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Carrying out thermodynamic and flow analyses of engine components; understanding the aero-thermodynamic aspects of aircraft engine component design and their performance relationship.
The course will review the fundamental principles of thermodynamics, combustion and fluid mechanics and how they may be applied to aircraft propulsion. The theory of jet propulsion is introduced along with the concepts relating to thrust generation. Propulsion cycle analysis and the performances for different engine cycles and various engine components will be evaluated. Rocket propulsion concepts will also be discussed.
Approval from Head of Department
ENME660
Dan Zhao
For detailed course, policy, regulatory and integrity information, please refer to the UC web site, or see relevant Course or Department LEARN pages, (which are available to enrolled students).
Domestic fee $1,002.00
International fee $5,625.00
* All fees are inclusive of NZ GST or any equivalent overseas tax, and do not include any programme level discount or additional course-related expenses.
Maximum enrolment is 40
For further information see Mechanical Engineering .