The effect of increasing rarefaction on the formation of Edney shock interaction patterns: type-I to type-VI

IF 1.7 4区 工程技术 Q3 MECHANICS Shock Waves Pub Date : 2022-12-06 DOI:10.1007/s00193-022-01109-y
M. B. Agir, C. White, K. Kontis
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Abstract

A shock–shock interaction problem can arise in high-speed vehicles where an oblique shock from one part of the body impinges on a bow shock from a different part of the body. The nature of the interaction can change as the vehicle increases in altitude to a more rarefied environment. In this work, the outcomes of a numerical study investigating the formation of Edney shock patterns from type-I to type-VI as a result of shock–shock interactions at different rarefaction levels are presented. The computations are conducted with a direct simulation Monte Carlo solver for a free-stream flow at a Mach number of 10. In shock–shock interaction problems, both geometrical and rarefaction parameters determine what type of Edney pattern is formed. The region on the shock impinged surface that experiences enhanced thermo-mechanical loads increases when the free-stream flow becomes more rarefied, but the peak values decrease. It is known that these shock interactions can have unsteady behavior in the continuum regime; the current work shows that although increasing rarefaction tends to move the flow toward steady behavior, under some conditions the flow remains unsteady.

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增加稀薄度对Edney激波相互作用模式形成的影响:i型到vi型
在高速车辆中,来自车身某一部分的斜冲击与来自车身另一部分的弓形冲击发生碰撞,可能会产生冲击-冲击相互作用问题。这种相互作用的性质会随着飞行器高度的增加而改变,从而进入更稀薄的环境。在这项工作中,提出了一项数值研究的结果,该研究调查了在不同稀薄水平的激波相互作用下从i型到vi型Edney激波模式的形成。用直接模拟蒙特卡罗求解器对马赫数为10的自由流进行了计算。在激波-激波相互作用问题中,几何参数和稀疏参数决定了形成何种类型的Edney图案。受冲击表面受热机械载荷增强的区域随着自由流动的减少而增加,但峰值减小。已知这些激波相互作用在连续介质中具有非定常行为;目前的研究表明,尽管增大的稀薄度会使流动趋于稳定,但在某些条件下,流动仍然是非稳定的。
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来源期刊
Shock Waves
Shock Waves 物理-力学
CiteScore
4.10
自引率
9.10%
发文量
41
审稿时长
17.4 months
期刊介绍: Shock Waves provides a forum for presenting and discussing new results in all fields where shock and detonation phenomena play a role. The journal addresses physicists, engineers and applied mathematicians working on theoretical, experimental or numerical issues, including diagnostics and flow visualization. The research fields considered include, but are not limited to, aero- and gas dynamics, acoustics, physical chemistry, condensed matter and plasmas, with applications encompassing materials sciences, space sciences, geosciences, life sciences and medicine. Of particular interest are contributions which provide insights into fundamental aspects of the techniques that are relevant to more than one specific research community. The journal publishes scholarly research papers, invited review articles and short notes, as well as comments on papers already published in this journal. Occasionally concise meeting reports of interest to the Shock Waves community are published.
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