Accession Number : AD0645634
Title : COMBUSTION INSTABILITY IN LIQUID PROPELLANT ROCKET ENGINES.
Descriptive Note : Final rept.,
Corporate Author : POLYTECHNIC INST OF BROOKLYN N Y DEPT OF AEROSPACE ENGINEERING AND APPLIED MECHANICS
Personal Author(s) : Agosta,Vito D. ; Hammer,Sanford S.
Report Date : OCT 1966
Pagination or Media Count : 22
Abstract : The investigation is concerned with the development of a theoretical model for combustion instability, in the longitudinal mode, occurring in liquid propellant rocket engines that are employed in current practice. Experimental results are used both to help generate realistic physical models for combustion-wave phenomena in heterogeneously reacting systems, and for subsequent verification of theoretical results. (Author)
Descriptors : (*LIQUID PROPELLANT ROCKET ENGINES, COMBUSTION), (*COMBUSTION, STABILITY), MATHEMATICAL MODELS, DROPS, EVAPORATION, BIPROPELLANTS, OSCILLATION
Subject Categories : Combustion and Ignition
Liquid Propellant Rocket Engines
Distribution Statement : APPROVED FOR PUBLIC RELEASE