Numerical investigation of unsteady aerodynamic characteristics induced by the interaction of oblique/bow shock waves during rotation

doi:10.1063/5.0159710

	Numerical investigation of unsteady aerodynamic characteristics induced by the interaction of oblique/bow shock waves during rotation
	Wang DG(王大高); Han GL(韩桂来); Liu MK(刘美宽); Jiang ZL(姜宗林)
发表期刊	PHYSICS OF FLUIDS
	2023-08-01
卷号	35 期号:8 页码:86124
ISSN	1070-6631
摘要	The interactions between oblique and bow shock waves are significant problems related to the aerodynamic force and thermal performance of hypersonic vehicles, but few studies have considered the dynamic effect of the body's motion on the phenomena. In this work, a numerical study on the oblique and bow shock waves ahead of an elliptic cylinder rotating with a forced-oscillation approach was conducted at Mach 5 by solving the unsteady, two-dimensional Navier-Stokes equations in a non-inertial coordinate system. The hysteresis loops of aerodynamic coefficients were analyzed first, and it was found that the moment is sensitive to rotation. Then, two different hysteresis forms were found at positive and negative angles of rotation (AOR), corresponding to cases with the interference point above or below the wall, respectively. When AOR is positive, the rate-dependent transition hysteresis among various shock interaction types causes the movement of strong flow structures (reflected shock wave, Mach stem, and jet) to always lag behind the body's motion. When AOR is negative, besides the evolution hysteresis of flow structures, two unusual patterns between Edney Types III and VI were observed on different transition paths, which led to very different peak pressures. Also discussed are the driving mechanisms associated with the effect of the subsonic region and the downstream boundary of the interaction zone, as well as the modulating action of the formed virtual Laval flow channel. Additional simulations were performed to study the effect of rotation speed on the transition boundary and the transition structures between Types III and VI.
DOI	10.1063/5.0159710
收录类别	SCI ; EI
语种	英语
WOS记录号	WOS:001053895200002
WOS研究方向	Mechanics ; Physics
WOS类目	Mechanics ; Physics, Fluids & Plasmas
项目资助者	This work was supported by the National Natural Science Foundation of China (Nos. 12132017, 11872066, and 11727901) and National Key Ramp ; amp ; D Program of China (No. 2022YFB3207000). [11872066, 11727901, 2022YFB3207000] ; National Natural Science Foundation of China ; National Key Ramp ; amp ; D Program of China ; [12132017]
论文分区	一类/力学重要期刊
力学所作者排名	1
RpAuthor	Han, GL (corresponding author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China. ; Han, GL (corresponding author), Univ Chinese Acad Sci, Sch Engn Sci, Beijing 100049, Peoples R China.
引用统计	被引频次：5[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/311007/92662
专题	高温气体动力学国家重点实验室
作者单位	1.{Wang Dagao, Han Guilai, Liu Meikuan, Jiang Zonglin} Chinese Acad Sci Inst Mech State Key Lab High Temp Gas Dynam Beijing 100190 Peoples R China 2.{Wang Dagao, Han Guilai, Liu Meikuan, Jiang Zonglin} Univ Chinese Acad Sci Sch Engn Sci Beijing 100049 Peoples R China
推荐引用方式 GB/T 7714	Wang DG,Han GL,Liu MK,et al. Numerical investigation of unsteady aerodynamic characteristics induced by the interaction of oblique/bow shock waves during rotation[J]. PHYSICS OF FLUIDS,2023,35,8,:86124.Rp_Au:Han, GL (corresponding author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China., Han, GL (corresponding author), Univ Chinese Acad Sci, Sch Engn Sci, Beijing 100049, Peoples R China.
APA	王大高,韩桂来,刘美宽,&姜宗林.(2023).Numerical investigation of unsteady aerodynamic characteristics induced by the interaction of oblique/bow shock waves during rotation.PHYSICS OF FLUIDS,35(8),86124.
MLA	王大高,et al."Numerical investigation of unsteady aerodynamic characteristics induced by the interaction of oblique/bow shock waves during rotation".PHYSICS OF FLUIDS 35.8(2023):86124.

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