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GOE 507 AIRFOIL (goe507-il)

GOE 507 AIRFOIL - Gottingen 507 airfoil


Airfoil goe507-il
Details Dat file Parser  
(goe507-il) GOE 507 AIRFOIL
Gottingen 507 airfoil
Max thickness 8.7% at 30% chord.
Max camber 2.9% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 507 AIRFOIL
       13.       13.

 0.0000000 0.0000000
 0.0250000 0.0241400
 0.0500000 0.0337800
 0.1000000 0.0480500
 0.2000000 0.0641000
 0.3000000 0.0706500
 0.4000000 0.0712000
 0.5000000 0.0672500
 0.6000000 0.0603000
 0.7000000 0.0488500
 0.8000000 0.0339000
 0.9000000 0.0169500
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0250000 -.0178600
 0.0500000 -.0212200
 0.1000000 -.0234500
 0.2000000 -.0199000
 0.3000000 -.0158500
 0.4000000 -.0128000
 0.5000000 -.0102500
 0.6000000 -.0087000
 0.7000000 -.0071500
 0.8000000 -.0056000
 0.9000000 -.0030500
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 507 AIRFOIL (goe507-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe507-il50,000937.6 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe507-il50,000538 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe507-il100,000955.4 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe507-il100,000553.6 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe507-il200,000973.8 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   goe507-il200,000567.4 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe507-il500,000995.1 at α=2.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe507-il500,000582 at α=3.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe507-il1,000,0009106.1 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   goe507-il1,000,000589.2 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
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