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
-
No Libraries matched.
- Remove all filters.
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
by "Nielsen BookData"