Overview

To provide students with a thorough understanding of energy systems, heat transfer and thermodynamic applications to Internal Combustion engines. An advanced understanding of the theory and operation of gas turbine engines is also addressed

Requisites

Prerequisites

Assumed Knowledge

PHY10002 Introduction to Physics

AND

MTH10008 Aviation Mathematics

Teaching periods
Location
Start and end dates
Last self-enrolment date
Census date
Last withdraw without fail date
Results released date
Semester 1
Location
Hawthorn
Start and end dates
02-March-2026
31-May-2026
Last self-enrolment date
15-March-2026
Census date
31-March-2026
Last withdraw without fail date
21-April-2026
Results released date
07-July-2026

Unit learning outcomes

Students who successfully complete this unit will be able to:

  1. Describe basic thermodynamics as applied to engine systems
  2. Apply thermodynamic principles to analyse and evaluate the design and operation of internal combustion engines
  3. Apply thermodynamic principles to analyse and evaluate the design and operation of gas turbine engines
  4. Interpret and apply aircraft engine certification, regulatory, and maintenance requirements in typical operational scenarios
  5. Identify and describe key current and emerging engine technologies

Teaching methods

Hawthorn

Type Hours per week Number of weeks Total (number of hours)
On-campus
Lecture
2.00  12 weeks  24
On-campus
Workshop
1.00  12 weeks  12
On-campus
Lab
2.00  1 weeks 2
Online
Directed Online Learning and Independent Learning
1.00 12 weeks 12
Unspecified Activities 
Independent Learning
8.33  12 weeks  100
TOTAL     150

Assessment

Type Task Weighting ULOs
Assignment 1 Individual  10 - 20%  1,2,3 
Assignment 2 Individual 10 - 20% 3,4,5
Examination Individual  30 - 40%  1,2,3,4,5 
Tutorial Exercises Group 10 - 20%  1,2,3,4,5
Quizzes Individual  10 - 20%  1,2,3,4,5 

Hurdle

As the minimum requirements of assessment to pass a unit and meet all ULOs to a minimum standard, an undergraduate student must have achieved:

(i) an aggregate mark of 50% or more, and
(ii) at least 40% in the final exam.

Students who do not successfully achieve hurdle requirement (ii) will receive a maximum of 45% as the total mark for the unit.

Content

  • Principles, components and operation of Internal Combustion Engines
  • Principles, components and operation of Basic Gas Turbines Engines
  • Basic Engineering Units and Unit Conversions
  • Review of First Law of Thermodynamics 
  • Heat transfer processes; basic heat exchanger design
  • Engine operation including FADEC/EEC
  • Engine derivatives and performance impact
  • Regulatory requirements
  • Fuel; types, limitations and availability

Study resources

Reading materials

A list of reading materials and/or required textbooks will be available in the Unit Outline on Canvas.