Max thickness: 2.4% at x = 21.45% chord
Max camber: 3.8% at x = 47.85% 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.