"Liquid Rocket Thrust Chambers: Aspects of Modeling, Analysis, and Design" ed. by Vigor Yang, Mohammed Habiballah, James Hulka, Michael Popp
American Institute of Aeronautics and Astronautics. Progress in Astronautics and Aeronautics, Vol. 200
AIAA | 2004 | ISBN: 1563472236 9781563472237 | 778 pages | PDF | 9 MB
American Institute of Aeronautics and Astronautics. Progress in Astronautics and Aeronautics, Vol. 200
AIAA | 2004 | ISBN: 1563472236 9781563472237 | 778 pages | PDF | 9 MB
This issue focuses on a specific aspect of liquid-propellant combustion and thrust chamber dynamics. The volume compiles results from many of the research and development programs conducted over the last several decades across the international community.
Contents
Preface
1 Propellant Injection Systems and Processes
2 Design and Dynamics of Jet and Swirl Injectors
3 Atomization in CoaxiaUet Injectors
4 Liquid Bipropellant Injectors
5 Distortion and Disintegration of Liquid Streams
6 Modeling Liquid-Propellant Spray Combustion Processes
7 Liquid-Propellant Droplet Vaporization and Combustion
8 Subcritical/Supercritical Droplet Cluster Behavior in Dense and Dilute Regions of Sprays
9 Fundamentals of Supercritical Mixing and Combustion of Cryogenic Propellants
10 CARS Measurements at High Pressure in Cryogenic LOX/GH2 Jet Flames
11 Propellant Ignition and Flame Propagation
12 Rocket Engine Nozzle Concepts
13 Nozzle Design and Optimization
14 Simulation and Analysis of Thrust Chamber Flowfields: Storable Propellant Rockets
15 Simulation and Analysis of Thrust Chamber Flowfields: Cryogenic Propellant Rockets
16 Scaling Techniques for Design, Development, and Test
17 Assessment of Thrust Chamber Performance
18 Thermodynamic Power Cycles for Pump-Fed Liquid Rocket Engines
19 Tripropellant Engine Technology for Reusable Launch Vehicles
20 Oxidizer-Rich Preburner Technology for Oxygen/Hydrogen Full Flow Cycle Applications
SUBJECT INDEX
AUTHOR INDEX
with TOC BookMarkLinks