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LAPCAT II intake starting tests

Abstract:

As part of the EU LAPCAT II programme, the University of Oxford tested and analysed a 1:100 scale Scramjet intake for starting capabilities. Tests were performed at a Mach 7 condition in the Oxford Gun Tunnel, with a unit Reynolds number of 20x106/m. The model was instrumented with 61 measurements of wall static pressure throughout the intake and isolator, 24 thin film heat transfer gauges on the end of the intake and start of the isolator and video Schlieren of the cowl closure region of the...

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Publication status:
Published
Peer review status:
Peer reviewed

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Institution:
University of Oxford
Division:
MPLS
Department:
Engineering Science
Role:
Author
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Institution:
University of Oxford
Division:
MPLS Division
Department:
Department of Engineering Science
Role:
Author
Publisher:
European Space Agency
Host title:
8th European Symposium on Aerothermodynamics for Space Vehicles
Journal:
8th European Symposium on Aerothermodynamics for Space Vehicles More from this journal
Publication date:
2015-05-04
Acceptance date:
2015-05-04
Keywords:
Pubs id:
pubs:946512
UUID:
uuid:8c573436-ddcd-4c13-becf-1b1f7b95aee7
Local pid:
pubs:946512
Source identifiers:
946512
Deposit date:
2018-11-26

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