Max thickness: 4.1% at x = 18.39% chord
Max camber: 1.2% at x = 31.92% 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.