| Unit name | Aircraft Propulsion |
|---|---|
| Unit code | AENGM9002 |
| Credit points | 10 |
| Level of study | M/7 |
| Teaching block(s) |
Academic Year (weeks 1 - 52) |
| Unit director | |
| Open unit status | Not open |
| Pre-requisites |
None |
| Co-requisites |
None |
| School/department | Department of Aerospace Engineering |
| Faculty | Faculty of Engineering |
This module aims to provide a comprehensive overview of the characteristics of gas turbines for application in aircraft and helicopters. This will include technical performance, design and manufacturing aspects as well as their impact on the design of aircraft and helicopters and their relevance to operation and support. On completion of the module, delegates will be able to: Understand the fundamental thermodynamic principles involved; Predict the performance of propulsion systems over the whole flight envelope; Describe the aerodynamic and other factors affecting component performance; Understand the effects of aircraft/helicopter requirements, operation, maintenance and emissions on engine selection; Show a physical understanding of propulsion system installation and the basic interaction between airframe and engine characteristics; Appreciate the requirements relating to mechanical integrity, rig and component testing and certification.
