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On the development of mach waves radiated by small disturbances.Relevance of Mach wave field to practical rocket flow noise problems
Document ID
19650042163
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Williams, J. E. F.
Date Acquired
August 2, 2013
Publication Date
May 1, 1965
Subject Category
Fluid Mechanics
Accession Number
65A24867
Distribution Limits
Public
Copyright
Other
Keywords
ROCKET EXHAUST
SHOCK WAVE
AERODYNAMIC NOISE
SUPERSONIC FLOW
TURBULENT FLOW

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