运载火箭结构动力学模拟技术研究进展

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doi:10.6052/1000-0992-12-063

1 北京宇航系统工程研究所, 北京 100076
2 北京航空航天大学固体力学研究所, 北京 100191

基金项目:总装备部十一五预研项目(51320103), 航天支撑项目(618010604-02), 国防“973” 项目(613133) 资助

详细信息

通讯作者:
潘忠文

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- 文章访问数:1913
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- 被引次数:0
出版历程
- 收稿日期:2012-03-20
- 修回日期:2015-05-31
- 刊出日期:2012-07-25

REVIEWS IN STRUCTURAL DYNAMICS ANALOGY TECHNIQUE OF LAUNCH VEHICLE

1 Beijing Institute of Astronautical System Engineering , Beijing 100076, China
2 The Solid Mechanics Institute, Beihang University, Beijing 100191, China

Funds:The project was supported by the Eleventh Five General Armament Department Advanced Research Project (51320103), Space-Support Project (618010604-02) and 973 National Defense Project (613133).

More Information

Corresponding author:PAN Zhongwen

摘要

摘要:本文首先按照火箭的不同型号, 综述了国内外全箭模态分析及试验验证的进展情况; 然后, 从蒙皮加筋圆柱壳结构动力学建模、液体推进剂动力学模拟、局部振型斜率预示三个方面, 综述了火箭动力学建模技术进展; 最后根据火箭动力学发展需求, 对后续研究提出了一些建议.
- 全箭模态/
- 试验验证/
- 板壳结构/
- 推进剂/
- 振型斜率
Abstract:First in this paper, based on different kinds of launch vehicles, domestic and overseas overall modal analysis and experiments verification are respectively reviewed. Then dynamics modeling techniques are respectively summarized from three directions, such as dynamics modeling of cylindrical shell- stiffened, dynamics simulation of liquid propellant, prediction methods of local mode shape-slope. Finally, further research directions are suggested based on the development needs of structural dynamics of launch vehicles.
- overall model/
- experiments verification/
- cylindrical shell-stiffened/
- liquid propellant/
- mode shapeslope

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参考文献 (81)

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