Thesis
Numerical simulation of stagnation point transpiration cooling in non-equilibrium hypersonic flow
- Abstract:
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Hypersonic flight is an essential component of strategic defense and planetary exploration missions. Recent advances in physical understanding, material technology, and design practice have opened new possibilities both in defense and commercial applications and have led to a resurgence of interest in hypersonic technologies. Aerodynamic heating still presents the primary technical challenge in hypersonic flight. Traditionally, vehicles mitigate large heat loads with blunt leading edges and s...
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(Preview, Dissemination version, pdf, 7.0MB, Terms of use)
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Authors
Contributors
+ di Mare, L
- Institution:
- University of Oxford
- Division:
- MPLS
- Department:
- Engineering Science
- Role:
- Supervisor
- ORCID:
- 0000-0003-2551-2822
+ McGilvray, M
- Institution:
- University of Oxford
- Division:
- MPLS
- Department:
- Engineering Science
- Role:
- Supervisor
- ORCID:
- 0000-0001-9873-7737
+ Ireland, P
- Institution:
- University of Oxford
- Division:
- MPLS
- Department:
- Engineering Science
- Role:
- Examiner
+ Martin, A
- Institution:
- University of Kentucky
- Role:
- Examiner
+ Marshall Aid Commemoration Commission
More from this funder
- Funder identifier:
- https://ror.org/04q062s21
- Funding agency for:
- Brody, SD
- DOI:
- Type of award:
- DPhil
- Level of award:
- Doctoral
- Awarding institution:
- University of Oxford
- Language:
-
English
- Keywords:
- Subjects:
- Pubs id:
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2350331
- Local pid:
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pubs:2350331
- Deposit date:
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2025-11-22
- ARK identifier:
Terms of use
- Copyright holder:
- Samuel D. Brody
- Copyright date:
- 2025
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