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GOE 323 (HANSA-BRANDENBURG V.1) AIRFOIL (goe323-il) Xfoil prediction polar at RE=100,000 Ncrit=9


Details Polar file
Airfoil: GOE 323 (HANSA-BRANDENBURG V.1) AIRFOIL (goe323-il)
Reynolds number: 100,000
Max Cl/Cd: 48.91 at α=8.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe323-il-100000.txt
Download as CSV file: xf-goe323-il-100000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 323 (HANSA-BRANDENBURG V.1) AIRFOIL         
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.100 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
  -8.750  -0.1898   0.09661   0.09231  -0.0256   0.8302   0.0796
  -8.500  -0.1909   0.09424   0.08990  -0.0276   0.8237   0.0819
  -8.250  -0.2006   0.09275   0.08845  -0.0331   0.8170   0.0832
  -8.000  -0.2113   0.09087   0.08658  -0.0396   0.8105   0.0836
  -7.750  -0.1841   0.08440   0.08006  -0.0331   0.8049   0.0853
  -7.500  -0.1692   0.08091   0.07656  -0.0321   0.7980   0.0878
  -7.250  -0.1624   0.07801   0.07364  -0.0328   0.7923   0.0908
  -7.000  -0.1592   0.07515   0.07077  -0.0353   0.7871   0.0942
  -6.750  -0.1658   0.07270   0.06829  -0.0469   0.7817   0.0972
  -6.500  -0.1586   0.06798   0.06354  -0.0497   0.7771   0.0985
  -6.250  -0.1453   0.06448   0.06005  -0.0453   0.7731   0.1004
  -6.000  -0.1315   0.06141   0.05701  -0.0453   0.7681   0.1034
  -5.750  -0.1194   0.05820   0.05376  -0.0481   0.7630   0.1077
  -5.500  -0.1061   0.05415   0.04943  -0.0582   0.7585   0.1139
  -5.250  -0.0942   0.05068   0.04604  -0.0555   0.7547   0.1159
  -5.000  -0.0782   0.04795   0.04336  -0.0557   0.7501   0.1199
  -4.750  -0.0571   0.04463   0.03975  -0.0623   0.7454   0.1305
  -4.500  -0.0443   0.04169   0.03691  -0.0602   0.7415   0.1340
  -4.250  -0.0223   0.03925   0.03419  -0.0639   0.7371   0.1473
  -4.000  -0.0069   0.03652   0.03160  -0.0631   0.7326   0.1515
  -3.750   0.0148   0.03417   0.02907  -0.0654   0.7280   0.1652
  -3.500   0.0320   0.03202   0.02693  -0.0645   0.7241   0.1736
  -3.250   0.0518   0.02989   0.02472  -0.0654   0.7197   0.1868
  -3.000   0.0722   0.02809   0.02287  -0.0663   0.7144   0.2032
  -2.750   0.0918   0.02634   0.02106  -0.0663   0.7095   0.2224
  -2.500   0.1103   0.02450   0.01910  -0.0657   0.7055   0.2504
  -2.250   0.1274   0.02324   0.01793  -0.0656   0.6984   0.2843
  -2.000   0.1428   0.02171   0.01646  -0.0638   0.6928   0.3240
  -1.750   0.1573   0.02005   0.01483  -0.0614   0.6884   0.3717
  -1.500   0.1741   0.01904   0.01393  -0.0606   0.6811   0.4098
  -1.250   0.1940   0.01758   0.01243  -0.0593   0.6758   0.4427
  -1.000   0.3055   0.03182   0.02354  -0.0729   0.6793   0.1318
  -0.750   0.3335   0.03062   0.02210  -0.0720   0.6746   0.1218
  -0.500   0.3619   0.02994   0.02110  -0.0718   0.6684   0.1165
  -0.250   0.3900   0.02974   0.02063  -0.0713   0.6617   0.1126
   0.000   0.4171   0.02877   0.01951  -0.0703   0.6572   0.1109
   0.250   0.4434   0.02851   0.01924  -0.0704   0.6494   0.1101
   0.500   0.4702   0.02802   0.01866  -0.0696   0.6432   0.1104
   0.750   0.4970   0.02766   0.01817  -0.0685   0.6384   0.1136
   1.000   0.5212   0.02747   0.01817  -0.0685   0.6291   0.1179
   1.250   0.5473   0.02694   0.01762  -0.0670   0.6241   0.1222
   1.500   0.5714   0.02716   0.01787  -0.0667   0.6149   0.1279
   1.750   0.5977   0.02675   0.01744  -0.0656   0.6087   0.1417
   2.000   0.6233   0.02676   0.01754  -0.0651   0.6007   0.1678
   2.250   0.6584   0.02462   0.01717  -0.0654   0.5930   1.0000
   2.500   0.6849   0.02464   0.01691  -0.0642   0.5869   1.0000
   2.750   0.7093   0.02497   0.01714  -0.0637   0.5769   1.0000
   3.000   0.7376   0.02460   0.01654  -0.0624   0.5723   1.0000
   3.250   0.7606   0.02510   0.01704  -0.0620   0.5604   1.0000
   3.500   0.7895   0.02463   0.01637  -0.0608   0.5557   1.0000
   3.750   0.8127   0.02504   0.01681  -0.0603   0.5436   1.0000
   4.000   0.8401   0.02481   0.01645  -0.0594   0.5369   1.0000
   4.250   0.8653   0.02487   0.01649  -0.0587   0.5266   1.0000
   4.500   0.8911   0.02488   0.01646  -0.0580   0.5175   1.0000
   4.750   0.9186   0.02461   0.01610  -0.0572   0.5093   1.0000
   5.000   0.9434   0.02478   0.01627  -0.0565   0.4988   1.0000
   5.250   0.9725   0.02432   0.01569  -0.0558   0.4918   1.0000
   5.500   0.9962   0.02461   0.01603  -0.0552   0.4802   1.0000
   5.750   1.0268   0.02401   0.01524  -0.0545   0.4741   1.0000
   6.000   1.0499   0.02434   0.01566  -0.0539   0.4617   1.0000
   6.250   1.0746   0.02452   0.01586  -0.0534   0.4511   1.0000
   6.500   1.1036   0.02420   0.01540  -0.0528   0.4435   1.0000
   6.750   1.1265   0.02464   0.01594  -0.0523   0.4319   1.0000
   7.000   1.1521   0.02477   0.01604  -0.0517   0.4224   1.0000
   7.250   1.1791   0.02473   0.01591  -0.0512   0.4133   1.0000
   7.500   1.2015   0.02526   0.01653  -0.0506   0.4025   1.0000
   7.750   1.2283   0.02543   0.01660  -0.0502   0.3944   1.0000
   8.000   1.2514   0.02594   0.01715  -0.0496   0.3846   1.0000
   8.250   1.2743   0.02651   0.01775  -0.0491   0.3751   1.0000
   8.500   1.3019   0.02662   0.01770  -0.0487   0.3663   1.0000
   8.750   1.3209   0.02747   0.01869  -0.0479   0.3558   1.0000
   9.000   1.3454   0.02800   0.01916  -0.0475   0.3475   1.0000
   9.250   1.3668   0.02871   0.01994  -0.0468   0.3384   1.0000
   9.500   1.3879   0.02957   0.02084  -0.0462   0.3301   1.0000
   9.750   1.4104   0.03027   0.02154  -0.0457   0.3221   1.0000
  10.000   1.4301   0.03133   0.02269  -0.0451   0.3148   1.0000
  10.250   1.4500   0.03224   0.02369  -0.0444   0.3073   1.0000
  10.500   1.4715   0.03321   0.02469  -0.0439   0.3005   1.0000
  10.750   1.4860   0.03440   0.02607  -0.0429   0.2931   1.0000
  11.000   1.5131   0.03512   0.02670  -0.0428   0.2866   1.0000
  11.250   1.5193   0.03676   0.02868  -0.0412   0.2797   1.0000
  11.500   1.5473   0.03729   0.02909  -0.0411   0.2730   1.0000
  11.750   1.5501   0.03908   0.03121  -0.0393   0.2661   1.0000
  12.000   1.5734   0.03946   0.03153  -0.0388   0.2581   1.0000
  12.250   1.5743   0.04118   0.03350  -0.0368   0.2512   1.0000
  12.500   1.5950   0.04141   0.03366  -0.0361   0.2428   1.0000
  12.750   1.5901   0.04331   0.03580  -0.0338   0.2365   1.0000
  13.000   1.5947   0.04432   0.03687  -0.0319   0.2297   1.0000
  13.250   1.6005   0.04560   0.03821  -0.0305   0.2234   1.0000
  13.500   1.5846   0.04836   0.04122  -0.0287   0.2184   1.0000
  13.750   1.6133   0.04799   0.04067  -0.0281   0.2107   1.0000
  14.000   1.5849   0.05218   0.04521  -0.0270   0.2069   1.0000
  14.250   1.5745   0.05519   0.04839  -0.0267   0.2018   1.0000
  14.500   1.5958   0.05528   0.04838  -0.0259   0.1954   1.0000
  14.750   1.5643   0.06085   0.05428  -0.0263   0.1921   1.0000
  15.000   1.5450   0.06544   0.05906  -0.0268   0.1882   1.0000
  15.250   1.5762   0.06402   0.05751  -0.0257   0.1812   1.0000
  15.500   1.5370   0.07131   0.06512  -0.0272   0.1789   1.0000
  15.750   1.4812   0.08161   0.07571  -0.0300   0.1777   1.0000
  16.000   1.5471   0.07452   0.06837  -0.0271   0.1676   1.0000
  16.250   1.5000   0.08370   0.07787  -0.0297   0.1663   1.0000
  16.500   1.4156   0.10018   0.09461  -0.0357   0.1674   1.0000
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