Experiments on the Interaction of a Fast-Moving Shock with an Elastic Panel
Author:
Affiliation:
1. DLR, German Aerospace Center, 51147 Cologne, Germany
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J054233
Reference22 articles.
1. Side-Load Phenomena in Highly Overexpanded Rocket Nozzles
2. SchmuckerR. “TUM-LRT Bericht TB-10: Strömungsvorgänge beim Betrieb Überexpandierter Düsen chemischer Raketentriebwerke,” Technische Univ. München—Lehrstuhl für Raumfahrttechnik TR, Munich, Germany, 1973.
3. KoschelW. “Flight 157—Ariane 5 ECA: Report of the Inquiry Board,” ESA TR, 2003.
4. Large-eddy simulation of a supersonic turbulent boundary layer over a compression–expansion ramp
5. Large-eddy simulation of passive shock-wave/boundary-layer interaction control
Cited by 68 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. Flow Response of a Laminar Shock–Boundary Layer Interaction to Prescribed Surface Motions;AIAA Journal;2024-08-13
2. Nonlinear aeroelastic behavior of a panel impinged by oscillating shock;Nonlinear Dynamics;2024-08-06
3. Effect of Model Fidelity on High-Speed Aeroelastic Behavior of a Cantilever Plate;AIAA Journal;2024-08-05
4. Synchronized shock wave and compliant wall interactions: Experimental characterization and aeroelastic modeling;Journal of Fluids and Structures;2024-08
5. Fluid–Structure Interactions between Oblique Shock Trains and Thin-Walled Structures in Isolators;Aerospace;2024-06-18
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