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Dynamic response of a supersonic diffuser to bypass and spike oscillationInvestigation of amplitude and phase shift of static pressure variations in supersonic diffuser for separate oscillation of spike and bypass
Document ID
19650003083
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Bowditch, D. N. (NASA Lewis Research Center Cleveland, OH, United States)
Wilcox, F. A. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1959
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-10
Report Number: NASA-TM-X-10
Accession Number
65N12684
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
PHASE SHIFT
SUPERSONIC DIFFUSER
STATIC PRESSURE

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