units
MAE3405
Faculty of Engineering
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6 points, SCA Band 2, 0.125 EFTSL
SynopsisThis 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. Objectives
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. Assessment
Problem solving: 15% Chief examiner(s)Contact hoursFive 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 |