AER345   Aero Propulsion   (10 credits)

Description

The aim of this module is to provide the students with an understanding of principles of operation of gas turbines, as applied to aero propulsion and power generation.The module introduces the theory of gas turbines and how they should function. The study is based on fundamental thermodynamic and fluid mechanic analyses and introduces methods for improving efficiencies and increasing specific work output. The effect of simple thermodynamics of combustion, jet engine losses and efficiences are considered, together with an analysis of turbojet and turbofan designs.Website Version:This module provides students with an understanding of principles of operation of gas turbines, pulse-jets, RAM-jets and solid and liquid fuelled rocket engines as applied to aero propulsion. The understanding is built upon fundamental thermodynamic and fluid mechanic analyses of components and systems for each propulsion method. Methods for improving efficiencies and increasing specific work output of components are also introduced as well as an introduction to combustion, losses and efficiencies.

Reading List