Accession Number : ADA315528
Title : Modeling of Liquid Jet Atomization Processes.
Descriptive Note : Final technical rept. 1 Jul 94-30 Jun 96,
Corporate Author : PURDUE UNIV LAFAYETTE IN SCHOOL OF AERONAUTICS AND ASTRONAUTICS
Personal Author(s) : Heister, Stephen D.
PDF Url : ADA315528
Report Date : 01 AUG 1996
Pagination or Media Count : 99
Abstract : This report summarizes atomization simulations performed to investigate the role of this process in liquid rocket engine combustion instabilities. The research involves the development and application of a series of nonlinear free surface models based on boundary element methods (B EMs). Models have been developed to study the effects of unsteady injection, transverse acoustic wave interactions (such as those experienced in the F-1 engine), longitudinal acoustic wave interactions, and the dynamics of droplets in the presence of an acoustic wave. Results for each of these four models is presented in this document.
Descriptors : *MATHEMATICAL MODELS, *COMBUSTION, *LIQUID JETS, *ATOMIZATION, SIMULATION, INTERACTIONS, DYNAMICS, ACOUSTIC WAVES, SURFACES, BOUNDARIES, NONLINEAR SYSTEMS, DROPS, LIQUID PROPELLANT ROCKET ENGINES, TRANSVERSE WAVES, INJECTORS, INSTABILITY.
Subject Categories : Operations Research
Combustion and Ignition
Solid Propellant Rocket Engines
Distribution Statement : APPROVED FOR PUBLIC RELEASE