X-35 LOW DRAG BODY

X-35 LOW DRAG BODY (J. HYDRONAUTICS, JULY 1974)
DB Name: X-35 LOW DRAG BODY
Family: Uncategorized
Max thickness: 20.6% at x = 58.01% chord
Max camber: 0.0% at x = 99.88% chord
Available data sources:
JavaFoil+Calcfoil stall+Eppler ext transition
XFOIL ncrit=5
XFOIL ncrit=12
NF ncrit=5
NF ncrit=9
NF ncrit=12

Notes:

Low drag axismmetric body presented in Parsons, Goodson, and Goldschmied, "Shaping of Axisysmmetric Bodies for Minimum Drag in Incompressible Flow", Journal of Hydronautics, Vol. 8 No. 3, July 1974.
https://arc.aiaa.org/doi/10.2514/3.48131
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