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

thesis
posted on 27.03.2017 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

© 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

This Thesis is restricted until 01/07/2021. A Doctoral Thesis. Submitted in partial fulfilment of the requirements for the award of Doctor of Philosophy of Loughborough University.

Language

en

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