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GOE 767 AIRFOIL (goe767-il)

GOE 767 AIRFOIL - Gottingen 767 airfoil


Airfoil goe767-il
Details Dat file Parser  
(goe767-il) GOE 767 AIRFOIL
Gottingen 767 airfoil
Max thickness 12% at 20% chord.
Max camber 1.5% at 20% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 767 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0299000
 0.0250000 0.0400000
 0.0500000 0.0533000
 0.1000000 0.0672000
 0.1500000 0.0738000
 0.2000000 0.0750000
 0.2500000 0.0737000
 0.3000000 0.0705000
 0.4000000 0.0609000
 0.5000000 0.0498000
 0.6000000 0.0390000
 0.7000000 0.0294000
 0.8000000 0.0197000
 0.9000000 0.0097000
 0.9500000 0.0050000
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0190000
 0.0250000 -.0260000
 0.0500000 -.0348000
 0.1000000 -.0420000
 0.1500000 -.0444000
 0.2000000 -.0450000
 0.2500000 -.0452000
 0.3000000 -.0443000
 0.4000000 -.0410000
 0.5000000 -.0364000
 0.6000000 -.0306000
 0.7000000 -.0236000
 0.8000000 -.0162000
 0.9000000 -.0084000
 0.9500000 -.0042000
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 767 AIRFOIL (goe767-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe767-il50,000915.5 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe767-il50,000523.9 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe767-il100,000930.3 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe767-il100,000538.6 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe767-il200,000949.7 at α=8.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe767-il200,000554.9 at α=8°Mach=0 Ncrit=5Xfoil predictionDetails
   goe767-il500,000976 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe767-il500,000574.7 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe767-il1,000,000993.1 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe767-il1,000,000591.5 at α=9.25°Mach=0 Ncrit=5Xfoil predictionDetails
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