摘要
对高频问题,为了捕捉到结构特征长度,有限元和边界元需要很小的网格尺度,这样数值计算的工作量相当大,甚至不可实现。笔者研究求解了航天飞行器仪器舱高频结构声振问题的统计能量方法,给出了用统计能量法计算的一般步骤;编程实现了动响应参数的计算,并对结果进行了分析。
For the problems of high-frequencies,in order to capture the structural characteristic length,many smaller mesh sizes is required for finite element or boundary element model,thus to make the computational work becoming considerable,even impossible implement.The statistic energy method for solving high-frequency structural acoustic-vibration problem of high speed aero-craft is studied in this paper.The basic principle of SEA was given,the dynamic response parameters were calculated by programming and its results were analyzed.
出处
《装备制造技术》
2007年第6期1-4,共4页
Equipment Manufacturing Technology
基金
国家自然科学基金资助项目(10471109)
教育部留学归国基金项目[2004]527
关键词
统计能量分析
动响应
声振系统
Statistical energy analysis
Dynamic response
Acoustic-vibration system