A numerical investigation of flow dynamics inside wall cavity and strut cavity placed in supersonic airflows

Author:

Dhankarghare A. A.1ORCID,Jayachandran T.1,Muruganandam T. M.1

Affiliation:

1. Aerospace Department, IIT Madras, Chennai, Tamil Nadu 600036, India

Abstract

A study on flow dynamics in strut cavity and wall cavity in different freestream Mach numbers using numerical simulations has been conducted. A strut cavity is the space between two struts longitudinally aligned next to each other, and a wall cavity is the cavity in the wall. Our earlier results showed that both cavities exhibited oscillations for low values of supersonic Mach numbers, while oscillations decreased for high values. However, the strut cavity responded better to the change in Mach number than the wall cavity. The present work explores wave propagation and wave interactions inside the cavities in different Mach number flows. It is shown that the flow velocity inside a cavity affects wave propagation. Secondary recirculation inside the cavities has been discussed. The work also revisits the process of wave generation inside the cavities. Furthermore, an insight into the vortex propagation along the cavity length has also been provided. The results suggest that the vortex velocity may not remain uniform throughout the cavity length and may depend on the flow Mach number. Finally, the mass exchange between the cavity and the freestream is described and compared for different cavities. Flow particles are tracked in the shear layer and inside the cavity to suggest the locations of mass exchange.

Publisher

AIP Publishing

Subject

Condensed Matter Physics,Fluid Flow and Transfer Processes,Mechanics of Materials,Computational Mechanics,Mechanical Engineering

Reference70 articles.

1. Computational analysis of unsteady supersonic cavity flows driven by thick shear layers

2. Flow-induced pressure oscillations in shallow cavities

3. Cavity Flame-Holders for Ignition and Flame Stabilization in Scramjets: An Overview

4. K. Krishnamurty , “ Acoustic radiation from two-dimensional rectangular cutouts in aerodynamic surfaces,” Technical Note 3487 (1955); available at https://digital.library.unt.edu/ark:/67531/metadc57843/.

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