Using a sketch / diagram show the load path between major components of a fuselage structure (bulkheads, formers, frame assemblies, skin, longerons, stringers). Explain how the load is transferred.
There are basically two ways loads are transferred
– Surface forces which act upon the surface of the structure,
e.g. aerodynamic and hydrostatic pressure
– Body forces which act over the volume of the structure and
are produced by gravitational and inertial effects.
• Eg. Turns, dive pull-up etc
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