Fr. 177.60

Liquid Rocket Thrust Chambers - Aspects of Modeling, Analysis, and Design

English · Hardback

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Description

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List 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

Summary

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.

Product details

Assisted by Mohammed Habiballah (Editor), James Hulka (Editor), Michael Popp (Editor), Vigor Yang (Editor)
Publisher Scitech Publishing
 
Languages English
Product format Hardback
Released 01.02.2003
 
EAN 9781563472237
ISBN 978-1-56347-223-7
No. of pages 725
Dimensions 155 mm x 247 mm x 44 mm
Weight 1104 g
Series Progress in Astronautics and A
Subject Natural sciences, medicine, IT, technology > Technology > Aviation and space engineering

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