首页 | 本学科首页   官方微博 | 高级检索  
     检索      

声激励柱壳响应分析中的结合受纳函数
引用本文:曹茂国,李琳.声激励柱壳响应分析中的结合受纳函数[J].航空动力学报,2002,17(2):201-204.
作者姓名:曹茂国  李琳
作者单位:北京航空航天大学,动力系,北京,100083
基金项目:航空科学基金资助项目 (99C5 10 78
摘    要:结合受纳函数 (Joint Acceptance Function)是分析声载荷作用下结构特性时遇到的一个特殊的函数。这个函数不仅取决于结构模态 ,还取决于声场特性。本文以柱壳结构为研究对象 ,从分析结合受纳函数的定义、性质入手 ,研究如何利用结构分析中广泛采用的有限元数值结果来计算结合受纳函数 ,获得一种解决工程问题的通用方法。通过和解析解获得的结果比较说明这种结合受纳函数的数值计算方法是可行的。

关 键 词:声激励  随机振动  响应分析  结合受纳函数
文章编号:1000-8055(2002)02-0201-04
收稿时间:2001/4/20 0:00:00
修稿时间:2001年4月20日

The Joint Acceptance Function in Response Analysis of Cylindrical Shell Excited by Noise
CAO Mao-guo and LI Lin.The Joint Acceptance Function in Response Analysis of Cylindrical Shell Excited by Noise[J].Journal of Aerospace Power,2002,17(2):201-204.
Authors:CAO Mao-guo and LI Lin
Institution:Beijing University of Aeronautics and Astronautics,Beijing 100083,China;Beijing University of Aeronautics and Astronautics,Beijing 100083,China
Abstract:In analysis of structures excited by noise a special function joint acceptance function should be calculated.This function represents the coupled relation between structural modes and sound modes.It is an integration of them in space.In general,this function can be obtained only in the case where the analytical experssions for both structural modes and sound modes have been established.However,for most engineering structures such as the casing of aero engine it is difficult to obtain the analytical expression for its modes (either structural or sound).The article presents the research work in view of this problem.Considering the main structural type of the aero engine,we take cylindrical shell as studied structural type.In the article it is studied how to calculate the joint acceptance function based on the result obtained by finite element method,which is used widely in structure analysis.A general numerical calculating method is presented.The result obtained by this method is compared with the analytical result.
Keywords:acoustic excitation  random vibration  response analysis  joint acceptance function
本文献已被 CNKI 万方数据 等数据库收录!
点击此处可从《航空动力学报》浏览原始摘要信息
点击此处可从《航空动力学报》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号