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Nonlinear combustion instability in liquid-propellant rocket engines. The transverse mode. I. The hydrodynamic differential and difference equations and computer algorithmHydrodynamic differential and difference equations and computer algorithm for nonlinear combustion instability in liquid propellant rocket engines, and Fortran IV listing
Document ID
19670027953
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Burstein, S. Z. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 3, 2013
Publication Date
September 15, 1967
Subject Category
Propulsion Systems
Report/Patent Number
NASA-CR-88763
JPL-TR-32-1111
Report Number: NASA-CR-88763
Report Number: JPL-TR-32-1111
Accession Number
67N37282
Funding Number(s)
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
ALGORITHM
FORTRAN
DIFFERENCE EQUATION
NONLINEARITY
DIFFERENTIAL EQUATION
COMBUSTION INSTABILITY
LIQUID PROPELLANT ROCKET ENGINE
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