15.750   1.8116   0.04009   0.03454  -0.0407   0.0763   1.0000
  16.000   1.8115   0.04267   0.03718  -0.0405   0.0749   1.0000
  16.250   1.8085   0.04563   0.04020  -0.0404   0.0734   1.0000
  16.500   1.8035   0.04893   0.04357  -0.0405   0.0720   1.0000
  16.750   1.7977   0.05241   0.04712  -0.0408   0.0705   1.0000
  17.000   1.7932   0.05582   0.05061  -0.0411   0.0695   1.0000
  17.250   1.7867   0.05953   0.05440  -0.0416   0.0683   1.0000
  17.500   1.7771   0.06365   0.05860  -0.0422   0.0669   1.0000
  17.750   1.7651   0.06812   0.06315  -0.0430   0.0656   1.0000
  18.000   1.7523   0.07276   0.06787  -0.0439   0.0646   1.0000
  18.250   1.7388   0.07750   0.07270  -0.0448   0.0638   1.0000
  18.500   1.7272   0.08207   0.07736  -0.0458   0.0628   1.0000
  18.750   1.7156   0.08672   0.08210  -0.0470   0.0622   1.0000
  19.000   1.7022   0.09161   0.08708  -0.0482   0.0610   1.0000
  19.250   1.6892   0.09658   0.09212  -0.0496   0.0602   1.0000
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