AER284   Aerostructures   (10 credits)

Description

The overall aim of the course is to explain clearly some fundamental theories of solid mechanics for the modelling of basic aircraft structure problems. In specific terms this means truss system analysis, bending of statically determinate and indeterminate beams, analysis of cross-sections, axes of symmetry, section properties for structural beams, beams loaded by moments and by UDLs, Macaulay's method for beams under point loads and moments, general stress, strain, and displacements in open and closed section thin-walled beams, shear flow and shear centre, torsion of closed and open section beams, torsion of beams, aircraft structural materials, and aircraft structural components.

Reading List