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Multiple-orifice liquid injection into hypersonic air streams.Review of oblique water and fluorocarbon injection test results obtained in experimental studies of the effects of multiple-orifice liquid injection into hypersonic air streams. The results include the finding that maximum lateral penetration from such injections increases linearly with the square root of the jet-to-freestream dynamic-pressure ratio and is proportional to an equivalent orifice diameter.
Document ID
19730035174
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Weaver, W. L.
(NASA Langley Research Center Space Technology Div., Hampton, Va., United States)
Date Acquired
August 7, 2013
Publication Date
December 1, 1972
Publication Information
Publication: AIAA Journal
Volume: 10
Subject Category
Aerodynamics
Accession Number
73A19976
Distribution Limits
Public
Copyright
Other

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