ELINA

ELINA
DB Name: ELINA
Family: Uncategorized
Max thickness: 9.5% at x = 30.06% chord
Max camber: 3.0% at x = 37.73% chord
Available data sources:
JavaFoil+Calcfoil stall+Eppler ext transition
XFOIL ncrit=9
XFOIL ncrit=12
XFOIL ncrit=5
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.

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