中国科学院机构知识库网格
Chinese Academy of Sciences Institutional Repositories Grid
On theoretical modeling of underdriven oblique detonation phenomenon

文献类型:期刊论文

作者Li HY(李昊洋)2,4; Zhang, Zijian1,3; Yao KP(姚克鹏)2,4; Wang C(王春)2,4; Wen, Chihyung5
刊名PHYSICS OF FLUIDS
出版日期2025-09-01
卷号37期号:9页码:15
ISSN号1070-6631
DOI10.1063/5.0285978
英文摘要

Polar analysis is an important theoretical method in shock and detonation fields. However, a detonation polar is fundamentally different from the well-established shock polar due to not only the reaction heat release but also its involvement of a so-called underdriven oblique detonation wave (ODW) with a flow deflection angle theta smaller than the Chapman-Jouguet (CJ) angle theta(CJ,) whose traditional modeling is recognized as non-physical in the literature. In this study, a far-field physical model of underdriven ODWs neglecting the initiation zone, as a CJ ODW surface followed by a centered expansion fan, is proposed based on the numerical observations of the flow features of a wedge-induced ODW at theta < theta CJ simulated using a finite-rate two-step chain-branching reaction model. Accordingly, the polar segment of underdriven ODWs in terms of pressure p and theta, i.e., the p-theta relation, is quantitatively constructed using a combination of the theoretical solution of a CJ ODW and the Prandtl-Meyer isentropic expansion relation. Thereafter, such physical and mathematical modeling of underdriven ODWs from a far-field perspective is well verified with a series of numerical cases simulated using a quasi-equilibrium reaction model. Finally, a sensitivity analysis is carried out to evaluate the effects of the viscous boundary layer developed on the wedge surface. The results showed that the initiation zone of viscous wedge-induced underdriven ODWs is significantly shorter than that of the inviscid counterparts, but the viscosity effect is negligible from the far-field perspective. This work advances the fundamental understanding of underdriven ODWs and supplements the theoretical modeling of the oblique detonation phenomenon.

分类号一类/力学重要期刊
WOS关键词BOUNDARY-LAYER ; SHOCK ; WAVE ; STABILITY ; INSTABILITY ; INITIATION ; STEADY
资助项目National Natural Science Foundation of China10.13039/501100001809[12202374] ; National Natural Science Foundation of China10.13039/501100001809[12072353] ; National Natural Science Foundation of China10.13039/501100001809[12132017] ; National Natural Science Foundation of China
WOS研究方向Mechanics ; Physics
语种英语
WOS记录号WOS:001562002800021
资助机构National Natural Science Foundation of China10.13039/501100001809 ; National Natural Science Foundation of China
其他责任者Zhang, Zijian
源URL[http://dspace.imech.ac.cn/handle/311007/103611]  
专题力学研究所_高温气体动力学国家重点实验室
作者单位1.State Key Lab Environm Characterist & Effects Near, Beijing 100081, Peoples R China;
2.Univ Chinese Acad Sci, Sch Engn Sci, Beijing 100049, Peoples R China;
3.Beijing Inst Technol, Sch Aerosp Engn, Beijing 100081, Peoples R China;
4.Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China;
5.Hong Kong Polytech Univ, Dept Aeronaut & Aviat Engn, Hong Kong, Peoples R China
推荐引用方式
GB/T 7714
Li HY,Zhang, Zijian,Yao KP,et al. On theoretical modeling of underdriven oblique detonation phenomenon[J]. PHYSICS OF FLUIDS,2025,37(9):15.
APA Li HY,Zhang, Zijian,Yao KP,Wang C,&Wen, Chihyung.(2025).On theoretical modeling of underdriven oblique detonation phenomenon.PHYSICS OF FLUIDS,37(9),15.
MLA Li HY,et al."On theoretical modeling of underdriven oblique detonation phenomenon".PHYSICS OF FLUIDS 37.9(2025):15.

入库方式: OAI收割

来源:力学研究所

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