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Shock Tunnel Studies of Scramjet Phenomena 1994Reports by the research staff and graduate students of the Mechanical Engineering Department at the University of Queensland are collected and presented. These reports cover various studies related to the advancement of scramjet technology and the operation of advanced hypervelocity shock-expansion tubes. The report topics include the experimental studies of mixing and combustion in a scramjet flow path, the measurement of integrated thrust and skin friction, and the development of a free-piston-driven expansion tunnel capable of delivering a test gas at superorbital velocities.
Document ID
19970022388
Acquisition Source
Headquarters
Document Type
Contractor Report (CR)
Authors
Morgan, R. G.
(Queensland Univ. Brisbane, Australia)
Paull, A.
(Queensland Univ. Brisbane, Australia)
Stalker, R. J.
(Queensland Univ. Brisbane, Australia)
Date Acquired
September 6, 2013
Publication Date
April 1, 1997
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NAS 1.26:201693
NASA-CR-201693
Report Number: NAS 1.26:201693
Report Number: NASA-CR-201693
Accession Number
97N22936
Funding Number(s)
CONTRACT_GRANT: NAGw-674
PROJECT: RTOP 522-51-31-10
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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