Useful links
This unit aims to develop and understanding of aircraft propulsion systems. Students will learn to solve problems related to the analysis and selection of various propulsion systems in use- propellers, gas turbines, etc. The topics covered include: Propulsion unit requirements for subsonic and supersonic flight; thrust components, efficiencies, additive drag of intakes; Piston engine components and operation; Propeller theory; Operation, components and cycle analysis of gas turbine engines, turbojets, turbofans, turboprops, ramjets; Components: compressor, fan, burner, turbine, nozzle; Efficiency of components: Off-design considerations; Future directions: minimisation of noise and pollution, scram-jets, hybrid engines.
Code | AERO8261 |
---|---|
Academic unit | Aerospace, Mechanical and Mechatronic |
Credit points | 6 |
Prerequisites:
?
|
None |
---|---|
Corequisites:
?
|
None |
Prohibitions:
?
|
AERO9261 |
Assumed knowledge:
?
|
Mathematics and Physics to a level of Bachelor of Science or equivalent. Good knowledge of fluid dynamics and thermodynamics |
At the completion of this unit, you should be able to:
Unit outlines will be available 2 weeks before the first day of teaching for the relevant session.
Key dates through the academic year, including teaching periods, census, payment deadlines and exams.
Enrolment, course planning, fees, graduation, support services, student IT
Code of Conduct for Students, Conditions of Enrollment, University Privacy Statement, Academic Integrity
Academic appeals process, special consideration, rules and guidelines, advice and support
Policy register, policy search
Scholarships, interest free loans, bursaries, money management
Learning Centre, faculty and school programs, Library, online resources
Student Centre, counselling & psychological services, University Health Service, general health and wellbeing