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Effect of fan root flow on the low-pressure compressor transition duct for an ultra high bypass ratio turbofan engine

thesis
posted on 2023-04-18, 14:37 authored by Dimitra Tsakmakidou

Effect of fan root flow on the low-pressure compressor transition duct for an ultra high bypass ratio turbofan engine

Funding

Integrated Core Technologies (iCORE)

Innovate UK

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Loughborough University and Rolls-Royce plc

Innovate UK

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History

School

  • Aeronautical, Automotive, Chemical and Materials Engineering

Department

  • Aeronautical and Automotive Engineering

Publisher

Loughborough University

Rights holder

© Dimitra Tsakmakidou

Publication date

2023

Notes

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

Language

  • en

Supervisor(s)

A Duncan Walker ; Jon Carrotte

Qualification name

  • PhD

Qualification level

  • Doctoral

This submission includes a signed certificate in addition to the thesis file(s)

  • I have submitted a signed certificate