Max thickness: 2.1% at x = 18.40% chord
Max camber: 3.0% 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 Hand and Catapult Launched Glider.