Liquid rocket thrust chambers : aspects of modeling, analysis, and design
著者
書誌事項
Liquid rocket thrust chambers : aspects of modeling, analysis, and design
(Progress in astronautics and aeronautics, v. 200)
American Institute of Aeronautics and Astronautics, c2004
大学図書館所蔵 全13件
  青森
  岩手
  宮城
  秋田
  山形
  福島
  茨城
  栃木
  群馬
  埼玉
  千葉
  東京
  神奈川
  新潟
  富山
  石川
  福井
  山梨
  長野
  岐阜
  静岡
  愛知
  三重
  滋賀
  京都
  大阪
  兵庫
  奈良
  和歌山
  鳥取
  島根
  岡山
  広島
  山口
  徳島
  香川
  愛媛
  高知
  福岡
  佐賀
  長崎
  熊本
  大分
  宮崎
  鹿児島
  沖縄
  韓国
  中国
  タイ
  イギリス
  ドイツ
  スイス
  フランス
  ベルギー
  オランダ
  スウェーデン
  ノルウェー
  アメリカ
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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