期刊文献+

载荷参数和非线性因素对简支梁热振响应的影响分析

Analysis of the Effects of Load Parameters and Nonlinearity on the Thermo-Vibration Response of Simply Supported Beam
下载PDF
导出
摘要 本文建立了两端简支梁在热载荷作用下的运动方程。通过Galerkin离散,得到系统的前二阶常微分方程,并对其进行了热屈曲计算,对屈曲后的平衡点进行了稳定性分析。计算了简支梁在简谐激励下的热振响应,分析了热载荷、外激励频率、外激励幅值等系统参数对系统动力学行为的影响,讨论了非线性因素对振动响应的影响。 In this paper, the motion equation of the simply supported beam under thermal load is built. By Galerkin discretization method, the first two order differential equations are obtained. The thermal buckling of the beam and the stability of the balance points are analyzed. Additionally, a harmonic excitation is put on the beam. The thermo-vibration response of the beam is calculated. The effects of the thermal load, frequency and amplitude of the external excitation to the dynamical behavior of the beam are analyzed. And the dynamical behavior aroused by the nonlinear factors is discussed.
作者 秦朝红 任方 程昊 张忠 刘振皓 郭静 QIN Zhao-hong;REN Fang;CHEN Hao;ZHANG Zhong;LIU Zhen-hao;GUO Jing(Beijing Institute of Structure and Environment Engineering ,Beijing 100076,China)
出处 《强度与环境》 CSCD 2019年第2期7-12,共6页 Structure & Environment Engineering
基金 国家自然科学基金(编号:11402028 11502023 11502024)
关键词 简支梁 非线性 热振 热屈曲 稳定性 simply supported beam nonlinear thermal vibration thermal buckling stability
  • 相关文献

参考文献5

二级参考文献92

  • 1吴大方,赵寿根,晏震乾,赵星.巡航导弹防热部件热-振联合试验[J].航空动力学报,2009,24(7):1507-1511. 被引量:23
  • 2夏巍,杨智春.热环境下复合材料壁板的振动特性分析[J].应用力学学报,2005,22(3):359-363. 被引量:13
  • 3史晓鸣,杨炳渊.瞬态加热环境下变厚度板温度场及热模态分析[J].计算机辅助工程,2006,15(B09):15-18. 被引量:37
  • 4Blevins R D,Holehouse I,Wentz K R.Thermoacoustic loads and fatigue of hypersonic vehicle skin panels[J].Journal of Aircraft,1993,30(6):971-978.
  • 5Swanson A D,Coghlan S C,Pratt D M,et al.Hypersonic vehicle thermal test challenges[R].AIAA-2007-1670.
  • 6Clarkson B L.Review of sonic fatigue technology[R].NASA-N94-29407.
  • 7Mixson J S,Roussos L A.Acoustic fatigue:overview of activities at NASA Langley[R].NASA-N87-24965.
  • 8Leatherwood J D,Clevenson S A,Powell C A.et al.Acoustic testing of high-temperature panels[J].Journal of Aircraft,1992,29(6):1130-1136.
  • 9Bayerdoerfer G,Freyberg L.Thermoacoustic tests to quniify TPS-Design[C].ESA SP-386:591-596,1996.
  • 10Clevenson S A,Daniels E F.Capabilities of the thermal acoustic fatigue apparatus[R].NASA-N92-22212.

共引文献95

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部