GA 35-617

GA 35-617
DB Name: GA 35-617
Family: Riblett 35-series
Max thickness: 17.0% at x = 33.83% chord
Max camber: 4.5% at x = 43.76% chord
Available data sources:
JavaFoil+Calcfoil stall+Eppler ext transition
XFOIL ncrit=9
XFOIL ncrit=5
XFOIL ncrit=12
NF ncrit=5
NF ncrit=9
NF ncrit=12

Notes:

Coordinates generated by Jamie "TinBender" Halford spreadsheet GA_Airfoils_Ver_3.8.2_Stable.xls https://www.homebuiltairplanes.com/forums/threads/excel-based-ga-airfoil-coordinate-generation-for-windows.20803/
More information on Harry Riblett and his airfoils can be found in his Book "GA Airfoils" and in the Kitplanes article The Airfoil Adventures of Harry Riblett by Scott Spangler, July 19, 2013.
NeuralFoil data computed using Peter Sharpe's NeuralFoil: An airfoil aerodynamics analysis tool using physics-informed machine learning, 2023, GitHub repository: https://github.com/peterdsharpe/NeuralFoil. Version 0.3.1 xxxlarge