Overview

This unit builds on concepts in MAE3401 and relates aircraft and rocket engines to the laws of thermodynamics, various fuel-air power cycles, their real behaviour plus fuel and combustion chemistry. The efficiency and performance of aircraft engines based on electric, piston and gas turbine platforms are examined along with rotor … For more content click the Read More button below.

Offerings

S2-01-CLAYTON-ON-CAMPUS

Contacts

Chief Examiner(s)

Dr Daniel Duke

Unit Coordinator(s)

Dr Daniel Duke

Teaching approach

Active learning
Case-based teaching
Problem-based learning

Assessment summary

Continuous assessment: 40%

Final assessment: 60%

This unit contains a hurdle requirement that you must achieve to be able to pass the unit. You are required to achieve at least 45% in the total continuous assessment component and at least 45% in the final assessment component. The consequence of not achieving a hurdle requirement is a fail grade (NH) and a maximum mark of 45 for the unit.

Assessment

1 - Assignments
2 - Lab report
3 - Weekly quizzes
4 - Final assessment

Scheduled and non-scheduled teaching activities

Laboratories
Practical activities
Workshops

Workload requirements

Workload

Learning resources

Required resources

Other unit costs

The following item is mandatory for practical aspects of the unit and should be purchased at your own cost as you will be reusing them throughout your course.

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Availability in areas of study

E3001 Bachelor of Engineering (Honours) - Specialisation: Aerospace engineering