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Integrated design of compressor transition ducts with swirling flow and aerodynamic lifting struts

thesis
posted on 29.05.2019, 15:21 by Ian MariahIan Mariah
Integrated design of compressor transition ducts with swirling flow and aerodynamic lifting struts

Funding

European Union Seventh Framework Program under grant agreement n° 283216, LEMCOTEC (Low Emission Core Engine Technologies)

History

References

School

Aeronautical, Automotive, Chemical and Materials Engineering

Department

Aeronautical and Automotive Engineering

Publisher

Loughborough University

Rights holder

© I.L. Mariah

Publication date

2018

Notes

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

Language

en

Supervisor(s)

A.D. Walker ; J.F. 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

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Aeronautical and Automotive Engineering ThesesAeronautical and Automotive Engineering Theses

Categories

Keywords

s-ductstrutintercompressorductintegrationaerodynamic

Licence

CC BY-NC-ND 4.0

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