Author: David M. Mann Publisher: ISBN: 9781423524434 Category : Languages : en Pages : 185
Book Description
Abstracts are given for 6.1 basic research in chemical propulsion sponsored by the Army Research Office and the Air Force Office of Scientific Research.
Author: Publisher: ISBN: Category : Languages : en Pages : 0
Book Description
Abstracts are given for research in chemical propulsion supported by the Air Force Office of Scientific Research and the Army Research Office.
Author: David M. Mann Publisher: ISBN: Category : Chemical reactions Languages : en Pages : 302
Book Description
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
Author: David M. Mann Publisher: ISBN: 9781423543039 Category : Languages : en Pages : 111
Book Description
Abstracts are given for 6.1 basic research in chemical propulsion supported by the Army Research Office and the Air Force Office of Scientific Research.
Author: Publisher: ISBN: Category : Languages : en Pages : 0
Book Description
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.
Author: David M. Mann Publisher: ISBN: Category : Science Languages : en Pages : 186
Book Description
Abstracts are given for 6.1 basic research in chemical propulsion sponsored by the Army Research Office and the Air Force Office of Scientific Research.
Author: Publisher: ISBN: Category : Languages : en Pages : 298
Book Description
Abstracts are given for research in airbreathing combustion, rocket propulsion, and diagnostics in reacting media supported by the Air Force Office of Scientific Research. Instability, Flames, Propulsion, Gas Turbines Combustion, Shear Layer, Supersonic, Soot, Sprays, Lasers, Fluorescence, Spectroscopy, Rocket, Plasma, Scramjets.
Author: M. A. Birkan Publisher: ISBN: Category : Languages : en Pages : 315
Book Description
There is a strong need to improve our fundamental understanding of electrothermal arcjets with the ultimate goal of increasing both efficiency and specific impulse. A research effort using emission spectroscopy, two-color pyrometry and analytical modeling is being developed to better understand and minimize the major energy loss mechanisms in arcjet thrusters, for example; anode heat losses, viscous losses and frozen flow losses. Research in these areas will assist in optimizing the overall design configuration and thermal characteristics of arcjet propulsion devices. Keywords: Instability, Flames, Propulsion, Gas turbines, Combustions, Shear layer, Supersonic, Soot, Sprays, Boron, Lasers, Fluorescence, Rocket, Scramjet, Nitramines, Turbulence. (JES).
Author: David M. Mann
Author: 
Author: David M. Mann
Author: David M. Mann
Author: 
Author: INSTITUTO NACIONAL DE TECNICA AEROESPACIAL MADRID (Spain)
Author: David M. Mann
Author: Armour Research Foundation (U.S.)
Author: 
Author: M. A. Birkan