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Titlebook: Detonation Control for Propulsion; Pulse Detonation and Jiun-Ming Li,Chiang Juay Teo,Cheng Wang Book 2018 Springer International Publishing

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发表于 2025-3-21 19:22:52 | 显示全部楼层 |阅读模式
书目名称Detonation Control for Propulsion
副标题Pulse Detonation and
编辑Jiun-Ming Li,Chiang Juay Teo,Cheng Wang
视频videohttp://file.papertrans.cn/270/269362/269362.mp4
概述Collects chapter contributions from the world’s notable researchers and groups currently carrying out research programs on detonation technology.Includes up-to-date reviews and research results of det
丛书名称Shock Wave and High Pressure Phenomena
图书封面Titlebook: Detonation Control for Propulsion; Pulse Detonation and Jiun-Ming Li,Chiang Juay Teo,Cheng Wang Book 2018 Springer International Publishing
描述.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 scie
出版日期Book 2018
关键词Shock wave; Deflagration and Detonation; Air-breathing Propulsion; Rocket Propulsion; Detonation Technol
版次1
doihttps://doi.org/10.1007/978-3-319-68906-7
isbn_softcover978-3-319-88679-4
isbn_ebook978-3-319-68906-7Series ISSN 2197-9529 Series E-ISSN 2197-9537
issn_series 2197-9529
copyrightSpringer International Publishing AG 2018
The information of publication is updating

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Development of Gasturbine with Detonation Chamber, achieved are presented. It was found that for conditions when the GTD-350 engine was supplied by gaseous hydrogen or by dual-fuel, Jet-A and gaseous hydrogen, thermal efficiency of the engine could be improved even by 5–7% as compared to the efficiency of the base engine.
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Flow Structure in Rotating Detonation Engine with Separate Supply of Fuel and Oxidizer: Experiment specific impulse. With the growth of the specific mass flow rate of reactive mixture, the operation process, on the one hand, becomes more stable, and on the other hand, the number of detonation waves simultaneously rotating in one direction in the combustor annulus increases. The results of DLRE fi
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On the Investigation of Detonation Re-initiation Mechanisms and the Influences of the Geometry Confmes, which is discovered to be the main reason leading to the discrepancies between the previous similar studies. The width of the bifurcation channel is also critical as it can directly affect the induction length during detonation diffraction which determines the shock reflection strength. The dif
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Jessica L. Dillon,Laura J. Tafespecific impulse. With the growth of the specific mass flow rate of reactive mixture, the operation process, on the one hand, becomes more stable, and on the other hand, the number of detonation waves simultaneously rotating in one direction in the combustor annulus increases. The results of DLRE fi
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Grasiella A. Andriani,Cristina Montagnames, which is discovered to be the main reason leading to the discrepancies between the previous similar studies. The width of the bifurcation channel is also critical as it can directly affect the induction length during detonation diffraction which determines the shock reflection strength. The dif
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