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Thesis

Transpiration cooling of a hypersonic vehicle

Abstract:

In this thesis, a porous Ultra-High-Temperature-Ceramic (UHTC) made of zirconium diboride (ZrB2) is qualified for the purpose for transpiration cooling for the first time. Subsequently, the mixing mechanism between the coolant and a laminar, hypersonic boundary-layer gas at the wall downstream of a transpiration-cooled injector is investigated. This has led to understanding the mixing process at the wall in a laminar boundary layer.

Porous UHTCs are a candidate group of materials f...

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Division:
MPLS
Department:
Engineering Science
Research group:
Oxford Thermofluids Laboratory
Oxford college:
Wolfson College
Role:
Author
ORCID:
0000-0002-8398-8987

Contributors

Institution:
University of Oxford
Division:
MPLS
Department:
Engineering Science
Research group:
Oxford Thermofluids Laboratory
Oxford college:
St Hilda's College
Role:
Supervisor
Institution:
University of Oxford
Division:
MPLS
Department:
Engineering Science
Research group:
Oxford Thermofluids Laboratory
Oxford college:
St Hilda's College
Role:
Supervisor
Institution:
University of Oxford
Division:
MPLS
Department:
Engineering Science
Research group:
Oxford Thermofluids Laboratory
Role:
Examiner
Institution:
University of Queensland
Research group:
Centre for Hypersonics
Role:
Examiner


More from this funder
Funder identifier:
http://dx.doi.org/10.13039/501100000266
Funding agency for:
McGilvray, M
Grant:
EP/P000878/1
Programme:
Transpiration Cooling Systems for Jet Engine Turbines and Hypersonic Flight


DOI:
Type of award:
DPhil
Level of award:
Doctoral
Awarding institution:
University of Oxford

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