Decided rib spacing based on practical placement, and buckling analysis of skin. Sized spars to with stand deflection. Sized fasteners for attachment of wing to fuselage. Conducted FEA analysis of new structure in ANSYS.
Decided rib spacing based on practical placement, and buckling analysis of skin. Sized spars to with stand deflection. Sized fasteners for attachment of wing to fuselage. Conducted FEA analysis of new structure in ANSYS.