Aerodynamic Response to a Compliant Panel in Mach 4 Flow
Author:
Affiliation:
1. Air Force Research Laboratory
2. Quantitech
Publisher
American Institute of Aeronautics and Astronautics
Reference31 articles.
1. Theoretical considerations of panel flutter at high supersonic Mach numbers.
2. Panel flutter - A review of the aeroelastic stability of plates and shells
3. Review of Nonlinear Panel Flutter at Supersonic and Hypersonic Speeds
4. Studies on Fluid-Thermal-Structural Coupling for Aerothermoelasticity in Hypersonic Flow
Cited by 13 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. The Impact of Upstream Static Deformation on Flow Past a Cylinder/Flare;Aerospace;2024-05-20
2. Two-dimensional pressure field imaging of an elastic panel executing post-flutter oscillations;Journal of Fluids and Structures;2024-03
3. Wall Pressure Response of a Mach 3 Turbulent Boundary Layer to a Compliant Clamped-Free-Clamped-Free Panel;AIAA SCITECH 2024 Forum;2024-01-04
4. Numerical study on the nonlinear characteristics of shock induced two-dimensional panel flutter in inviscid flow;Journal of Sound and Vibration;2023-11
5. Fluid structure interactions generated by an oblique shock impinging on a thin elastic panel;Journal of Fluids and Structures;2023-05
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