Max thickness: 8.5% at x = 26.49% chord
Max camber: 3.5% at x = 56.01% 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 free flight models. Both airfoils are with the thickness of 8.5%c but camber at
MID 108a is 3.5% and at MID 108b is 3.0%. LE radius
at MID 108a is 0.8%c, at MID 108b is 0.55%c.