跨介质冲压发动机理论性能与工作参数分析

doi:10.7527/S1000-6893.2020.23764

流体力学与飞行力学

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跨介质冲压发动机理论性能与工作参数分析

陈文武, 黄利亚, 夏智勋, 李鹏飞

国防科技大学空天科学学院, 长沙 410073

收稿日期:2019-12-26 修回日期:2020-01-30 出版日期:2020-11-15 发布日期:2020-04-10
通讯作者: 黄利亚 E-mail:huangliya05@nudt.edu.cn

Theoretical performance and working parameters analysis of trans-medium ramjet

CHEN Wenwu, HUANG Liya, XIA Zhixun, LI Pengfei

College of Aerospace Science and Engineering, National University of Defense Technology, Changsha 410073, China

Received:2019-12-26 Revised:2020-01-30 Online:2020-11-15 Published:2020-04-10

摘要/Abstract

摘要： 针对空水一体跨介质导弹应用需求，提出了一种采用同一金属基固体推进剂，能够实现在空中和水中工作的跨介质冲压发动机方案。分析了空中和水中典型工况下，金属基固体推进剂配方、空/水燃比、金属种类等对跨介质冲压发动机理论性能的影响。针对给定的跨介质导弹飞行弹道和金属基固体推进剂配方，对发动机设计参数进行了选取，并完成了空中和水中工作条件下发动机工作参数计算，从理论上验证了该跨介质冲压发动机方案的可行性。

关键词: 跨介质, 冲压发动机, 理论性能, 设计参数, 构型方案

Abstract: A scheme of trans-medium ramjet engine which can work in both air and water with the same metal solid propellant is proposed to satisfy the application requirements of air-water integrated trans-medium missiles. We study the influence of the solid propellant formulation, air/water fuel ratio and metal type on the theoretical performance of trans-medium ramjets, followed by the selection of the design parameters of the engine with a given flight trajectory of the trans-medium missile and the metal based solid propellant. The operating parameters of the engine working in both air and water are obtained, theoretically verifying the feasibility of the scheme of trans-medium ramjets.

Key words: trans-medium, ramjet, theoretical performance, design parameters, configuration scheme

中图分类号:

V236

陈文武, 黄利亚, 夏智勋, 李鹏飞. 跨介质冲压发动机理论性能与工作参数分析[J]. 航空学报, 2020, 41(11): 123764-123764.

CHEN Wenwu, HUANG Liya, XIA Zhixun, LI Pengfei. Theoretical performance and working parameters analysis of trans-medium ramjet[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(11): 123764-123764.

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E-mail：hkxb@buaa.edu.cn

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主管单位：中国科学技术协会主办单位：中国航空学会北京航空航天大学

跨介质冲压发动机理论性能与工作参数分析

Theoretical performance and working parameters analysis of trans-medium ramjet

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