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GOE 532 AIRFOIL (goe532-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: GOE 532 AIRFOIL (goe532-il)
Reynolds number: 200,000
Max Cl/Cd: 76.61 at α=6.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe532-il-200000.txt
Download as CSV file: xf-goe532-il-200000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 532 AIRFOIL                                 
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -10.000  -0.2755   0.10583   0.10210  -0.0341   1.0000   0.0576
  -9.750  -0.2757   0.10296   0.09927  -0.0353   1.0000   0.0596
  -9.500  -0.3078   0.09930   0.09573  -0.0426   1.0000   0.0612
  -9.250  -0.2989   0.09562   0.09208  -0.0409   1.0000   0.0618
  -9.000  -0.2861   0.09333   0.08982  -0.0385   1.0000   0.0624
  -8.750  -0.2787   0.09129   0.08782  -0.0370   1.0000   0.0633
  -8.500  -0.2767   0.08926   0.08585  -0.0359   1.0000   0.0645
  -8.250  -0.2812   0.08731   0.08398  -0.0347   1.0000   0.0657
  -8.000  -0.2945   0.08584   0.08261  -0.0323   1.0000   0.0667
  -7.750  -0.3103   0.08259   0.07944  -0.0372   0.9945   0.0694
  -7.500  -0.2892   0.07492   0.07178  -0.0497   0.9839   0.0717
  -7.250  -0.2611   0.07285   0.06970  -0.0500   0.9780   0.0735
  -7.000  -0.2363   0.05841   0.05491  -0.0811   0.9600   0.0817
  -6.750  -0.2036   0.05678   0.05342  -0.0801   0.9567   0.0829
  -6.500  -0.1754   0.05485   0.05152  -0.0811   0.9474   0.0849
  -6.250  -0.1475   0.04625   0.04244  -0.0954   0.9339   0.0947
  -6.000  -0.1135   0.04441   0.04071  -0.0967   0.9256   0.0971
  -5.750  -0.0872   0.04004   0.03593  -0.1023   0.9098   0.1085
  -5.500  -0.0590   0.03856   0.03454  -0.1024   0.8944   0.1120
  -5.250  -0.0349   0.03566   0.03133  -0.1047   0.8761   0.1238
  -5.000  -0.0099   0.03422   0.02984  -0.1045   0.8573   0.1290
  -4.750   0.0122   0.03225   0.02764  -0.1049   0.8376   0.1409
  -4.500   0.0430   0.02301   0.01612  -0.1050   0.8210   0.0702
  -4.250   0.0679   0.02105   0.01395  -0.1044   0.8015   0.0693
  -4.000   0.0933   0.01964   0.01230  -0.1036   0.7811   0.0681
  -3.750   0.1189   0.01856   0.01097  -0.1027   0.7601   0.0674
  -3.500   0.1448   0.01770   0.00987  -0.1018   0.7396   0.0673
  -3.250   0.1710   0.01700   0.00895  -0.1010   0.7203   0.0675
  -3.000   0.1973   0.01648   0.00824  -0.1002   0.7025   0.0687
  -2.750   0.2238   0.01614   0.00770  -0.0995   0.6859   0.0701
  -2.500   0.2497   0.01549   0.00695  -0.0987   0.6709   0.0712
  -2.250   0.2754   0.01494   0.00635  -0.0980   0.6575   0.0728
  -2.000   0.3013   0.01458   0.00596  -0.0974   0.6440   0.0749
  -1.750   0.3275   0.01431   0.00564  -0.0968   0.6315   0.0777
  -1.500   0.3540   0.01412   0.00534  -0.0962   0.6207   0.0818
  -1.250   0.3801   0.01382   0.00504  -0.0957   0.6100   0.0884
  -1.000   0.4071   0.01362   0.00480  -0.0953   0.6010   0.0987
  -0.750   0.4315   0.01267   0.00466  -0.0950   0.5926   0.3077
  -0.500   0.4543   0.01218   0.00486  -0.0939   0.5853   0.5331
  -0.250   0.4778   0.01200   0.00499  -0.0926   0.5769   0.6334
   0.000   0.5014   0.01191   0.00504  -0.0912   0.5700   0.7218
   0.250   0.5266   0.01152   0.00506  -0.0898   0.5621   0.8501
   0.500   0.5753   0.01153   0.00498  -0.0938   0.5547   1.0000
   0.750   0.6029   0.01173   0.00506  -0.0937   0.5489   1.0000
   1.000   0.6301   0.01189   0.00513  -0.0934   0.5423   1.0000
   1.250   0.6576   0.01208   0.00517  -0.0931   0.5364   1.0000
   1.500   0.6847   0.01227   0.00529  -0.0929   0.5304   1.0000
   1.750   0.7117   0.01243   0.00540  -0.0925   0.5242   1.0000
   2.000   0.7391   0.01263   0.00547  -0.0922   0.5187   1.0000
   2.250   0.7658   0.01282   0.00562  -0.0919   0.5126   1.0000
   2.500   0.7925   0.01297   0.00573  -0.0915   0.5060   1.0000
   2.750   0.8197   0.01317   0.00580  -0.0912   0.4999   1.0000
   3.000   0.8457   0.01331   0.00597  -0.0907   0.4931   1.0000
   3.250   0.8722   0.01347   0.00610  -0.0903   0.4869   1.0000
   3.500   0.8990   0.01368   0.00621  -0.0899   0.4808   1.0000
   3.750   0.9244   0.01379   0.00636  -0.0893   0.4728   1.0000
   4.000   0.9507   0.01395   0.00642  -0.0888   0.4654   1.0000
   4.250   0.9758   0.01407   0.00660  -0.0882   0.4570   1.0000
   4.500   1.0014   0.01422   0.00668  -0.0876   0.4492   1.0000
   4.750   1.0265   0.01437   0.00688  -0.0870   0.4408   1.0000
   5.000   1.0515   0.01451   0.00698  -0.0863   0.4321   1.0000
   5.250   1.0759   0.01464   0.00716  -0.0855   0.4218   1.0000
   5.500   1.1000   0.01480   0.00728  -0.0847   0.4113   1.0000
   5.750   1.1233   0.01493   0.00741  -0.0838   0.3980   1.0000
   6.000   1.1462   0.01508   0.00758  -0.0828   0.3827   1.0000
   6.250   1.1684   0.01528   0.00776  -0.0817   0.3653   1.0000
   6.500   1.1898   0.01553   0.00799  -0.0805   0.3433   1.0000
   6.750   1.2094   0.01591   0.00826  -0.0791   0.3173   1.0000
   7.000   1.2280   0.01641   0.00863  -0.0776   0.2925   1.0000
   7.250   1.2459   0.01700   0.00909  -0.0761   0.2753   1.0000
   7.500   1.2642   0.01759   0.00961  -0.0746   0.2634   1.0000
   7.750   1.2817   0.01823   0.01016  -0.0731   0.2547   1.0000
   8.000   1.3014   0.01876   0.01070  -0.0718   0.2475   1.0000
   8.250   1.3187   0.01941   0.01129  -0.0703   0.2412   1.0000
   8.500   1.3375   0.01996   0.01187  -0.0690   0.2357   1.0000
   8.750   1.3552   0.02053   0.01246  -0.0675   0.2299   1.0000
   9.000   1.3701   0.02128   0.01314  -0.0657   0.2244   1.0000
   9.250   1.3872   0.02177   0.01373  -0.0642   0.2197   1.0000
   9.500   1.4016   0.02238   0.01438  -0.0622   0.2144   1.0000
   9.750   1.4142   0.02318   0.01512  -0.0602   0.2094   1.0000
  10.000   1.4284   0.02378   0.01584  -0.0583   0.2044   1.0000
  10.250   1.4401   0.02449   0.01662  -0.0563   0.1986   1.0000
  10.500   1.4503   0.02547   0.01753  -0.0542   0.1929   1.0000
  10.750   1.4610   0.02620   0.01843  -0.0523   0.1871   1.0000
  11.000   1.4686   0.02724   0.01947  -0.0502   0.1808   1.0000
  11.250   1.4761   0.02833   0.02066  -0.0482   0.1741   1.0000
  11.500   1.4817   0.02955   0.02195  -0.0463   0.1669   1.0000
  11.750   1.4861   0.03098   0.02343  -0.0445   0.1597   1.0000
  12.000   1.4895   0.03251   0.02504  -0.0430   0.1519   1.0000
  12.250   1.4929   0.03420   0.02681  -0.0416   0.1444   1.0000
  12.500   1.4959   0.03602   0.02868  -0.0404   0.1375   1.0000
  12.750   1.4996   0.03792   0.03065  -0.0394   0.1312   1.0000
  13.000   1.5028   0.03993   0.03272  -0.0387   0.1259   1.0000
  13.250   1.5044   0.04218   0.03499  -0.0380   0.1220   1.0000
  13.500   1.5089   0.04427   0.03718  -0.0375   0.1178   1.0000
  13.750   1.5104   0.04669   0.03964  -0.0371   0.1145   1.0000
  14.000   1.5102   0.04933   0.04227  -0.0368   0.1119   1.0000
  14.250   1.5138   0.05166   0.04470  -0.0365   0.1093   1.0000
  14.500   1.5166   0.05410   0.04723  -0.0363   0.1069   1.0000
  14.750   1.5189   0.05664   0.04981  -0.0362   0.1048   1.0000
  15.000   1.5214   0.05916   0.05235  -0.0361   0.1029   1.0000
  15.250   1.5270   0.06124   0.05437  -0.0357   0.1009   1.0000
  15.500   1.5308   0.06374   0.05701  -0.0356   0.0993   1.0000
  15.750   1.5352   0.06617   0.05955  -0.0356   0.0976   1.0000
  16.000   1.5397   0.06861   0.06206  -0.0356   0.0959   1.0000
  16.250   1.5442   0.07103   0.06453  -0.0357   0.0940   1.0000
  16.500   1.5598   0.07188   0.06523  -0.0347   0.0911   1.0000
  16.750   1.5601   0.07497   0.06847  -0.0351   0.0895   1.0000
  17.000   1.5574   0.07853   0.07221  -0.0359   0.0878   1.0000
  17.250   1.5578   0.08169   0.07549  -0.0366   0.0860   1.0000
  17.500   1.5622   0.08424   0.07808  -0.0369   0.0841   1.0000
  17.750   1.5780   0.08519   0.07897  -0.0361   0.0818   1.0000
  18.000   1.5822   0.08797   0.08186  -0.0362   0.0800   1.0000
  18.250   1.5719   0.09274   0.08686  -0.0381   0.0790   1.0000
  18.500   1.5629   0.09746   0.09179  -0.0399   0.0778   1.0000
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