This unit provides an advanced study of aerodynamics as applied to aircraft design, focusing on the principles that govern airflow, lift, drag, and aerodynamic efficiency at high speeds. The course builds on fundamental aerodynamic principles and introduces more complex theories, including compressible flow, boundary layer behaviour, and high-speed aerodynamics.
Students will explore subsonic and supersonic aerodynamics in relation to aircraft design, analysing the behaviour of airflows over aerofoils, wings, and entire aircraft structures. The unit also delves into aerodynamic heating, flow separation, and the effects of turbulence, all of which are critical considerations in the design and performance of modern aircraft.
By the end of this unit, learners will have a comprehensive understanding of aerodynamic forces, flow behaviour, and how these principles influence the design of aircraft for optimal performance in both subsonic and supersonic flight.
During this unit, you will cover the below four learning outcomes:
LO1: Understand advanced aerodynamic forces and flow behaviour
LO2: Understand compressible flow and high-speed aerodynamics
LO3: Understand boundary layer theory and flow separation
LO4: Understand aerodynamic heating and its impact on high-speed flight
