Numerical investigation of shock-turbulent mixing layer interaction and shock-associated noise-Reference-Cited by-同舟云学术

登录注册会员服务联系我们

Numerical investigation of shock-turbulent mixing layer interaction and shock-associated noise

Published:2021-02-01 Issue:2 Volume:33 Page:025105
ISSN:1070-6631
Container-title:Physics of Fluids
language:en
Short-container-title:Physics of Fluids

Author:

Shi Fangcheng¹,Gao Zhenxun¹²³^ORCID,Jiang Chongwen¹,Lee Chun-Hian¹^ORCID

Affiliation:

1. Beihang University, Beijing 100191, People’s Republic of China

2. Laboratory of Aero-Thermal Protection Technology for Aerospace Vehicles, Beijing 100191, People’s Republic of China

3. Ningbo Institute of Technology, Zhejiang 315800, People’s Republic of China

Funder

National Defense Foundation Enhancement Program

Foundation for Innovative Research Groups of the National Natural Science Foundation of China

National Natural Science Foundation of China

Publisher

AIP Publishing

Subject

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

Link

https://aip.scitation.org/doi/pdf/10.1063/5.0034346

Reference81 articles.

1. Vorticity-production mechanisms in shock/mixing-layer interaction problems

2. Irregular self-similar configurations of shock-wave impingement on shear layers

3. Interaction of oblique shock waves and planar mixing regions

4. Organized structure in a compressible turbulent shear layer

Cited by 15 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

1. Shock waves affected turbulent mixing region development in a strut-based scramjet combustor;Acta Astronautica;2024-12

2. Effect of vibrational excitation on vorticity amplification and transportation in shock/isotropic turbulence interaction: A numerical investigation;Physics of Fluids;2024-08-01

3. Modified advection upstream splitting method: Revolutionizing accuracy and convergence speed in low-Mach flows;Physics of Fluids;2023-10-01

4. Effect of passive strut angle on the vortical structures and mixing characteristics of scramjet combustor;Physics of Fluids;2023-06-01

5. Effect of pressure gradient on flow instability in the subsonic–supersonic mixing layer;Physics of Fluids;2023-04-01

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