ONERA D, BLUNT TRAILING EDGE

ONERA D AIRFOIL, BLUNT TRAILING EDGE
DB Name: Onera_D_bluntTE
Family: Onera
Max thickness: 9.8% at x = 37.73% chord
Max camber: 0.0% at x = 63.88% 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 NASA NPARC Alliance Validation Archivehttps://www.grc.nasa.gov/WWW/wind/valid/m6wing/m6wing.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. Version 0.3.1 xxxlarge