Conference item
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
- 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
- Language:
-
English
- Keywords:
-
- Pubs id:
-
2090811
- Local pid:
-
pubs:2090811
- Deposit date:
-
2025-09-18
- ARK identifier:
Terms of use
- Copyright holder:
- Ceruzzi et al
- Copyright date:
- 2025
- Rights statement:
- © 2025 by Andrew P. Ceruzzi , Laurent M. Le Page, Liam P. McQuellin, Wesley Condren, and Matthew McGilvray. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission.
- Notes:
- This paper was presented at the AIAA SCITECH 2025 Forum, 6th-10th January 2025, Orlando, FL, USA.
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