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GOE 285 AIRFOIL (goe285-il)

GOE 285 AIRFOIL - Gottingen 285 airfoil


Airfoil goe285-il
Details Dat file Parser  
(goe285-il) GOE 285 AIRFOIL
Gottingen 285 airfoil
Max thickness 11.7% at 30% chord.
Max camber 3.7% at 30% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 285 AIRFOIL
       18.       18.

 0.0000000 0.0000000
 0.0125000 0.0251200
 0.0250000 0.0344400
 0.0500000 0.0495800
 0.0750000 0.0607300
 0.1000000 0.0695700
 0.1500000 0.0836600
 0.2000000 0.0905400
 0.2500000 0.0942200
 0.3000000 0.0958100
 0.4000000 0.0930800
 0.5000000 0.0861500
 0.6000000 0.0744200
 0.7000000 0.0602900
 0.8000000 0.0431600
 0.9000000 0.0249300
 0.9500000 0.0147200
 1.0000000 0.0030000

 0.0000000 0.0000000
 0.0125000 -.0167800
 0.0250000 -.0210600
 0.0500000 -.0254200
 0.0750000 -.0264700
 0.1000000 -.0266300
 0.1500000 -.0253400
 0.2000000 -.0240600
 0.2500000 -.0227700
 0.3000000 -.0214900
 0.4000000 -.0189200
 0.5000000 -.0163500
 0.6000000 -.0137800
 0.7000000 -.0112100
 0.8000000 -.0086400
 0.9000000 -.0051700
 0.9500000 -.0027800
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 285 AIRFOIL (goe285-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe285-il50,000926.1 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe285-il50,000534.6 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe285-il100,000947.2 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe285-il100,000550.1 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe285-il200,000965.2 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe285-il200,000565.2 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe285-il500,000989.3 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe285-il500,000587 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe285-il1,000,0009109.1 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe285-il1,000,0005103.5 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
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