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再入飞行器复杂结构随机振动响应分析研究
引用本文:徐孝诚,王成华,韩增尧. 再入飞行器复杂结构随机振动响应分析研究[J]. 强度与环境, 2002, 29(3): 1-4
作者姓名:徐孝诚  王成华  韩增尧
作者单位:北京特殊机电研究所,北京,100076;北京特殊机电研究所,北京,100076;北京特殊机电研究所,北京,100076
摘    要:本文用MSC/NASTRAN软件对再入飞行器复杂结构轴向随机振动试验和横向随机振动试验进行了响应分析,并与试验测量结果进行了比较,两者基本相符:加速度响应均方根值预示误差小于30%(轴向随机振动响应分析)和50%(横向随机振动响应分析)。本文采用的飞行器复杂结构随机振动响应分析方法和技术途径得到试验验证。

关 键 词:飞行器复杂结构  随机振动  响应分析  试验验证  MSC/NASTRAN
文章编号:1006-3919(2002)03-0001-04
修稿时间:2001-06-22

Study on Random Vibration Response Analysis of Reentry Vehicle Complex Structure
XU Xiao cheng WAN Cheng hua HAN Zeng yao. Study on Random Vibration Response Analysis of Reentry Vehicle Complex Structure[J]. Structure & Environment Engineering, 2002, 29(3): 1-4
Authors:XU Xiao cheng WAN Cheng hua HAN Zeng yao
Abstract:The response analysis on axial and transverse random vibration tests of reentry vehicle complex structure have been done using software MSC/NASTRAN in this paper,and are compared with test results.Results of response analysis are closed to test results:the prediction erros of acceleration response RMS values are less than 30%(axial random vibration)and 50%(transverse random vibration).The method and technical route on random vibration response analysis of vehicle complex structure have been validated.
Keywords:Vehicle complex structure  Random vibration  Response analysis  Test validation  MSC/NASTRAN
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