Course/Module
Organiser, Group Design Project. (Short Courses)
Computational Mechanics S7 - MSc AERO70009
Aims
This module builds on the optional Finite Elements module and introduces advanced concepts in the application of the finite element method to the analysis of aerostructures. It explores the basics of non-linear structural analysis and relevant solution methods based on the finite element method and introduces the Boundary Element Method for two-dimensional potential, elastostatic and acoustic problems.
Role
Lecturer
Aeroelasticity - AERO70004 / 97083
Aims
This module introduces the theory and practice of aeroelasticity in fixed-wing aircraft. Aeroelasticity is concerned with coupled problems involving structural dynamics and unsteady flows, such as vibrations of wings in flight, their dynamic response to atmospheric turbulence, and the changes on control effectiveness of deforming air vehicles. All those are addressed in this module, which will introduce the most common analytical and numerical models used for aeroelastic analysis.
Role
Lecturer
Computational Mechanics S7 - AERO70009 / 96015
Aims
This module builds on the optional Finite Elements module and introduces advanced concepts in the application of the finite element method to the analysis of aerostructures. It explores the basics of non-linear structural analysis and relevant solution methods based on the finite element method and introduces the Boundary Element Method for two-dimensional potential, elastostatic and acoustic problems.
Role
Lecturer
Emerging Technology for Green Aviation - MSc AERO70031
Aims
The aim is to introduce the key technological advances, and the corresponding underlying principles, for a greener aviation. This includes the potential advantages of alternative configurations, flow control and drag-reduction using both active and passive systems, load alleviation systems and structural weight-reduction strategies and aircraft end of life and recycling. The module will consist of timetabled lectures and tutorials, delivered by academics with the relevant research expertise.
Role
Lecturer
Aeroelasticity S9 - MSc AERO70004
Aims
This module introduces the theory and practice of aeroelasticity in fixed-wing aircraft. Aeroelasticity is concerned with coupled problems involving structural dynamics and unsteady flows, such as vibrations of wings in flight, their dynamic response to atmospheric turbulence, and the changes on control effectiveness of deforming air vehicles. All those are addressed in this module, which will introduce the most common analytical and numerical models used for aeroelastic analysis.
Role
Lecturer