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GOE 425 AIRFOIL (goe425-il)

GOE 425 AIRFOIL - Gottingen 425 airfoil


Airfoil goe425-il
Details Dat file Parser  
(goe425-il) GOE 425 AIRFOIL
Gottingen 425 airfoil
Max thickness 16% at 29.3% chord.
Max camber 4.5% at 39.3% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 425 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0111700 0.0249000
 0.0230000 0.0374300
 0.0470300 0.0554200
 0.0713300 0.0686200
 0.0957300 0.0797300
 0.1448300 0.0966600
 0.1941100 0.1099900
 0.2933700 0.1238100
 0.3933700 0.1237600
 0.4940100 0.1118500
 0.5950000 0.0934600
 0.6962100 0.0707800
 0.7974200 0.0481000
 0.8986700 0.0248200
 0.9493100 0.0129400
 1.0000000 0.0005500

 0.0000000 0.0000000
 0.0134800 -.0182800
 0.0262000 -.0224000
 0.0514500 -.0270400
 0.0766700 -.0310900
 0.1017400 -.0324500
 0.1518800 -.0351700
 0.2019700 -.0367800
 0.3019500 -.0363300
 0.4017500 -.0325900
 0.5013600 -.0254500
 0.6009700 -.0181200
 0.7006000 -.0121800
 0.8004300 -.0080400
 0.9002600 -.0047900
 0.9501700 -.0032200
 1.0000000 -.0005500
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Lednicer format dat file
Selig format dat file

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Polars for GOE 425 AIRFOIL (goe425-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe425-il50,00095.2 at α=8.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe425-il50,000517.4 at α=2.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe425-il100,000922.7 at α=2.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe425-il100,000544.6 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe425-il200,000969.8 at α=10.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe425-il200,000574 at α=8.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe425-il500,0009111 at α=9°Mach=0 Ncrit=9Xfoil predictionDetails
   goe425-il500,0005108.4 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe425-il1,000,0009142.1 at α=8°Mach=0 Ncrit=9Xfoil predictionDetails
   goe425-il1,000,0005132.4 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
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