10 Credits SPRING

Pre-requisites: A-level Maths and Physics

MEC132 or MEC192

Aims/Description: 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.

Staff Contact: HOWELL ROBERT J
Teaching Methods: Lectures, Tutorials, Problem solving, Independent Study, Formal Exam
Assessment: Formal Exam
WebCT resources are available for this module

Information on the department responsible for this unit (Mechanical Engineering):

Departmental Home Page
Teaching timetable


The content of our courses is reviewed annually to make sure it's up-to-date and relevant. Individual modules are occasionally updated or withdrawn. This is in response to discoveries through our world-leading research; funding changes; professional accreditation requirements; student or employer feedback; outcomes of reviews; and variations in staff or student numbers. In the event of any change we'll consult and inform students in good time and take reasonable steps to minimise disruption.

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Teaching methods and assessment displayed on this page are indicative for 2021-22. Students will be informed by the academic department of any changes made necessary by the ongoing pandemic.

Western Bank, Sheffield, S10 2TN, UK