RAE 2822

RAE 2822 AIRFOIL
DB Name: rae2822
Family: RAE
Max thickness: 12.1% at x = 37.73% chord
Max camber: 1.3% at x = 76.22% chord
Available data sources:
JavaFoil+Calcfoil stall+Eppler ext transition
XFOIL ncrit=9
CFD (BigFoil, Mach 0.13)
XFOIL ncrit=5
XFOIL ncrit=12
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
CFD Data computed by BigFoil, RANS k-Omega.
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