In this course, you will develop your understanding of the theories underpinning low speed and high-speed aerodynamics, and study advanced topics in aerodynamics. The course builds on the concepts underlying the generation of lift and drag in aircraft, and the main methods available to determine aerodynamic forces considering different flow conditions (2D and 3D, incompressible and compressible, inviscid or viscous flow). Advanced topics include an overview of theories applied to rotary aerodynamics (lifting disc and blade element theories, hovering/vertical/forward flight mechanics), computational, experimental and flight testing. The main governing equations for aircraft flight mechanics are presented and used to analyse the flight performance of aircraft in different situations.