Aerospace structural mechanics

This unit aims to develop an understanding of the analytical methodologies used in strength and stiffness assessment of aircraft structures. The unit will develop an understanding of the translation of aerodynamics and ground loading on aircraft wings and fuselage to the overall airframe. An understanding of the concept of structural idealisation and constraint will be developed along with real-world limitations. The principles of stressed skin construction will be considered in detail. Fracture mechanics and the role crack growth plays in limiting the airworthiness of aircraft will be considered. The unit will provide you with the tools necessary to design and maintain aerospace structures.