高超声速飞行器结构热-声振耦合动力学研究进展
Research Progress on Thermal-Acoustic Vibration Coupling Dynamics of Hypersonic Aircraft Structures
查看参考文献59篇
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文摘
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高超声速飞行器服役环境十分复杂,气动热、气动力和强噪声等多种环境载荷的共同作用,给飞行器结构安全性带来了巨大挑战;尤其在极致追求结构轻量化设计和实现时,热-声振耦合效应将会十分显著。本文大致总结了国内外高超声速飞行器热-声振耦合动力学研究的主要进展,归纳了在典型热、声及其耦合环境作用下飞行器结构的动力学响应,梳理了动态载荷环境结构动力学建模、计算方法和实验分析方法,描述了结构热-声振耦合动力学理论基础,并探讨了高超声速飞行器结构热-声振耦合动力学研究的重要方向。 |
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其他语种文摘
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The service environment of hypersonic aircraft is very complex. The combined action of various environmental loads such as aerodynamic heat, aerodynamic force and strong noise has brought great challenges to the structural safety of the aircraft. In particular, the vibration-acoustic coupling effect will be very significant for the extremely light-weighted aircraft structures. This paper roughly summarizes the main progress of the research on the thermal-acoustic-vibration coupling dynamics of hypersonic vehicles, summarizes the dynamic response of the aircraft structure under the action of typical thermal, acoustic and their coupled environments, and sorts out the dynamic structure of the dynamic load environment. Models, calculation methods and experimental analysis methods are classified to investigate the structural thermal-acoustic-vibration coupling dynamics, and the important directions of the research on the structural thermal-acoustic-vibration coupling dynamics of hypersonic vehicles are discussed. |
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来源
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强度与环境
,2022,49(4):1-8 【扩展库】
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DOI
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10.19447/j.cnki.11-1773/v.2022.04.001
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关键词
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高超声速飞行器
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热-声振耦合
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结构响应
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实验分析
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数值模拟
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地址
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1.
中国科学院力学研究所, 北京, 100190
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中国科学院大学工程科学学院, 北京, 100049
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语种
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中文 |
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文献类型
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综述型 |
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ISSN
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1006-3919 |
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学科
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航天(宇宙航行) |
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基金
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中国科学院A类先导项目
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文献收藏号
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CSCD:7320887
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