MID 108b

MID 108b
DB Name: MID 108b
Family: Midic
Max thickness: 8.5% at x = 26.49% chord
Max camber: 3.0% at x = 56.01% 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 TraCFoil.
Commercial use of the airfoil may be restricted by the designer's copyright.
For free flight models. Both airfoils are with the thickness of 8.5%c but camber at
MID 108a is 3.5% and at MID 108b is 3.0%. LE radius
at MID 108a is 0.8%c, at MID 108b is 0.55%c.
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