Max thickness: 15.0% at x = 33.83% chord
Max camber: 2.3% at x = 28.24% 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.
Hang glider for Re 300k up to more than 2M