units

MAE3405

Faculty of Engineering

Undergraduate - Unit

This unit entry is for students who completed this unit in 2014 only. For students planning to study the unit, please refer to the unit indexes in the the current edition of the Handbook. If you have any queries contact the managing faculty for your course or area of study.

print version

6 points, SCA Band 2, 0.125 EFTSL

Refer to the specific census and withdrawal dates for the semester(s) in which this unit is offered, or view unit timetables.

LevelUndergraduate
FacultyFaculty of Engineering
Organisational UnitDepartment of Mechanical and Aerospace Engineering
OfferedClayton Second semester 2014 (Day)
Coordinator(s)D Honnery

Synopsis

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. Efficiency and performance of aircraft engines based on piston and gas turbine platforms is examined along with piston and turboprop engines and propeller design for subsonic speed. For jets and turbofan engines, nozzle design for transonic to supersonic speed is covered, as are supersonic engines. The unit concludes with an introduction to rocket motors and their design and performance for both atmospheric and space flight.

Outcomes

Introduce students to the design, operation and performance of engines used for aircraft and rockets:

  1. Understand the thermodynamics of fuel-air power cycles used for aircraft propulsion systems and undertake calculations of their thermodynamic properties.
  2. Recognise the differences in real versions of the power cycles relative to their fuel-air analogues.
  3. Demonstrate knowledge of the fuels used in aircraft and rocket engines and be able to undertake simple combustion related calculations dealing with these fuels.
  4. Understand and undertake calculations on the operation and performance of piston engines, turboprops, and ramjets.
  5. Understand and calculate the effects of high speed flight on jets, turbofans and ramjets intakes.
  6. Demonstrate knowledge of propeller design through the application of various blade theories
  7. Understand and undertake calculations on propeller operation and performance.
  8. Understand and undertake calculations on the operation and performance of propulsion systems used in rockets operating in the atmosphere and in space.
  9. Fuelling requirements of propulsion systems.
  10. Aircraft and space flight propulsion systems, their operation and performance. Propeller design, operation and performance based on simple aerodynamic principles.

Assessment

Problem solving
Laboratory work: 30%
Examination: (3 hours) 70%

Chief examiner(s)

Workload requirements

Five hours of contact hours - usually 3 hours lectures and 2 hours practice sessions or laboratories per week as well as 7 hours of private study per week

Prerequisites