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

thesis
posted on 27.03.2017, 14:58 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

Exports

Aeronautical and Automotive Engineering Theses

Exports