Merahi, Larbi (1988) Gas Turbine Models for Compensation of Transient Fuel Flow Schedules. MSc(R) thesis, University of Glasgow.
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Abstract
In the present work, mathematical models have been devised to enable the prediction of the gas turbine engine performance during transient operations. The method used is based upon the engine component characteristics where an adequate information for a typical two-spool turbofan engine with mixed exhaust was available. Basically, this thesis deals with the effects of heat transfer on the engine performance and behaviour, especially during transient operations. Also methods of improving the engine response and performance are of great concern in this work. Therefore, the scope of this project lies on the following points:
Item Type: | Thesis (MSc(R)) |
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Qualification Level: | Masters |
Keywords: | Mechanical engineering |
Date of Award: | 1988 |
Depositing User: | Enlighten Team |
Unique ID: | glathesis:1988-76822 |
Copyright: | Copyright of this thesis is held by the author. |
Date Deposited: | 14 Jan 2020 09:34 |
Last Modified: | 14 Jan 2020 09:34 |
URI: | https://theses.gla.ac.uk/id/eprint/76822 |
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