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Academic Year: | 2012/3 |
Owning Department/School: | Department of Mechanical Engineering |
Credits: | 6 |
Level: | Masters UG & PG (FHEQ level 7) |
Period: |
Semester 1 |
Assessment: | CW20EX80 |
Supplementary Assessment: | Mandatory extra work (where allowed by programme regulations) |
Requisites: | |
Description: | Aims: To provide knowledge of the development, performance and design of gas-turbine aeroengines. To apply the fundamentals of fluid mechanics and thermodynamics to the performance and design of aircraft and aeroengines. To introduce the basic mechanics of turbomachinery. Learning Outcomes: After taking this unit the student should be able to: * Understand the fundamental differences between the performance characteristics of turbojet, turbofan and turboprop engines. * Analyse thermodynamic cycles for turboprop, turboshaft, turbojet and turbofan engines. * Understand principles and performance of compressor, turbine, combustor, intake and exhaust nozzle. * Calculate performance of engines at design and off-design conditions. Understand basic turbomachinery design. * Undertake individual independent study of relevant topic. Skills: Problem solving; numeracy; working independently. Content: Birth of jet engine; engine classification; operational envelope; thrusts and efficiencies; thermodynamic cycles (turboshaft, turbojet, turbofan); combustors; intakes (subsonic and supersonic), afterburners and nozzles; design and off-design performance; turbine cooling. Topics for self study that could be examined. |
Programme availability: |
ME50218 is Compulsory on the following programmes:Department of Mechanical Engineering
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