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Acoustic losses of a subscale, cold-flow rocket motor for various ''J'' valuesGeometric variables effect on acoustic attenuation in axial mode combustion instability in subscale rocket engine models
Document ID
19660010218
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Buffum, F. G. (Naval Ordnance Test Station China Lake, CA, United States)
Dehority, G. L. (Naval Ordnance Test Station China Lake, CA, United States)
Price, E. W. (Naval Ordnance Test Station China Lake, CA, United States)
Slates, R. O. (Naval Ordnance Test Station China Lake, CA, United States)
Date Acquired
August 3, 2013
Publication Date
February 1, 1966
Subject Category
Propulsion Systems
Report/Patent Number
NASA-CR-71086
NOTS-TP-3932
NAVWEPS-8971
Report Number: NASA-CR-71086
Report Number: NOTS-TP-3932
Report Number: NAVWEPS-8971
Accession Number
66N19507
Funding Number(s)
CONTRACT_GRANT: NASA ORDER WO-3034
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
ACOUSTIC ATTENUATION
GEOMETRIC FACTOR
ROCKET ENGINE
COMBUSTION INSTABILITY

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