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GOE 324 (HANSA-BRANDENBURG) AIRFOIL (goe324-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: GOE 324 (HANSA-BRANDENBURG) AIRFOIL (goe324-il)
Reynolds number: 200,000
Max Cl/Cd: 70.62 at α=8.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe324-il-200000.txt
Download as CSV file: xf-goe324-il-200000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 324 (HANSA-BRANDENBURG) 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
  ------ -------- --------- --------- -------- -------- --------
  -8.500  -0.2531   0.10304   0.09882  -0.0093   0.7083   0.0419
  -8.250  -0.2503   0.10011   0.09590  -0.0138   0.7036   0.0427
  -8.000  -0.2535   0.09694   0.09274  -0.0223   0.6995   0.0431
  -7.750  -0.2465   0.09338   0.08915  -0.0236   0.6955   0.0433
  -7.500  -0.2306   0.09008   0.08586  -0.0212   0.6903   0.0436
  -7.250  -0.2197   0.08724   0.08302  -0.0212   0.6847   0.0441
  -7.000  -0.2106   0.08449   0.08024  -0.0225   0.6800   0.0447
  -6.750  -0.1996   0.08154   0.07723  -0.0251   0.6760   0.0457
  -6.500  -0.1861   0.07825   0.07396  -0.0291   0.6708   0.0468
  -6.250  -0.1692   0.07449   0.07015  -0.0358   0.6659   0.0484
  -6.000  -0.1449   0.06910   0.06451  -0.0479   0.6620   0.0495
  -5.750  -0.1322   0.06632   0.06171  -0.0465   0.6579   0.0499
  -5.500  -0.1162   0.06371   0.05914  -0.0467   0.6524   0.0505
  -5.250  -0.0977   0.06103   0.05643  -0.0480   0.6468   0.0515
  -5.000  -0.0769   0.05820   0.05348  -0.0501   0.6422   0.0530
  -4.750  -0.0404   0.05418   0.04885  -0.0579   0.6387   0.0567
  -4.500  -0.0229   0.05110   0.04593  -0.0579   0.6327   0.0573
  -4.250  -0.0033   0.04881   0.04364  -0.0581   0.6274   0.0582
  -4.000   0.0188   0.04672   0.04144  -0.0587   0.6230   0.0600
  -3.750   0.0524   0.04416   0.03833  -0.0615   0.6189   0.0656
  -3.500   0.0733   0.04164   0.03594  -0.0619   0.6127   0.0667
  -3.250   0.0967   0.03977   0.03401  -0.0622   0.6076   0.0685
  -3.000   0.1299   0.03870   0.03230  -0.0631   0.6035   0.0756
  -2.750   0.1519   0.03589   0.02962  -0.0636   0.5982   0.0771
  -2.500   0.1767   0.03428   0.02802  -0.0639   0.5927   0.0798
  -2.250   0.2068   0.03301   0.02631  -0.0643   0.5883   0.0884
  -2.000   0.2311   0.03123   0.02451  -0.0644   0.5846   0.0913
  -1.750   0.2605   0.03034   0.02338  -0.0648   0.5788   0.1024
  -1.500   0.2859   0.02872   0.02182  -0.0650   0.5735   0.1069
  -1.250   0.3136   0.02760   0.02047  -0.0652   0.5694   0.1199
  -1.000   0.3405   0.02666   0.01939  -0.0653   0.5655   0.1361
  -0.750   0.3672   0.02565   0.01841  -0.0657   0.5600   0.1542
   0.250   0.4948   0.02145   0.01287  -0.0638   0.5430   0.0856
   0.500   0.5250   0.02037   0.01158  -0.0634   0.5387   0.0736
   0.750   0.5538   0.01961   0.01071  -0.0632   0.5351   0.0720
   1.000   0.5826   0.01913   0.01008  -0.0629   0.5319   0.0718
   1.250   0.6109   0.01871   0.00972  -0.0629   0.5267   0.0702
   1.500   0.6391   0.01834   0.00934  -0.0627   0.5222   0.0694
   1.750   0.6673   0.01799   0.00896  -0.0624   0.5185   0.0696
   2.000   0.6955   0.01774   0.00863  -0.0622   0.5151   0.0706
   2.250   0.7230   0.01759   0.00861  -0.0622   0.5093   0.0727
   2.500   0.7509   0.01733   0.00834  -0.0621   0.5039   0.0770
   2.750   0.7793   0.01712   0.00803  -0.0619   0.4997   0.0821
   3.000   0.8072   0.01714   0.00806  -0.0619   0.4949   0.0904
   3.250   0.8372   0.01521   0.00822  -0.0622   0.4900   1.0000
   3.500   0.8652   0.01534   0.00815  -0.0620   0.4859   1.0000
   3.750   0.8933   0.01549   0.00811  -0.0619   0.4823   1.0000
   4.000   0.9201   0.01577   0.00840  -0.0619   0.4774   1.0000
   4.250   0.9473   0.01597   0.00857  -0.0618   0.4725   1.0000
   4.500   0.9751   0.01611   0.00863  -0.0617   0.4684   1.0000
   4.750   1.0031   0.01633   0.00870  -0.0617   0.4649   1.0000
   5.000   1.0290   0.01663   0.00910  -0.0616   0.4594   1.0000
   5.250   1.0561   0.01680   0.00926  -0.0616   0.4544   1.0000
   5.500   1.0840   0.01694   0.00929  -0.0615   0.4501   1.0000
   5.750   1.1102   0.01726   0.00963  -0.0614   0.4451   1.0000
   6.000   1.1364   0.01748   0.00990  -0.0614   0.4393   1.0000
   6.250   1.1639   0.01759   0.00993  -0.0613   0.4344   1.0000
   6.500   1.1900   0.01787   0.01022  -0.0612   0.4288   1.0000
   6.750   1.2156   0.01807   0.01047  -0.0610   0.4221   1.0000
   7.000   1.2429   0.01819   0.01049  -0.0609   0.4168   1.0000
   7.250   1.2675   0.01850   0.01089  -0.0607   0.4102   1.0000
   7.500   1.2932   0.01869   0.01110  -0.0605   0.4038   1.0000
   7.750   1.3199   0.01893   0.01124  -0.0604   0.3985   1.0000
   8.000   1.3430   0.01926   0.01172  -0.0601   0.3911   1.0000
   8.250   1.3687   0.01944   0.01187  -0.0599   0.3849   1.0000
   8.500   1.3921   0.01980   0.01230  -0.0596   0.3778   1.0000
   8.750   1.4160   0.02005   0.01258  -0.0593   0.3707   1.0000
   9.000   1.4398   0.02039   0.01293  -0.0590   0.3641   1.0000
   9.250   1.4618   0.02076   0.01338  -0.0585   0.3564   1.0000
   9.500   1.4858   0.02109   0.01364  -0.0582   0.3503   1.0000
   9.750   1.5055   0.02160   0.01431  -0.0576   0.3425   1.0000
  10.000   1.5283   0.02197   0.01463  -0.0571   0.3365   1.0000
  10.250   1.5470   0.02258   0.01537  -0.0564   0.3293   1.0000
  10.500   1.5671   0.02307   0.01587  -0.0558   0.3231   1.0000
  10.750   1.5860   0.02367   0.01652  -0.0551   0.3170   1.0000
  11.000   1.6019   0.02432   0.01725  -0.0541   0.3101   1.0000
  11.250   1.6204   0.02489   0.01777  -0.0533   0.3043   1.0000
  11.500   1.6321   0.02577   0.01880  -0.0520   0.2982   1.0000
  11.750   1.6448   0.02650   0.01956  -0.0507   0.2930   1.0000
  12.000   1.6571   0.02739   0.02047  -0.0494   0.2881   1.0000
  12.250   1.6629   0.02862   0.02183  -0.0481   0.2824   1.0000
  12.500   1.6742   0.02961   0.02279  -0.0471   0.2769   1.0000
  12.750   1.6793   0.03115   0.02445  -0.0462   0.2714   1.0000
  13.000   1.6834   0.03281   0.02620  -0.0455   0.2656   1.0000
  13.250   1.6937   0.03403   0.02736  -0.0448   0.2598   1.0000
  13.500   1.6920   0.03635   0.02986  -0.0443   0.2542   1.0000
  13.750   1.6968   0.03810   0.03163  -0.0438   0.2486   1.0000
  14.000   1.7003   0.04005   0.03364  -0.0433   0.2433   1.0000
  14.250   1.6974   0.04265   0.03639  -0.0430   0.2377   1.0000
  14.500   1.7039   0.04427   0.03795  -0.0424   0.2321   1.0000
  14.750   1.6977   0.04731   0.04116  -0.0422   0.2269   1.0000
  15.000   1.6938   0.05014   0.04409  -0.0421   0.2214   1.0000
  15.250   1.6977   0.05205   0.04596  -0.0416   0.2159   1.0000
  15.500   1.6856   0.05594   0.05006  -0.0418   0.2105   1.0000
  15.750   1.6826   0.05881   0.05294  -0.0419   0.2044   1.0000
  16.000   1.6735   0.06263   0.05689  -0.0423   0.1982   1.0000
  16.250   1.6641   0.06662   0.06096  -0.0429   0.1916   1.0000
  16.500   1.6562   0.07049   0.06490  -0.0435   0.1852   1.0000
  16.750   1.6450   0.07497   0.06949  -0.0444   0.1783   1.0000
  17.000   1.6355   0.07923   0.07381  -0.0452   0.1717   1.0000
  17.250   1.6229   0.08409   0.07875  -0.0463   0.1644   1.0000
  17.500   1.6112   0.08886   0.08359  -0.0475   0.1574   1.0000
  17.750   1.5998   0.09362   0.08837  -0.0487   0.1506   1.0000
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