Aircraft Propulsion Systems

Code School Level Credits Semesters
MMME4010 Mechanical, Materials & Manufacturing Engineering 4 10 Spring Malaysia
Code
MMME4010
School
Mechanical, Materials & Manufacturing Engineering
Level
4
Credits
10
Semesters
Spring Malaysia

Summary

An advanced module covering the following topics:



Principles of aircraft jet propulsion

Principles of the gas turbine engine

Layout of jet engines

Compressible flow in gas turbine engines

Principles of turbomachinery as applied to gas turbine engines

Characteristics of main components of a jet engine

Design of aircraft engines

Target Students

Primarily for 4th/3rd year students in the Department of Mechanical, Materials and Manufacturing EngineeringPassing Mark/Grade: 40% for UG BEng; 50% for UG MEng ; 50% for PG MSc

Classes

Assessment

Educational Aims

The aims of the module are:To provide an understanding of the basic thermofluid principles of aircraft propulsion and gas turbine enginesTo provide knowledge of the layout and design principles of jet engines and how individual components can be designed to achieve the required performance

Learning Outcomes

On successful completion of this module students will be able to:

LO1 : Apply core engineering science (from pre-requisite and current modules) to evaluate gas turbine thermofluid systems.- AHEP4: M1; EAC: PO1.

LO2 : Formulate appropriate analysis and computational methods related to the thermofluids design of gas turbines.- AHEP4: M2; EAC: PO2.

LO3 : Evaluate and appraise an appropriate system and components for propulsion scenarios.– AHEP4: M13; EAC: PO2.

LO4 : Identify and assess appropriate technologies/components by critically appraising cost and sustainability issues. – AHEP4: M4; EAC: PO4.                                                         

LO5 : Critically analyse and communicate engineering calculations, data analysis and system wide design conclusions.)-AHEP4: M5, M3; EAC: PO3, PO5.

 

 

 

Conveners

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Last updated 09/01/2025.