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Commissioning of the Oxford High Density Tunnel (HDT) for boundary layer stability measurements at Mach 7

Abstract:

Experiments have been completed in the University of Oxford’s High Density Tunnel (HDT) to verify that it can be used for boundary layer stability measurements. These have replicated the research previously undertaken in the DLR H2K facility in 2013 using a sub-scale model of the HIFiRE-1 flight. This was a 7-degree half-angle axisymmetric cone with small nose bluntness. For the tests, the facility was operated in Ludwieg Tube mode with a contoured Mach 7 nozzle at a range of unit Reynolds nu...

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Publication status:
Published
Peer review status:
Peer reviewed

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Publisher copy:
10.2514/6.2018-3074

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Institution:
University of Oxford
Division:
MPLS Division
Department:
Engineering Science
Role:
Author
More by this author
Institution:
University of Oxford
Division:
MPLS Division
Department:
Engineering Science
Role:
Author
More by this author
Institution:
University of Oxford
Division:
MPLS
Department:
Engineering Science
Role:
Author
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Name:
European Office Aerospace Research and Development
Publisher:
American Institute of Aeronautics and Astronautics
Host title:
2018 Fluid Dynamics Conference, AIAA AVIATION Forum, (AIAA 2018-3074)
Journal:
2018 Fluid Dynamics Conference More from this journal
Publication date:
2018-06-25
DOI:
ISBN:
9781624105531
Pubs id:
pubs:908379
UUID:
uuid:e7135b5c-d993-4494-8eea-10c36f4791da
Local pid:
pubs:908379
Source identifiers:
908379
Deposit date:
2018-11-26

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