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运载火箭结构动力学模拟技术研究进展

潘忠文 曾耀祥 廉永正 邢誉峰

潘忠文, 曾耀祥, 廉永正, 邢誉峰. 运载火箭结构动力学模拟技术研究进展[J]. 力学进展, 2012, 42(4): 406-415. doi: 10.6052/1000-0992-12-063
引用本文: 潘忠文, 曾耀祥, 廉永正, 邢誉峰. 运载火箭结构动力学模拟技术研究进展[J]. 力学进展, 2012, 42(4): 406-415. doi: 10.6052/1000-0992-12-063
PAN Zhongwen, ZENG Yaoxiang, LIAN Yongzheng, XING Yufeng. REVIEWS IN STRUCTURAL DYNAMICS ANALOGY TECHNIQUE OF LAUNCH VEHICLE[J]. Advances in Mechanics, 2012, 42(4): 406-415. doi: 10.6052/1000-0992-12-063
Citation: PAN Zhongwen, ZENG Yaoxiang, LIAN Yongzheng, XING Yufeng. REVIEWS IN STRUCTURAL DYNAMICS ANALOGY TECHNIQUE OF LAUNCH VEHICLE[J]. Advances in Mechanics, 2012, 42(4): 406-415. doi: 10.6052/1000-0992-12-063

运载火箭结构动力学模拟技术研究进展

doi: 10.6052/1000-0992-12-063
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

REVIEWS IN STRUCTURAL DYNAMICS ANALOGY TECHNIQUE OF LAUNCH VEHICLE

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: 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.

     

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  • 收稿日期:  2012-03-20
  • 修回日期:  2015-05-31
  • 刊出日期:  2012-07-25

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