Max thickness: 6.6% at x = 21.46% chord
Max camber: 2.4% at x = 41.74% 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.
horizontal stabilizer at free flight models (F1A,B,C,...)