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The unsteady fuel flow response of liquid fuelled gas turbine injector to applied fluctuation

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posted on 2021-07-08, 07:55 authored by Ran Mo
The unsteady fuel flow response of liquid fuelled gas turbine injector to applied fluctuation

Funding

Rolls-Royce

EPSRC

History

School

  • Aeronautical, Automotive, Chemical and Materials Engineering

Department

  • Aeronautical and Automotive Engineering

Publisher

Loughborough University

Rights holder

© Ran Mo

Publisher statement

This work is made available according to the conditions of the Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International (CC BY-NC-ND 4.0) licence. Full details of this licence are available at: https://creativecommons.org/licenses/by-nc-nd/4.0/

Publication date

2017

Notes

A Doctoral Thesis. Submitted in partial fulfilment of the requirements for the award of Doctor of Philosophy of Loughborough University.

Language

  • en

Supervisor(s)

Jon Carrotte

Qualification name

  • PhD

Qualification level

  • Doctoral

Administrator link

Usage metrics

    Aeronautical and Automotive Engineering Theses

    Categories

    Keywords

    Gas turbinesStabilityFuelEngineering not elsewhere classified

    Licence

    CC BY-NC-ND 4.0

    Exports

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