Max thickness: 4.0% at x = 15.59% chord
Max camber: 1.5% at x = 37.73% 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.