Liquid rocket thrust chambers : aspects of modeling, analysis, and design
Author(s)
Bibliographic Information
Liquid rocket thrust chambers : aspects of modeling, analysis, and design
（Progress in astronautics and aeronautics, v. 200）
American Institute of Aeronautics and Astronautics, c2004
Available at 13 libraries
Description and Table of Contents
Description
This is the first major publication on liquid-rocket combustion devices since 1960. A total of 26 chapters prepared by world-renowned experts in their subject areas are included. 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 countries - China, France, Germany, Italy, Japan, The Netherlands, Russia, Sweden, and the United States.
Table of Contents
- 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
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