Max thickness: 4.2% at x = 19.89% chord
Max camber: 2.0% at x = 56.00% 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.