This is the first major publication on liquid-rocket combustion devices since 1960, and includes 20 chapters prepared by world-renowned experts. Each chapter focuses on a specific aspect of liquid-propellant combustion and thrust chamber dynamics, and is incorporated into the volume in a well-organized, cohesive manner. There are contributions from nine different countriesChina, France, Germany, Italy, Japan, the Netherlands, Russia, Sweden, and the United States.
Inhaltsverzeichnis
Injection and Atomization; Propellant Injection Systems and Processes; Dynamics of Liquid Rocket Injectors; Atomization of Coaxial-Jet Injectors; Atomization of Impinging-Liquid Jets; Disintegration and Distortion of Liquid Streams; Combustion and Ignition; Modeling of Liquid-Propellant Combustion in Rocket Engine Combustor; Liquid-Propellant Droplet Vaporization and Combustion; Droplet Cluster Behavior in Dense and Dilute Regions of Sprays; Supercritical Combustion; CARS Measurements in Cryogenic LOX-GH2 Jet Flames; Propellant Ignition and Flame Propagation; Nozzle Concepts, Design, and Optimization; Rocket Engine Nozzle Concepts; Nozzle Design and Optimization; Thrust Chamber Dynamics, Heat Transfer, and Performance; Simulation and Analysis of Thruster Chamber Flowfields: Storable Propellant Rockets; Simulation and Analysis of Thrust Chamber Flowfields: Cryogenic-Propellant Rockets; Scaling Techniques in Liquid Rocket Engine Combustion Devices Testing; Thrust Chamber Cooling and Heat Transfer; Assessment of Thrust Chamber Performance; Aspects of Engine System Design; Thermodynamic Power Cycles for Pump-Fed Liquid Rocket Engines; Tripropellant Liquid Rocket Engine Technology; Oxidizer-Rich Preburner Technology for Oxygen/Hydrogen Full Flow Cycle Applications
