Scramjet propulsion
Author(s)
Bibliographic Information
Scramjet propulsion
(Progress in astronautics and aeronautics, v. 189)
American Institute of Aeronautics and Astronautics, c2000
Available at 14 libraries
  Aomori
  Iwate
  Miyagi
  Akita
  Yamagata
  Fukushima
  Ibaraki
  Tochigi
  Gunma
  Saitama
  Chiba
  Tokyo
  Kanagawa
  Niigata
  Toyama
  Ishikawa
  Fukui
  Yamanashi
  Nagano
  Gifu
  Shizuoka
  Aichi
  Mie
  Shiga
  Kyoto
  Osaka
  Hyogo
  Nara
  Wakayama
  Tottori
  Shimane
  Okayama
  Hiroshima
  Yamaguchi
  Tokushima
  Kagawa
  Ehime
  Kochi
  Fukuoka
  Saga
  Nagasaki
  Kumamoto
  Oita
  Miyazaki
  Kagoshima
  Okinawa
  Korea
  China
  Thailand
  United Kingdom
  Germany
  Switzerland
  France
  Belgium
  Netherlands
  Sweden
  Norway
  United States of America
Description and Table of Contents
Description
Supersonic combustion ramjet (SCRJ) engine research and development begun some 40 years ago is the key to airbreathing hypersonic flight. Many unexpected complexities of SCRJ engine combustion and combustor-inlet interaction have been continuing challenges. However, valuable progress has been made in several aspects. In the next few years, it would appear that significant flight testing will take place in several countries and this should lead to further understanding of SCRJ processes in engine design for cruise and accelerator vehicle applications. This volume - the third and final in a mini-series on hypersonic propulsion along with High Speed Flight Propulsion Systems, volume 137, and Developments in High Speed Flight Propulsion Systems, volume 165 - presents a comprehensive and detailed exposition of the gradual maturing of scramjet technologies. Developments in several parts of the world are described by those intimately involved in the main stream of SCRJ activities. It is clear that fresh opportunities exist to improve the robustness of high-speed-fight propulsion, and this book offers a timely lead to a new entrant to this technology as well as new insights to specialists.
Table of Contents
- Supersonic Flow Combustors
- Scramjet-Airframe Integration
- The Strutjet Engine
- Dual-Mode SCRJ Flowpath Analysis
- Hydrocarbon Fuels
- SCRJ Inlets
- Combustion-Inlet Interactions
- SCRJ Combustor-Nozzle Performance
- SCRM Developments in France
- SCRM Developments in Russia
- Electro-Magnetic Field Interactions and Scramjet Propulsion
- Detonation Wave Ramjets
- Forces and Moments Associated with Hypersonic Vehicle Design Research on Scram Combustors in Australia
- System Sizing
- Energy Effectiveness of Scram Combustors.
by "Nielsen BookData"