Experimental and theoretical study of swept-wing boundary-layer instabilities. Three-dimensional Tollmien-Schlichting instability-Reference-Cited by-同舟云学术

登录注册会员服务联系我们

Experimental and theoretical study of swept-wing boundary-layer instabilities. Three-dimensional Tollmien-Schlichting instability

Published:2019-11-01 Issue:11 Volume:31 Page:114104
ISSN:1070-6631
Container-title:Physics of Fluids
language:en
Short-container-title:Physics of Fluids

Author:

Borodulin V. I.¹^ORCID,Ivanov A. V.¹,Kachanov Y. S.¹^ORCID,Mischenko D. A.¹,Örlü R.²^ORCID,Hanifi A.²,Hein S.³

Affiliation:

1. Khristianovich Institute of Theoretical and Applied Mechanics, Novosibirsk 630090, Russian Federation

2. KTH Royal Institute of Technology, Linné FLOW Centre, Department of Mechanics, SE-100 44 Stockholm, Sweden

3. Institute of Aerodynamics and Flow Technology, DLR, 37073 Göttingen, Germany

Funder

Seventh Framework Programme

Siberian Branch, Russian Academy of Sciences

Publisher

AIP Publishing

Subject

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

Link

http://aip.scitation.org/doi/pdf/10.1063/1.5125812

Reference32 articles.

1. Experimental and theoretical study of swept-wing boundary-layer instabilities. Unsteady crossflow instability

2. Swept-wing boundary-layer receptivity to surface non-uniformities

3. STABILITY AND TRANSITION OF THREE-DIMENSIONAL BOUNDARY LAYERS

4. On the stability of an infinite swept attachment line boundary layer

Cited by 14 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. Investigation of Hybrid Laminar Flow Control Capabilities from the Flight Envelope Perspective;Journal of Aircraft;2024-08-23

2. Roughness induced transition delay in a swept-wing boundary layer in presence of freestream disturbances, Part 1: Turbulence effects;European Journal of Mechanics - B/Fluids;2024-01

3. Receptivity and Stability Theory Analysis of a Transonic Swept Wing Experiment;Aerospace;2023-10-23

4. Multidisciplinary Design Optimization of Transonic Wings with Boundary-Layer Suction;Journal of Aircraft;2023-10-04

5. Influence of Reynolds number on the natural transition of boundary layers over underwater axisymmetric bodies;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