斜爆轰的多波结构及其稳定性研究进展

滕宏辉; 姜宗林

doi:10.6052/1000-0992-19-011

斜爆轰的多波结构及其稳定性研究进展

doi: 10.6052/1000-0992-19-011

滕宏辉^1,†, ,,
姜宗林^2,3

¹ 北京理工大学宇航学院,北京 100081
² 中国科学院力学研究所高温气体动力学国家重点实验室, 北京 100190
³ 中国科学院大学工程科学学院宇航工程科学系, 北京 100049

基金项目:

国家自然科学基金资助项目 (11822202; 91641130).

详细信息

作者简介:
滕宏辉, 北京理工大学教授, 主要研究气相爆轰物理及其应用.2003年于中国科学技术大学获学士学位,2008年于中国科学院力学研究所获博士学位.2010——2017年在中国科学院力学研究所工作,历任助理研究员、副研究员; 2017年至今在北京理工大学工作,历任特别研究员、教授. 在国内外学术期刊上发表论文50多篇,其中包括流体力学和燃烧学权威期刊J. Fluid Mech., Phys.Fluids, Combust. Flame, Proc. Combust. Inst.共15篇.获国家自然科学基金委优青项目、重大研究计划培育项目、面上项目以及若干国防类重点项目资助.2014年入选中国科学院青年创新促进会,2016年获中国科学院杰出科技成就奖(集体奖).现担任中国力学学会激波与激波管专业委员会委员,中国航空学会燃烧与传热传质专业委员会委员,中国工程热物理学会新型热力循环专业委员会委员,《推进技术》《航空学报》等期刊编辑委员会(青年)委员.

通讯作者:
滕宏辉

中图分类号: O381
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出版历程
- 收稿日期: 2019-07-22
- 刊出日期: 2020-10-08

Progress in multi-wave structure and stability of oblique detonations

TENG Honghui^{1,†
, ,},
JIANG Zonglin^2,3

¹ School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China
² State Key Laboratory of High Temperature Gas Dynamics, Institute of Mechanics, Chinese Academy of Sciences, Beijing 100190, China
³ Department of Aerospace Engineering Science, School of Engineering Science, University of Chinese Academy of Sciences, Beijing 100049, China

More Information

Corresponding author: TENG Honghui

摘要

摘要: 斜爆轰是气相爆轰物理的一个重要研究方向,在航空航天新型动力领域有重要的潜在应用价值.作为激波诱导的高速燃烧, 斜爆轰波可以简化为包含能量添加的间断面.然而, 斜爆轰流动中往往涉及激波、湍流等多种的流体力学现象,它们和燃烧放热耦合在一起, 导致流动和燃烧机理非常复杂. 一方面,斜爆轰波具有的多尺度和非线性的特征, 理论研究难以深入; 另一方面,爆轰波流场高温、高压、高速的特点, 又给实验研究带来了很大的困难.过去20年, 主要借助数值方法,研究者对斜爆轰波开展了系统的模拟和分析,在诸多方面取得了明显的进展.本文首先介绍了理想情况下的起爆区波系结构和波面稳定性研究进展;其次着眼于推进系统的问题,关注了非均匀来流效应以及斜爆轰波与稀疏波的作用;最后对未来的研究工作提出一些建议.
- 斜爆轰 /
- 激波 /
- 爆燃波 /
- 起爆 /
- 稳定性
Abstract: Oblique detonation is an important direction in gaseous detonation physics and has great potential in the application of new-concept aeronautic and astronautic propulsion. As the fast combustion induced by shock, the oblique detonation wave could be simplified into a discontinuity with energy input. However, in oblique detonation flow, there concern several complicated fluid phenomena, such as shock wave and turbulence, which are coupled with the heat release and result in complicated flow and combustion mechanisms. A theoretical investigation is hard to be performed due to the characteristics of multi-scale and nonlinearity. Meanwhile, experimental investigation encounters the difficulties from measuring the flow fields of high temperature, high pressure, and high velocity. In the last two decades, the main progress of oblique detonation is achieved by numerical investigation through comprehensive simulation and analysis. First of all, the multi-wave structure of the initiation region and surface stability are introduced in the ideal inflow conditions. Then, derived from the application in engines, the effects of inflow inhomogeneity and interaction with expansion waves are studied and analyzed. Finally, some suggestions on future work are proposed and discussed.
- oblique detonation /
- shock /
- deflagration /
- initiation /
- stability

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