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Titlebook: Subsonic Combustion Ramjet Design; Antonella Ingenito Book 2021 The Author(s), under exclusive license to Springer Nature Switzerland AG 2

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发表于 2025-3-21 16:42:47 | 显示全部楼层 |阅读模式
书目名称Subsonic Combustion Ramjet Design
编辑Antonella Ingenito
视频video
概述Presents a thorough guide to the design of ramjet engines.Explains how to improve performance through material use, fuel type, and sizing.Offers a succinct, focused analysis of ramjet combustion in th
丛书名称SpringerBriefs in Applied Sciences and Technology
图书封面Titlebook: Subsonic Combustion Ramjet Design;  Antonella Ingenito Book 2021 The Author(s), under exclusive license to Springer Nature Switzerland AG 2
描述.This book presents a step-by-step methodology for the design of ramjet engines. It explores ramjet combustion, provides guidelines on how to size the engines, and discusses performance analysis...The book begins with an introduction to ramjet design, including fundamental definitions in the field. It then discusses ramjet engine performance, and fuels which can be used. Several types of ramjet engines are then explored, and guidelines for their design are presented, including flame holders, injectors, and combustors. Finally, the book concludes with a discussion of the types of materials which should be used for ramjet engines. ..This book is of interest to engine designers and engineers, researchers, and graduate students, as it collates research in a succinct, clear guide to the issue of designing ramjet engines. .
出版日期Book 2021
关键词Ramjet Engines; Ramjet Design; Ramjet Performance; High-Speed Propulsion; Supersonic Propulsion; Combusto
版次1
doihttps://doi.org/10.1007/978-3-030-66881-5
isbn_softcover978-3-030-66880-8
isbn_ebook978-3-030-66881-5Series ISSN 2191-530X Series E-ISSN 2191-5318
issn_series 2191-530X
copyrightThe Author(s), under exclusive license to Springer Nature Switzerland AG 2021
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发表于 2025-3-21 22:14:03 | 显示全部楼层
Subsonic Combustion Ramjet Design978-3-030-66881-5Series ISSN 2191-530X Series E-ISSN 2191-5318
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发表于 2025-3-22 07:36:53 | 显示全部楼层
Ramjet Engines Performance,Ramjet performance is calculated by means of the well-acknowledged Bryton cycle. The real Bryton cycle accounting for friction losses, pressure recovery, combustion efficiency and the thermal chocking, has been analyzed to establish the greatest operative conditions for the ramjet engine.
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发表于 2025-3-22 15:43:56 | 显示全部楼层
Step by Step RJ Design Methodology,In this section, an example of this step by step methodology to size a RJ engine for given input parameters and assumptions is reported.
发表于 2025-3-22 17:20:28 | 显示全部楼层
Antonella IngenitoPresents a thorough guide to the design of ramjet engines.Explains how to improve performance through material use, fuel type, and sizing.Offers a succinct, focused analysis of ramjet combustion in th
发表于 2025-3-22 21:29:19 | 显示全部楼层
Design of Supersonic/Hypersonic Vehicles,rating individually optimized system elements (as routinely done in designing subsonic aircraft) yields a significant reduction in performance [.]. Vanderkerchove (VDK) and Czysz [.] identified a new approach, based on the Küchemann tau, to screen, identify, and visualize the design to first order over a range of feasible solutions.
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SpringerBriefs in Applied Sciences and Technologyhttp://image.papertrans.cn/t/image/881385.jpg
发表于 2025-3-23 08:49:37 | 显示全部楼层
https://doi.org/10.1007/978-3-030-66881-5Ramjet Engines; Ramjet Design; Ramjet Performance; High-Speed Propulsion; Supersonic Propulsion; Combusto
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