TP202-9%

TP202-9%
DB Name: TP202-9%
Family: Platon
Max thickness: 9.0% at x = 30.06% chord
Max camber: 1.7% at x = 43.76% 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 TraCFoil.
Commercial use of the airfoil may be restricted by the designer's copyright.
aerobatics in light weather with gliders from 2m50 to 3m
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