Numerical investigation of free oblique detonation wave induced by non-intrusive energy deposition

doi:10.1063/5.0073035

	Numerical investigation of free oblique detonation wave induced by non-intrusive energy deposition
	Zhang WS(张文硕)1,2 ; Zhang, Zijian 3; Jiang ZL(姜宗林)1,2 ; Han X(韩信)1,2; Liu, Yunfeng1,2 ; Wang, Chun1,2
通讯作者	Liu, Yunfeng(liuyunfeng@imech.ac.cn)
发表期刊	AIP ADVANCES
	2021-12-01
卷号	11 期号:12 页码:17
摘要	To validate the concept of free oblique detonation waves (ODWs) induced by non-intrusive energy deposition applied in ODW engines (ODWEs), numerical simulations are performed by modeling the laser spark as a high-temperature and high-pressure zone embedding in the high-speed incoming flow and by solving the non-dimensional reactive Euler equations with one-step chemistry. The initiation process, flow structures, and self-adapted characteristics of such kinds of free ODWs in an open space are discussed with varying dimensionless source energy and inflow Mach number. The results show that free ODWs can be initiated successfully by local non-intrusive energy deposition. In particular, four ignition regimes, namely, the subcritical regime, the critical I regime, the critical II regime, and the supercritical regime, which are analogous to the one-dimensional direct initiation of detonation, are distinguished by varying the dimensionless source energy. However, the typical energy required by each ignition regime is higher than that in the one-dimensional case due to multi-dimensional energy transmission and instabilities. Moreover, the dimensionless source energy should be moderate to obtain a stable free ODW flow field because extremely low source energy leads to ignition failure, while extremely high source energy causes premature ignition. When the inflow Mach number varies, it is found that free ODWs can adjust automatically to a nearly Chapman-Jouguet state, indicating the self-sustaining nature of free detonation waves. Due to this feature, ODWE performance will be relatively stable despite the change in inflow Mach numbers if free ODWs are utilized in the combustor.
DOI	10.1063/5.0073035
收录类别	SCI ; EI
语种	英语
WOS记录号	WOS:000730522800003
关键词[WOS]	INDUCED SPARK-IGNITION ; DIRECT INITIATION ; LASER IGNITION ; SIMULATION ; STABILITY ; CRITERIA ; WEDGE
WOS研究方向	Science & Technology - Other Topics ; Materials Science ; Physics
WOS类目	Nanoscience & Nanotechnology ; Materials Science, Multidisciplinary ; Physics, Applied
资助项目	National Natural Science Foundation of China[11672312] ; National Natural Science Foundation of China[11532014]
项目资助者	National Natural Science Foundation of China
论文分区	二类
力学所作者排名	1
RpAuthor	Liu, Yunfeng
引用统计	被引频次：1[WOS] [WOS记录] [WOS相关记录]
文献类型	期刊论文
条目标识符	http://dspace.imech.ac.cn/handle/311007/88173
专题	高温气体动力学国家重点实验室
作者单位	1.Univ Chinese Acad Sci, Sch Engn Sci, Beijing 100049, Peoples R China; 2.Chinese Acad Sci, Inst Mech, Beijing 100190, Peoples R China; 3.Hong Kong Polytech Univ, Dept Aeronaut & Aviat Engn, Kowloon, Hong Kong, Peoples R China
推荐引用方式 GB/T 7714	Zhang WS,Zhang, Zijian,Jiang ZL,et al. Numerical investigation of free oblique detonation wave induced by non-intrusive energy deposition[J]. AIP ADVANCES,2021,11,12,:17.
APA	张文硕,Zhang, Zijian,姜宗林,韩信,Liu, Yunfeng,&Wang, Chun.(2021).Numerical investigation of free oblique detonation wave induced by non-intrusive energy deposition.AIP ADVANCES,11(12),17.
MLA	张文硕,et al."Numerical investigation of free oblique detonation wave induced by non-intrusive energy deposition".AIP ADVANCES 11.12(2021):17.

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