CURTIS CR-1

CURTIS CR-1 AIRFOIL
DB Name: cr1
Family: Uncategorized
Max thickness: 12.2% at x = 24.74% chord
Max camber: 4.7% at x = 41.73% 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 UIUC Airfoil Coordinates Database https://m-selig.ae.illinois.edu/ads/coord_database.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