Max thickness: 7.5% at x = 23.08% chord
Max camber: 4.0% at x = 45.81% 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 P-30 rubber powered. Airfoil MID 105 has thickness of 7.5%c, camber of 4%c, leading edge radius of
0.5%c, and trailling edge gap of 0.5%c.