Accession Number : ADA311354
Title : ARO and AFOSR Contractors Meeting in Chemical Propulsion, Held in Virginia Beach, Virginia on 3-6 June 1996.
Descriptive Note : Technical rept. 1 Jun 95-31 May 96,
Corporate Author : AIR FORCE OFFICE OF SCIENTIFIC RESEARCH BOLLING AFB DC
Personal Author(s) : Mann, David M. ; Birkan, Mitat A. ; Tishkoff, Julian M.
PDF Url : ADA311354
Report Date : 20 JUN 1996
Pagination or Media Count : 299
Abstract : Partial contents: Supercritical droplet behavior; Fundamentals of acoustic instabilities in liquid-propellant rockets; Modeling liquid jet atomization proceses; Liquid-propellant droplets dynamics and combustions in supercritical forced convective environments; Contributions of shear coaxial injectors to liquid rocket motor combustion instabilities; High pressure combustion studies under combustion driven oscillatory flow conditions; Droplet collision on liquid propellant combustion; Combustion and plumes; Development of a collisional radiative emission model for strongly nonequilibrium flows; Energy transfer processes in the production of excited states in reacting rocket flows; modeling nonequilibrium radiation in high altitude plumes; kinetics of plume radiation, and of HEDMs and metallic fuels combustion; Nonsteady combustion mechanisms of advanced solid propellants; Chemical mechanisms at the burning surface. p15
Descriptors : *PROPULSION SYSTEMS, *CHEMICAL REACTIONS, SHEAR PROPERTIES, EMISSION, METALS, DENSITY, RADIATION, SOOT, SYMPOSIA, COMPUTATIONS, ENVIRONMENTS, FLUORESCENCE, MODELS, CHEMICALS, INTERFACES, CONVECTION, PARALLEL PROCESSING, HIGH PRESSURE, ENERGY TRANSFER, NUCLEATION, JET ENGINES, PHASE, SURFACES, COMBUSTION, FUELS, RAMJET ENGINES, COAXIAL CONFIGURATIONS, HOLOGRAPHY, NONLINEAR SYSTEMS, HYDROCARBONS, DROPS, LIQUID PROPELLANT ROCKET ENGINES, ACOUSTICS, LIQUID PROPELLANTS, SUPERCRITICAL FLOW, IGNITION, DIFFUSION, FLOW, KINETICS, NONEQUILIBRIUM FLOW, PLUMES, FLAMES, UNSTEADY FLOW, BURNING RATE, INJECTORS, ROTATION, SUPERSONIC COMBUSTION RAMJET ENGINES, INSTABILITY, DIESEL FUELS, SOLID PROPELLANT ROCKET ENGINES, ROCKETS, COLLISIONS, LIQUID JETS, IONIC CURRENT, SOLID PROPELLANTS, FUEL INJECTION, ATOMIZATION.
Subject Categories : Jet and Gas Turbine Engines
Combustion and Ignition
Distribution Statement : APPROVED FOR PUBLIC RELEASE