Module overview
This module develops aerodynamic and thermodynamic methods for design of gas turbine engines. Starting from considerations of aircraft requirements and basic thermodynamics and fluid mechanics, students learn how the overall engine design can be tailored to achieve the required performance and develop a detailed understanding of turbomachinery design.
Linked modules
Pre-requisites: (FEEG2003 and SESM2017) or (SESA2022 and SESA2023)