| 引用本文: | 雷勇军,卓曙君,郑荣跃,等.卫星整流罩结构动力特性与分离运动分析.[J].国防科技大学学报,1997,19(4):21-25.[点击复制] |
| Lei Yongjun,Zhuo Shujun,Zheng Rongyue,et al.Dynamic Characteristic and Separation Behavior Analysis for Satellite Fairing[J].Journal of National University of Defense Technology,1997,19(4):21-25[点击复制] |
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| 卫星整流罩结构动力特性与分离运动分析 |
| 雷勇军, 卓曙君, 郑荣跃, 任均国 |
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(国防科技大学 航天技术系 湖南 长沙 410073)
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| 摘要: |
| 针对复合材料蜂窝夹芯板壳组成的卫星整流罩, 用有限元法建立了该罩的结构动力学数值模型, 编制了相应的有限元分析软件包, 计算了全罩、半罩在不同边界条件下的自由振动频率和模态, 并分析了抛罩时半罩的分离轨迹和气动力作用下爆炸螺栓的承载情况。 |
| 关键词: 有限元法, 整流罩, 频率, 振型, 分离 |
| DOI： |
| 投稿日期：1996-11-21 |
| 基金项目: |
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| Dynamic Characteristic and Separation Behavior Analysis for Satellite Fairing |
| Lei Yongjun, Zhuo Shujun, Zheng Rongyue, Ren Junguo |
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(Department of Aerospace Technology, NUDT, Changsha, 410073)
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| Abstract: |
| This paper gives the structural dynamic FEM model and corresponding FEM software package for a certain honeycomb sandwich composite satellite fairing. The natural frequencies and modes of the whole and half fairing under different boundary conditions are calculated. The separation behavior of half fairing and the load distribution in all binder blots subjected to aerodynamic load are analyzed. |
| Keywords: FEM, fairing, natural frequency, natural mode, separation |
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