Accession Number : AD0829888
Title : PARAMETRIC STUDY OF ROCKET INSTABILITY.
Descriptive Note : Final rept.,
Corporate Author : PURDUE UNIV LAFAYETTE IN SCHOOL OF MECHANICAL ENGINEERING
Personal Author(s) : Osborn, J. R. ; Netzer, D. W.
Report Date : 15 FEB 1968
Pagination or Media Count : 8
Abstract : The research program was concerned with (1) the problem of high frequency longitudinal pressure oscillations in premixed gaseous propellant combustors and (2) the steady-state and stability operating characteristics of bi-phase propellant rocket combustors operating at sub-critical conditions. Both analytical and experimental work were performed in order to study the aforementioned problems. (Author)
Descriptors : (*ROCKET ENGINES, COMBUSTION), COMBUSTION CHAMBERS, GASEOUS ROCKET PROPELLANTS, BIPROPELLANTS, STABILITY, OSCILLATION, PRESSURE, VAPORIZATION.
Subject Categories : Combustion and Ignition
Liquid Propellant Rocket Engines
Distribution Statement : APPROVED FOR PUBLIC RELEASE