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Hypersonic propulsionThe paper reviews the whys and hows of the concept of supersonic combustion for hypersonic propulsion. Attention is given to the problem areas, the current research and development efforts, and their implications. The operating boundary of the SCRAMJET is reasonably well defined. The paper also explores some air-breathing alternatives that may go beyond SCRAMJETS.
Document ID
19900034894
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Cheng, SIN-I.
(Princeton University NJ, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1989
Publication Information
Publication: Progress in Energy and Combustion Science
Volume: 15
Issue: 3 19
ISSN: 0360-1285
Subject Category
Aircraft Propulsion And Power
Accession Number
90A21949
Funding Number(s)
CONTRACT_GRANT: NAS1-17234
Distribution Limits
Public
Copyright
Other

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