Critical decoupling criterion for dual-incident shock wave/turbulent boundary layer interaction

Author:

Yang Shu-ziORCID,Xie Wen-zhongORCID,Sun Hao-yu

Abstract

Interaction zones resulting from the dual-incident shock wave/turbulent boundary layer interactions (D-ISWTBLI) typically exhibit one of two distinct flow patterns: the formation of two isolated small-scale interaction zones following decoupling or the presence of a coupled large-scale interaction zone. This paper investigates the underlying mechanism governing the transition of the flow field of D-ISWTBLI, shifting from a coupled flow pattern to an isolated one. To achieve this, we employ numerical simulations and propose a criterion for determining the critical decoupling condition. Our study commences by presenting an analysis of the time-averaged pressure distribution along-the-wall and the corresponding changes in the characteristic scale of the coupled interaction zone as the spacing between the shock incident points continuously increases. We elucidate the variation mechanism of the characteristic scale by analyzing the flow field. Subsequently, based on the intrinsic relationships among the characteristic scales of the coupled interaction zone in their critical state, we establish a relational expression that links the critical decoupling spacing with the characteristic scales of the interaction zone in the critical state. We then employ numerical simulation data, accounting for key influencing factors such as the intensity ratio of the individual incident shock components comprising the dual-incident shock system, the overall intensity of the dual-incident shock system, and the free-stream conditions to determine the critical decoupling condition. This critical decoupling condition effectively delineates the flow pattern of the interaction zone under various free-stream conditions and shock configurations, a conclusion that is corroborated by published experimental data.

Funder

National Natural Science Foundation of China

Qinglan Project of Jiangsu Province of China

Publisher

AIP Publishing

Reference44 articles.

1. S. D. Holland , “ Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6,” NASA-TM-109152, NASA Langley Technical Report Server (1994).

2. A joint study on the starting limits of a generic supersonic inlet,2017

3. Experimental investigation on the self-starting characteristics of hypersonic inlets,2017

4. Influence of internal contraction section configurations on self-starting ability of hypersonic inlets;J. Aerosp. Power,2017

Cited by 1 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

同舟云学术

1.学者识别学者识别

2.学术分析学术分析

3.人才评估人才评估

"同舟云学术"是以全球学者为主线,采集、加工和组织学术论文而形成的新型学术文献查询和分析系统,可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容,当前同舟云学术共收录了国内外主流学术期刊6万余种,收集的期刊论文及会议论文总量共计约1.5亿篇,并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询!咨询电话:010-8811{复制后删除}0370

www.globalauthorid.com

TOP

Copyright © 2019-2024 北京同舟云网络信息技术有限公司
京公网安备11010802033243号  京ICP备18003416号-3