HS 522

HS 522
DB Name: HS 522
Family: Siegmann
Max thickness: 8.7% at x = 28.24% chord
Max camber: 2.0% at x = 28.24% 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 from TraCFoil.
Commercial use of the airfoil may be restricted by the designer's copyright.
F5D, F3F, F3B
http://www.aerodesign.de/
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