Liquid rocket thrust chambers : aspects of modeling, analysis, and design

書誌事項

Liquid rocket thrust chambers : aspects of modeling, analysis, and design

edited by Vigor Yang ...[et al.]

(Progress in astronautics and aeronautics, v. 200)

American Institute of Aeronautics and Astronautics, c2004

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内容説明・目次

内容説明

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.

目次

  • 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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詳細情報

  • NII書誌ID(NCID)
    BA71239494
  • ISBN
    • 1563472236
  • 出版国コード
    us
  • タイトル言語コード
    eng
  • 本文言語コード
    eng
  • 出版地
    Reston, Va
  • ページ数/冊数
    xx, 725 p.
  • 大きさ
    24 cm
  • 分類
  • 件名
  • 親書誌ID
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