DA8523

DA8523 - Don Ayers
DB Name: DA8523
Family: Ayers
Max thickness: 8.5% at x = 23.07% chord
Max camber: 2.3% at x = 33.83% 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:

The first two digits represent the airfoil thickness in tenths of a percent.
The second two digits represent the camber in tenths of a percent.
Coordinates from https://www.rcgroups.com/forums/showthread.php?1016239-Download-airfoils-here
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