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Shock Tunnel Studies of Scramjet Phenomena 1995Reports 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 delivering a test gas at super orbital velocities.
Document ID
19970022216
Acquisition Source
Headquarters
Document Type
Contractor Report (CR)
Authors
Morgan, R. G. (Queensland Univ. Brisbane, Australia)
Stalker, R. J. (Queensland Univ. Brisbane, Australia)
Paull, A. (Queensland Univ. Brisbane, Australia)
Date Acquired
September 6, 2013
Publication Date
April 1, 1997
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-CR-201694
NAS 1.26:201694
Accession Number
97N22795
Funding Number(s)
PROJECT: RTOP 522-51-31-10
CONTRACT_GRANT: NAGw-674
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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