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有效载荷/运载火箭耦合分析的频域方法
引用本文:夏益霖.有效载荷/运载火箭耦合分析的频域方法[J].强度与环境,1997(1):20-25.
作者姓名:夏益霖
作者单位:北京强度环境研究所!北京,100076
摘    要:盘算尖响函数综合技术导出了用耦合频响函数和无有效载荷的运载火箭界面加速度响应表示的有效载荷/运载火箭耦合动力分析的频域方法,给出了以自由界面的运载火箭模态分数放自由界面或固定界面有效载荷模态参数构成的耦合频响函数表达式。

关 键 词:结构动力分析  模态综合法  频域分析  运载火箭

The Frequency-Domain Method for Dynamic Analysis of Payloads and Launch Vehicle Interaction
Xia Yilin.The Frequency-Domain Method for Dynamic Analysis of Payloads and Launch Vehicle Interaction[J].Structure & Environment Engineering,1997(1):20-25.
Authors:Xia Yilin
Institution:Beijing Institute of Structure and Environment Engineering
Abstract:In this paper the frequency-domain method for dynamic analysis of payloads and Launch vehicle interaction which is expressed by the coupling FRFs and the acceleration responses of interfaces of launch vehicle without payload is derived using the FRF's synthesis technique. The expressions of coupling FRFs which are formed by the modal parameters of launch vehicle with free interface and of payload with free interface or fixed interface are given. The acceleration responses of interfaces between different pay-loads can be transformed using the coupling FRFs. This method is suitable for the disign departments of payloads to conduct the dynamic analysis of interaction under the action of random excitation.
Keywords:Dynamic analysis  Structural dynamic response  Model integrated law  Frequency domain analysis
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