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Aircraft Propulsion

When you'll study it
Semester 1
CATS points
15
ECTS points
7.5
Level
Level 7
Module lead
Edward Richardson
Academic year
2025-26

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)