本文的目的就是对壁板的热颤振特性进行系统深入的分析和研究，为高速飞行器的壁板结构的防颤振设计和壁板颤振抑制的研究建立理论基础。
The aim of this thesis is to analyze the panel flutter mechanism and establish a mechanical model for panel flutter analysis and this work is the basis of panel flutter control studies.
本论文详细讨论了飞行器黑匣子硬件部分的设计，主要设计工作内容有：(1)分析功能需求，设计黑匣子系统的框架结构。
This paper detailedly discussed the planning of the part of hardware in aerocraft Event recorder, Mainly work includes: (1) Analyze the function requirements and design the architecture block.
在飞行器结构中，连接面的存在将影响结构的静、动态分析。
Contact surfaces exist in structure of aircraft, which effect static and dynamic analysis.
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