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A Theoretical Study of Nonlinear Transverse Combustion Instability in Liquid Propellant Rocket MotorsNonsteady flow conditions in subsonic section of Laval nozzle to investigate nonlinear transverse combustion instability in liquid propellant rocket motors
Document ID
19660020175
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Zinn, B. T. (Princeton Univ. NJ, United States)
Date Acquired
August 3, 2013
Publication Date
May 1, 1966
Subject Category
Thermodynamics And Combustion
Report/Patent Number
NASA-CR-75894
Report Number: NASA-CR-75894
Accession Number
66N29465
Funding Number(s)
CONTRACT_GRANT: NASR-217
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
COMBUSTION INSTABILITY
LIQUID PROPELLANT ROCKET ENGINE
SUBSONIC FLOW

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