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变质量梁的自适应Newmark法

王宇楠 邢誉峰

王宇楠, 邢誉峰. 变质量梁的自适应Newmark法[J]. 北京航空航天大学学报, 2014, 40(6): 829-833. doi: 10.13700/j.bh.1001-5965.2013.0400
引用本文: 王宇楠, 邢誉峰. 变质量梁的自适应Newmark法[J]. 北京航空航天大学学报, 2014, 40(6): 829-833. doi: 10.13700/j.bh.1001-5965.2013.0400
Wang Yunan, Xing Yufeng. Self-adaptive Newmark method of variable-mass beam dynamic system[J]. Journal of Beijing University of Aeronautics and Astronautics, 2014, 40(6): 829-833. doi: 10.13700/j.bh.1001-5965.2013.0400(in Chinese)
Citation: Wang Yunan, Xing Yufeng. Self-adaptive Newmark method of variable-mass beam dynamic system[J]. Journal of Beijing University of Aeronautics and Astronautics, 2014, 40(6): 829-833. doi: 10.13700/j.bh.1001-5965.2013.0400(in Chinese)

变质量梁的自适应Newmark法

doi: 10.13700/j.bh.1001-5965.2013.0400
基金项目: 

国家自然科学基金资助项目(1172028,11372021)

详细信息
    作者简介:

    王宇楠(1988- ),女,辽宁沈阳人,硕士生,wayunan@gmail.com.

  • 中图分类号: O342

Self-adaptive Newmark method of variable-mass beam dynamic system

  • 摘要: 用变质量梁来模拟推进剂减少的液体火箭.先以一弹簧-变质量小球系统为例,用其求解结果与解析解进行比较.再以时不变的简支梁为算例,确定多自由度系统下与结构动特性协同的自适应Newmark方法中的参数选取.最后用时变的简支梁模型模拟贮箱质量的实际变化方式,运用与结构动特性协同的自适应Newmark方法、模态叠加法、Newmark平均加速度方法(NMA法)和Fox-Goodwin方法(NMF法)对其求解.比较结果证明自适应Newmark算法对于时变系统的适用性,尤其具有高精度特性.

     

  • [1] Meshcherskii I V.Dynamics of a point of variable mass[D]. st Petersburg: Printing House of the Imperial Academy of Sciences,1897
    [2] Arutyunyan N K. Boundary value problem of the theory of creep for a body with accretion[J].Applied Math and Mech,1977, 41(5): 804-807
    [3] Arutyunyan N K, Metlov V V.Some problems in the theory of creep in bodies with variable boundaries[J].Mech of Solids,1982,17(5):92-95
    [4] Arutyunyan N K, Namov V E.The theory of viscoelastic Plasticity of a growing body [J].Applied Math and Mech,1984, 48(1): 1-4
    [5] Meirovitch L. General motion of a variable mass flexible rocket with internal flow[J].Journal of Spacecraft and Rockets,1970, 7(2): 186-195
    [6] Banerjee A K. Dynamics of a variable-mass,flexible-body system[J].Journal of Guidance,Control,and Dynamics,2000,23(3):501-508
    [7] McGhee D S. A method for incorporating changing structural characteristics due to propellant mass usage in a launch vehicle ascent simulation[R].NASA/TM-2004-213,2004
    [8] Huang X, Zeiler T A.Dynamics of flexible launch vehicles with variable mass[R].AIAA-2006-826,2006
    [9] 邢誉峰,李敏. 计算固体力学原理与方法[M].北京:北京航空航天大学出版社,2011:51-59,218-223 Xing Yufeng,Li Min.The principle and method of computation solid mechanics[M].Beijing:Beihang University Press,2011: 51-59,218-223(in Chinese)
    [10] 邢誉峰,郭静. 与结构动特性协同的自适应Newmark方法[J].力学学报,2012,44(5):904-911 Xing Yufeng,Guo Jing.A self-adaptive newmark method with parameters dependent upon structural dynamic characteristics[J].Chinese Journal of Theoretical and Applied Mechanics,2012,44(5):904-911(in Chinese)
    [11] 邢誉峰,李敏. 工程振动基础[M].2版.北京:北京航空航天大学出版社,2011:72-88 Xing Yufeng,Li Min.Foundation of engineering vibration[M].2nd ed.Beijing:Beihang University Press,2011:72-88(in Chinese)
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出版历程
  • 收稿日期:  2013-07-04
  • 网络出版日期:  2014-06-20

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