AZ2005tip

AZ2005tip
DB Name: AZ2005tip
Family: Zutter
Max thickness: 8.8% at x = 24.73% chord
Max camber: 1.3% 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.
http://alain.zutter.free.fr/Ailes/AZ2005/index.html
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