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GOE 265 AIRFOIL (goe265-il)

GOE 265 AIRFOIL - Gottingen 265 airfoil


Airfoil goe265-il
Details Dat file Parser  
(goe265-il) GOE 265 AIRFOIL
Gottingen 265 airfoil
Max thickness 7.7% at 14.9% chord.
Max camber 7.3% at 39.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 265 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0122600 0.0266100
 0.0246500 0.0390200
 0.0494900 0.0564400
 0.0743800 0.0689700
 0.0993000 0.0778900
 0.1491700 0.0923400
 0.1990900 0.1012800
 0.2990400 0.1069800
 0.3990700 0.1035700
 0.4991700 0.0929700
 0.5993000 0.0780600
 0.6994600 0.0602600
 0.7996300 0.0416600
 0.8998100 0.0215500
 0.9498900 0.0118000
 1.0000000 0.0010500

 0.0000000 0.0000000
 0.0125700 -.0082900
 0.0250900 -.0097800
 0.0500700 -.0075500
 0.0750200 -.0023300
 0.0999600 0.0039900
 0.1498600 0.0159400
 0.1997700 0.0252900
 0.2996600 0.0376800
 0.3996300 0.0415800
 0.4996400 0.0399700
 0.5996900 0.0346700
 0.6997600 0.0266600
 0.7998500 0.0171600
 0.8999299 0.0073500
 0.9499800 0.0027000
 1.0000000 -.0010500
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Lednicer format dat file
Selig format dat file

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Polars for GOE 265 AIRFOIL (goe265-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe265-il50,000923 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   goe265-il50,000539.1 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe265-il100,000952.6 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe265-il100,000561.5 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe265-il200,000979.3 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   goe265-il200,000582 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe265-il500,0009111.2 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe265-il500,0005109.1 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe265-il1,000,0009136.5 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe265-il1,000,0005129.7 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
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