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ATTENUATION OF TANGENTIAL-PRESSURE OSCILLATIONS IN A LIQUID-OXYGEN -N-HEPTANE ROCKET ENGINE WITH LONGITUDINAL FINSAttenuation of tangent-pressure oscillation in liquid-oxygen-heptane rocket engine combustion chamber using longitudinal fin
Document ID
19630004885
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
Priem, R. J. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 1, 2013
Publication Date
June 28, 1956
Subject Category
Propellants
Report/Patent Number
NACA-RM-E56C09
Report Number: NACA-RM-E56C09
Accession Number
63N14761
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
LIQUID OXYGEN /LOX/
PRESSURE OSCILLATION
COMBUSTION CHAMBER
FIN
LIQUID PROPELLANT ROCKET ENGINE
HEPTANE

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