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Detonation control for propulsion = ...

Li, Jiun-Ming.

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Detonation control for propulsion = pulse detonation and rotating detonation engines /

紀錄類型:	書目-電子資源 : Monograph/item
正題名/作者:	Detonation control for propulsion/ edited by Jiun-Ming Li ... [et al.].
其他題名:	pulse detonation and rotating detonation engines /
其他作者:	Li, Jiun-Ming.
出版者:	Cham :Springer International Publishing : : 2018.,
面頁冊數:	xiii, 239 p. :ill., digital ;24 cm.
內容註:	1. Performance of Rotating Detonation Engines for Air Breathing Applications -- 2. Development of Gasturbine with Detonation Chamber -- 3. Flow Structure in Rotating Detonation Engine with Separate Supply of Fuel and Oxidizer: Experiment and CFD -- 4. Application of Detonation Waves to Rocket Engine Chamber -- 5. Numerical Simulation on Rotating Detonation Engine: Effects of Higher-Order Scheme -- 6. Review on the Research Progresses in Rotating Detonation Engine -- 7. Continuous Detonation Engine Researches at Peking University -- 8. Pulse Detonation Cycle at Kilohertz Frequency -- 9. On the Investigation of Detonation Re-initiation Mechanisms and the Influences of the Geometry Confinements and Mixture Properties.
Contained By:	Springer eBooks
標題:	Rocket engines - Control systems. -
電子資源:	http://dx.doi.org/10.1007/978-3-319-68906-7
ISBN:	9783319689067

Detonation control for propulsion = pulse detonation and rotating detonation engines /
Detonation control for propulsionpulse detonation and rotating detonation engines /[electronic resource] :edited by Jiun-Ming Li ... [et al.]. - Cham :Springer International Publishing :2018. - xiii, 239 p. :ill., digital ;24 cm. - Shock wave and high pressure phenomena,2197-9529. - Shock wave and high pressure phenomena..

1. Performance of Rotating Detonation Engines for Air Breathing Applications -- 2. Development of Gasturbine with Detonation Chamber -- 3. Flow Structure in Rotating Detonation Engine with Separate Supply of Fuel and Oxidizer: Experiment and CFD -- 4. Application of Detonation Waves to Rocket Engine Chamber -- 5. Numerical Simulation on Rotating Detonation Engine: Effects of Higher-Order Scheme -- 6. Review on the Research Progresses in Rotating Detonation Engine -- 7. Continuous Detonation Engine Researches at Peking University -- 8. Pulse Detonation Cycle at Kilohertz Frequency -- 9. On the Investigation of Detonation Re-initiation Mechanisms and the Influences of the Geometry Confinements and Mixture Properties.

This book focuses on the latest developments in detonation engines for aerospace propulsion, with a focus on the rotating detonation engine (RDE) State-of-the-art research contributions are collected from international leading researchers devoted to the pursuit of controllable detonations for practical detonation propulsion. A system-level design of novel detonation engines, performance analysis, and advanced experimental and numerical methods are covered. In addition, the world's first successful sled demonstration of a rocket rotating detonation engine system and innovations in the development of a kilohertz pulse detonation engine (PDE) system are reported. Readers will obtain, in a straightforward manner, an understanding of the RDE & PDE design, operation and testing approaches, and further specific integration schemes for diverse applications such as rockets for space propulsion and turbojet/ramjet engines for air-breathing propulsion. Detonation Control for Propulsion: Pulse Detonation and Rotating Detonation Engines provides, with its comprehensive coverage from fundamental detonation science to practical research engineering techniques, a wealth of information for scientists in the field of combustion and propulsion. The volume can also serve as a reference text for faculty and graduate students and interested in shock waves, combustion and propulsion.

ISBN: 9783319689067

Standard No.: 10.1007/978-3-319-68906-7doiSubjects--Topical Terms:

3299714
Rocket engines
--Control systems.

LC Class. No.: TL782

Dewey Class. No.: 629.134354

Detonation control for propulsion = pulse detonation and rotating detonation engines /
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505 0 $a 1. Performance of Rotating Detonation Engines for Air Breathing Applications -- 2. Development of Gasturbine with Detonation Chamber -- 3. Flow Structure in Rotating Detonation Engine with Separate Supply of Fuel and Oxidizer: Experiment and CFD -- 4. Application of Detonation Waves to Rocket Engine Chamber -- 5. Numerical Simulation on Rotating Detonation Engine: Effects of Higher-Order Scheme -- 6. Review on the Research Progresses in Rotating Detonation Engine -- 7. Continuous Detonation Engine Researches at Peking University -- 8. Pulse Detonation Cycle at Kilohertz Frequency -- 9. On the Investigation of Detonation Re-initiation Mechanisms and the Influences of the Geometry Confinements and Mixture Properties.
520 $a This book focuses on the latest developments in detonation engines for aerospace propulsion, with a focus on the rotating detonation engine (RDE) State-of-the-art research contributions are collected from international leading researchers devoted to the pursuit of controllable detonations for practical detonation propulsion. A system-level design of novel detonation engines, performance analysis, and advanced experimental and numerical methods are covered. In addition, the world's first successful sled demonstration of a rocket rotating detonation engine system and innovations in the development of a kilohertz pulse detonation engine (PDE) system are reported. Readers will obtain, in a straightforward manner, an understanding of the RDE & PDE design, operation and testing approaches, and further specific integration schemes for diverse applications such as rockets for space propulsion and turbojet/ramjet engines for air-breathing propulsion. Detonation Control for Propulsion: Pulse Detonation and Rotating Detonation Engines provides, with its comprehensive coverage from fundamental detonation science to practical research engineering techniques, a wealth of information for scientists in the field of combustion and propulsion. The volume can also serve as a reference text for faculty and graduate students and interested in shock waves, combustion and propulsion.
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