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Due to the exceptional circumstances caused by the COVID-19 pandemic, the learning activities, assessments and attendance requirements for this unit may be subject to late changes. Please refer to this unit outline regularly for up to date information and to notices in the unit’s Canvas site for any adjustments.

Unit of study_

AERO9261: Propulsion

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 AERO9261
Academic unit Aerospace, Mechanical and Mechatronic
Credit points 6
Prerequisites:
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(AMME9261 and AMME9262) or AMME5200
Corequisites:
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None
Prohibitions:
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AERO8261
Assumed knowledge:
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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:

  • LO1. write an engineering report on an experimental test
  • LO2. discuss and present engine performance and design data in a written report
  • LO3. explain engine performance and different engine types in an oral exam
  • LO4. design and select a gas turbine engine type for a given application
  • LO5. select appropriate engine cycles and propellers for a given aircraft and flight conditions
  • LO6. carry out a cycle analysis of a gas turbine engine, including ramjet and turbo-fan engines
  • LO7. understand the working of various components of gas turbines and how their interaction results in the overall engine performance
  • LO8. identify relevant data to estimate performance of existing aircraft engines
  • LO9. solve systems of non-linear equations governing propeller performance
  • LO10. solve thermodynamic cycle calculations for both design point and off-design calculations.

Unit outlines

Unit outlines will be available 2 weeks before the first day of teaching for 1000-level and 5000-level units, or one week before the first day of teaching for all other units.

There are no unit outlines available online for previous years.