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Observations of boundary layer transition reversal on a blunt cone in hypersonic flow

Abstract:
The boundary layer transition on a 7-degree half-angle cone at zero angle of attack, with varying bluntness, is investigated experimentally in the High Density Tunnel (HDT) at the University of Oxford. The experiments are carried out in a cold Mach 6 flow, where surface heat f lux profiles are measured using infrared (IR) thermography, and the boundary and entropy layers are studied using high-speed schlieren imaging at 500 kHz. The onset of transition, XST, is identified as the location where the measured heat flux exceeds the laminar predictions based on Lees (1956). The bluntness Reynolds number, ReRN, defined using freestream conditions and the nose radius, is varied over the range 3 × 104 to 1.5 × 106. The transition Reynolds number, ReXST, increases with ReRN up to approximately 6 × 105. Beyond this value, the transition location exhibits greater scatter and a reversal trend with increasing bluntness, consistent with earlier findings by Stetson (1983) and Marineau (2014). The surface roughness profile of the nose tip is characterized, and schlieren images of the boundary and entropy layers are presented.
Publication status:
Published
Peer review status:
Peer reviewed

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Publisher copy:
10.2514/6.2025-0921

Authors

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Institution:
University of Oxford
Division:
MPLS
Department:
Engineering Science
Role:
Author
More by this author
Institution:
University of Oxford
Division:
MPLS
Department:
Engineering Science
Role:
Author
More by this author
Institution:
University of Oxford
Division:
MPLS
Department:
Engineering Science
Oxford college:
Wolfson College
Role:
Author
ORCID:
0000-0003-4322-711X
More by this author
Institution:
University of Oxford
Division:
MPLS
Department:
Engineering Science
Role:
Author
More by this author
Institution:
University of Oxford
Division:
MPLS
Department:
Engineering Science
Role:
Author
ORCID:
0000-0001-9873-7737


Publisher:
American Institute of Aeronautics and Astronautics
Host title:
AIAA SCITECH 2025 Forum
Article number:
AIAA 2025-0921
Publication date:
2025-01-03
Event title:
AIAA SCITECH 2025 Forum
Event location:
Orlando, FL, USA
Event website:
https://aiaa.org/scitech/
Event start date:
2025-01-06
Event end date:
2025-01-10
DOI:
EISBN:
9781624107238

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