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![]() | 2018/9 |
![]() | Department of Mechanical Engineering |
![]() | 6 [equivalent to 12 CATS credits] |
![]() | 120 |
![]() | Honours (FHEQ level 6) |
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![]() | EX 100% |
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![]() | 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 conditions. Understand basic turbomachinery design including the required cooling systems. 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; engine performance; turbine cooling. Topics for self study that could be examined. |
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ME30218 is Compulsory on the following programmes:Department of Mechanical Engineering
ME30218 is Optional on the following programmes:Department of Mechanical Engineering
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Notes:
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