期刊文献+

复合材料梁的几何精确非线性建模及非经典效应 被引量:1

Geometrically exact nonlinear modeling and non-classical effect influence of composite beams
原文传递
导出
摘要 基于Hodges的广义Timoshenko梁理论对具有任意剖面形状、任意材料分布及大变形的复合材料梁进行几何精确非线性建模,采用旋转张量分解法计算梁内任意一点的应变,采用变分渐近法确定梁剖面的任意翘曲,采用平衡方程由二次渐近精确的应变能导出广义Timoshenko应变能,采用广义Hamilton原理建立梁的几何精确非线性运动方程。将所建模型用于复合材料梁的静动力分析,通过与实验数据的对比,验证了建模方法的准确性,并进一步研究了剖面翘曲及横向剪切变形非经典效应对复合材料梁的影响。研究表明,剖面翘曲对复合材料梁的静变形和固有频率有显著影响,横向剪切变形对复合材料梁的静变形和固有频率的影响与梁的长度/剖面高度比有关。 The geometrically exact nonlinear modeling of composite beam with arbitrary cross sectional shape,generally anisotropic material behavior and large deflection had been presented,based on the generalized Timoshenko beam theory of Hodges.The concept of decomposition of rotation tensor was used to calculate the strains in the beam.The variational asymptotical method was used to determine the arbitrary warping of the beam cross section.The generalized Timoshenko strain energy was derived from the equilibrium equations and the second-order asymptotically correct strain energy.The geometrically exact nonlinear equations of motion were established by the Hamilton's generalized principle.The established modeling was used for the static and dynamic analysis of composite beams and was verified by the comparisons with experimental data.The influences of the non-classical effects such as the cross sectional warping and the transverse shear deformation on the composite beams were investigated.The results indicate that the cross sectional warping has significant influences on the static deformation and the natural frequencies of the composite beams,and the influences of the transverse shear deformation on the static deformation and the natural frequencies of the composite beams are related to the length to depth ratio of the beam.
出处 《复合材料学报》 EI CAS CSCD 北大核心 2018年第1期218-228,共11页 Acta Materiae Compositae Sinica
基金 国家自然科学基金(11572150)
关键词 复合材料梁 几何精确 非经典效应 翘曲 横向剪切变形 composite beam geometrically exact non-classical effect warping transverse shear deformation
  • 相关文献

参考文献3

二级参考文献39

  • 1向锦武,张呈林,王适存.低振动旋翼桨叶的动力学优化设计[J].航空动力学报,1996,11(2):125-128. 被引量:13
  • 2尹维龙,向锦武.考虑剪切和翘曲影响的直升机旋翼气弹稳定性分析[J].航空学报,2006,27(6):1130-1134. 被引量:3
  • 3Hong C H,Chopra I.Aeroelastic stability analysis of a composite rotor blade[J].Journal of the American Helicopter Society,1985,30(2):57-67.
  • 4Panda B,Chopra I.Dynamics of composite rotor blades in forward flight[J].Vertica,1987,11(1/2):107-209.
  • 5Yuan K A,Friedmann P P.Venkatesan C.Aeroelastic behavior of composite rotor blades with swept tips[C] //48th Annual Forum of the AHS.Alexandria:AHS,1992:1039-1059.
  • 6Smith E C,Chopra I.Aeroelastic response and blade loads of a composite rotor in forward flight,AIAA-92-2566-CP[R].New York:AIAA,1992.
  • 7Friedmann P P,Yuan K A.Terlizzi M D.An aeroelastic model for composite rotor blades with straight and swept tips Ⅰ:Aeroelastic stability in hover[J].International Journal of Non -linear Mechanics,2002,37(1):967-986.
  • 8Sivaneri N T,Chopra I.Finite element analysis for bearingless rotor blade aeroelasticity[J].Journal of the American Helicopter Society,1984,29(2):42-51.
  • 9Smith E C.Vibration and flutter of stiff-inplane elastically tailored composite rotor blades,AIAA-93-1302[R].New York:AIAA,1993
  • 10Hong C H,Chopra I.Aeroelastic stability analysis of a composite rotor blade[J].Journal of the American Helicopter Society,1985,30(2):57-67.

共引文献9

同被引文献8

引证文献1

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