Modelling and Control of Aircraft Gas Turbine Engines

Qi, Oliver Feng (1992) Modelling and Control of Aircraft Gas Turbine Engines. PhD thesis, University of Glasgow.

Abstract

In this thesis the main theme is to demonstrate the potential performance improvements of gas turbine engines that are brought about by using multivariable control systems. Particular emphasis is on designing such control systems using the well-established engine thermodynamic models since these models are considered as the true representations of engine thermodynamic process and enable engine variable geometry features to be easily incorporated and their effects studied.

• Item Type: Thesis (PhD)
• Qualification Level: Doctoral
• Keywords: Mechanical engineering, Aerospace engineering
• Date of Award: 1992
• Depositing User: Enlighten Team
• Unique ID: glathesis:1992-77321
• Copyright: Copyright of this thesis is held by the author.
• Date Deposited: 14 Jan 2020 09:12
• Last Modified: 14 Jan 2020 09:12
• URI: https://theses.gla.ac.uk/id/eprint/77321