Max thickness: 10.0% at x = 31.92% chord
Max camber: 2.1% at x = 39.72% chord
Available data sources:
JavaFoil+Calcfoil stall+Eppler ext transition
Coordinates from TraCFoil.
Commercial use of the airfoil may be restricted by the designer's copyright.
For a 4.05m Blanick L13.