大变形薄壁复合材料旋转梁静动态特性分析

该文研究了大变形薄壁复合材料旋转梁的静、动态特性以及复合材料旋转梁不同铺层角、转速对固有频率的影响变化规律。在梁截面上设立翘曲节点引入翘曲变形,假设应变沿薄壁厚度呈二次曲线形式变化;由Hamilton原理,推导了复合材料梁的大变形公式;建立了考虑剪切、翘曲薄壁复合材料大变形梁静、动态分析的有限元模型,并编写了相应的计算程序。分析了复合材料薄壁梁大变形状态下的静态变形行为;在旋转状态下,考虑哥氏力影响,不同转速、不同铺层角对复合材料梁动态特性的影响。计算结果表明:能够用该文建立的模型计算复合材料梁的静动态特性,与相关文献计算结果进行比较,说明了模型的优越性。     

空间薄壁截面梁非线性有限单元模型

基于Timoshenko梁理论和Vlasov薄壁杆件理论,通过设置单元内部节点并对弯曲转角和翘曲角采取独立插值的方法,建立了可考虑横向剪切变形和扭转剪切变形及其耦合作用、弯扭耦合、以及二次剪应力影响的空间薄壁梁非线性有限元模型。以更新的拉格朗日格式描述的几何非线性应变推得几何刚度矩阵。同时考虑了材料非线性,假定材料为理想塑性体,服从Von Mises屈服准则和Prandtle-Reuss增量关系,采用有限分割法,由数值积分得到空间薄壁梁的弹塑性刚度矩阵。算例表明该文所建梁单元模型具有良好的精度,适用于空间薄壁结构的有限元分析。     

基于Timoshenko梁理论的薄壁梁弯扭耦合分析

该文主要以截面形心与剪切中心不重合的等截面空间薄壁梁为研究对象。以Timoshenko梁理论和薄壁杆件理论为基础,考虑横向剪切变形以及横向剪力和二次剪应力所产生的翘曲,将转角位移和翘曲位移采取独立插值,利用虚功原理推导出薄壁截面空间梁元的弯扭耦合刚度矩阵。算例表明:所建立的模型具有很好的精度,满足工程应用;当截面有非对称轴时,计算须考虑弯扭耦合的影响。     

考虑剪滞效应的薄壁曲梁有限单元法

本文以最小势能原理为基础,考虑剪力滞后效应和翘曲扭转(包括二次翘曲剪切)的影响提出了一种用于分析单室或多室曲线薄壁箱型梁桥力学特性的曲梁单元,推导了单元刚度矩阵、等效节点荷载列阵。作为验证,在算例中对一双室曲线薄壁箱型梁模型的静力特性进行了分析,并将本文数值结果与试验结果和板壳有限元方法所得结果进行比较后证明了本文方法是有效的。     

复合材料变截面旋转薄壁悬臂梁自由振动分析

基于拉格朗日方程推导出复合材料封闭变截面旋转薄壁梁的自由振动方程。与基于哈密顿原理的动力学建模方法相比,该文所采用的方法更为简洁。此外,在薄壁梁的结构模型中还考虑除横向剪切外的扭转、拉伸和弯曲引起的翘曲,具有考虑翘曲因素多的特点。给出了两种刚度配置下的变矩形截面旋转悬臂直梁的自由振动方程简化形式及其相应的迦辽金法求解的固有频率。基于大型通用有限元软件ANSYS,计算了薄壁变截面旋转悬臂梁的固有频率,并且与迦辽金法的求解结果进行了对比。分析了复合材料的弹性耦合、铺层角度、截面变化和旋转速度对薄壁梁的自由振动的影响。     

箱形柱与工字梁连接节点翘曲变形的传递分析

箱形柱与工字形梁刚性连接节点是钢结构建筑中最常用的节点形式之一.通过对采用这种节点形式的梁柱节点处的梁柱构件之间的翘曲位移传递的研究,提出了这种节点处梁柱的翘曲位移的简单关系,并推导了在常用薄壁构件空间框架梁单元有限元模型中的实现方法.通过与壳体单元有限元的分析结果进行比较,发现壳体有限元与提出的方法结果非常吻合,同时...     

基于协调翘曲场的开闭口混合薄壁截面杆件约束扭转一维有限元分析

开口及闭口薄壁杆件约束扭转问题已由经典Timoshenko和Benscoter理论解决。然而,开闭口混合薄壁截面杆件约束扭转分析必须考虑开、闭口部分翘曲能力的差异,翘曲剪流形成机理有待进一步研究。该文假定开、闭口截面翘曲分别满足Vlasov和Umanskii假定,考虑开、闭口截面公共节点翘曲连续性要求,建立含有待定翘曲参数的协调翘曲模型。由截面受力平衡,确定翘曲参数显式列式,提出开闭口混合薄壁截面杆件约束扭转分析的一维有限元模型。算例及参数分析结果表明,基于Umanskii第二理论的I类方法在悬臂板及闭口周边引入附加剪流,影响翘曲剪应力精度。基于Umanskii第二理论的II类方法只能计算截面板件平均剪应力,无法反映真实翘曲剪流分布。基于Vlasov约束扭转假定的Beam-189单元忽略闭口周边约束效应产生的附加翘曲及剪流,影响翘曲正应力和剪应力精度。该文方法与Shell-63单元能得到基本吻合的变形与应力结果,说明一维梁元能正确反映开闭口混合薄壁截面杆件约束扭转及翘曲刚度。     

考虑主材节点刚域影响的钢管输电塔变截面梁单元有限元模型

为了准确、快捷地计算加劲板和连接板形成的主材节点刚域对输电塔受力的影响,将考虑节点刚域影响的主材视为若干段段不同截面梁单元的组合。首先,推导了主材两端节点刚域横截面转动惯量和面积的公式;然后,根据能量原理,推导了变截面梁单元的单元刚度矩阵,并采用C++语言将它引入开源有限元软件OpenSees;最后,将主材及节点刚域采用变截面梁单元,常截面梁单元,变弹性模量梁单元及壳单元离散的有限元模型计算结果和塔架试验的实测结果进行对比。结果表明:常截面梁单元会低估主材的弯矩和最大正应力,而变弹性模量梁单元会低估输电塔的挠度,均会使设计偏于不安全;变截面梁单元和壳单元的计算结果均实测结果很接近,但前者计算量远小于后者。可见:变截面梁单元有限元模型兼顾了计算效率和精度。     

异形截面木塑复合材料托盘的数值模拟与实验对比分析

利用有限元数值仿真技术,研究了具有异形截面的木塑复合材料托盘的承载能力。采用自定义截面梁单元建立木塑复合材料的异型截面梁模型;基于该异形截面梁模型,建立了托盘有限元模型,并进行承载能力计算;最后将数值计算结果与实验结果进行对比分析。研究结果表明：数值分析结果与实验结果有比较好的一致性;数值分析方法的计算精度满足实际工程需要。该方法用于具有复杂截面形状的木塑复合材料及制品的研究与开发,能节约实验及研发成本、缩短研发周期。     

框架梁柱节点处双力矩与翘曲位移的关系

对于薄壁构件框架结构的梁柱节点处翘曲未知量之间的转换,软件ANSYS和ABAQUS采用了错误的做法。该文把节点域梁柱翼缘和加劲肋看成井字梁系,考虑它们在框架平面外的弯曲和扭转,通过翼缘板件内力和位移与杆件截面内力和位移的关系,得到了节点域与杆件的四个连接面上双力矩和翘曲位移的关系。对 形框架进行了算例分析,与板壳有限元计算结果进行了对比,验证了得到的翘曲半刚性公式的正确性。通过算例也验证了梁柱节点处柱子翘曲位移与梁翘曲位移近似存在着相等相反的关系。     

On the importance of cross-sectional warping in solid composite beams

The relative importance of the cross-sectional warping components in composite beams is studied and demonstrated using an exact solution for solid orthotropic beam of arbitrary cross-sectional geometry that undergoes a bending moment. In light of the effort required for warping modeling in general numerical schemes of composite beams, the present study contributes to the understanding of the importance of modeling the in-plane and the out-of-plane warping components.     

复合材料薄壁梁力学特性分析

综述了人们在建立研究复合材料薄壁梁力学特性的非线性梁理论及分析结构剖面特性,确立结构算子参数等方面所做的工作以及这些研究工作的特点。同时,结合作者的工作,介绍了近年来各国学者在复合材料薄壁梁力学特性研究上的进展。      

不规则I型和L型横截面形状薄壁杆件的横向弯曲稳定分析

根据势能驻值原理,采用转换B3样条函数模拟杆件横截面的翘曲位移场,文[8]提出了用于分析在横向荷载作用下薄壁杆件稳定问题的样条有限杆元法。方法适用于任意横截面形状和任意边界条件的薄壁杆件,考虑了杆壁中面上剪切变形的影响,能很好地描述剪力滞后现象。本文讨论了不规则I型截面简支梁和L型截面简支梁的屈曲分析,数值算例的结果表明了方法的灵活性、精确性和有效性。     

On sixfold coupled vibrations of thin-walled composite box beams

This paper presents a general analytical model for free vibration of thin-walled composite beams with arbitrary laminate stacking sequences and studies the effects of shear deformation over the natural frequencies. This model is based on the first-order shear-deformable beam theory and accounts for all the structural coupling coming from the material anisotropy. The seven governing differential equations for coupled flexural–torsional–shearing vibration are derived from the Hamilton’s principle. The resulting coupling is referred to as sixfold coupled vibration. Numerical results are obtained to investigate the effects of fiber angle, span-to-height ratio, modulus ratio, and boundary conditions on the natural frequencies as well as corresponding mode shapes of thin-walled composite box beams.     

An improved model for naturally curved and twisted composite beams with closed thin-walled sections

This paper presents an improved model for naturally curved and twisted anisotropic beams with closed thin-walled cross-sections. By introducing eigenwarping functions and expanding axial displacements in series of eigenwarpings, the differential equation involving the generalized warping coordinate and the expression for eigenvalues can be derived using the principle of minimum potential energy. In the model the effects of some factors such as the initial curvature, torsion of the beams as well as torsion-related warping, transverse shear deformations and elastic coupling are incorporated. As an application, the present model is adopted to do an analysis for closed thin-walled composite box beams. Comparison with the existing experimental observation and numerical results shows that the proposed model is valid for analyzing such naturally curved and twisted beams.     

On a moderate rotation theory of thin-walled composite beams

A small strain and moderate rotation theory of laminated composite thin-walled beams is formulated by generalizing the classical Vlasov theory of sectorial areas. The proposed beam model accounts for axial, bending, torsion and warping deformations and allows one to predict critical loads and initial post-buckling behaviour. A finite element approximation of the theory is also carried out and several numerical applications are developed with reference to lateral buckling of composite thin-walled members. The sensitivity of critical load to second-order effects in the pre-buckling range is pointed out.     

A hybrid force/stiffness matrix method for the analysis of thin-walled composite frames

A novel method for the analysis of frames constructed of thin-walled members of anisotropic composite materials is presented in this paper. The method accounts for non-isotropic coupling effects that exist in composite material beams due to the anisotropy of the composite material laminates that form the thin-walled cross section. The method also accounts for warping effects known to be significant in thin-walled members. The analysis is performed by the direct stiffness matrix method utilizing a new approach that divides each thin-walled member of the frame into one-dimensional warping-beam superelements and non-warping conventional beam elements. The element stiffness matrices for these two one-dimensional beam elements are obtained by a numerical procedure that is based on the classical force method analysis. The stiffness matrices of both beam elements are 12 × 12 matrices corresponding to the six degrees of freedom per node required for conventional space frame analysis. The remarkable feature of this representation is that warping is accounted for without introducing additional degrees of freedom to account for the bimoment and warping twist in the members. This is accomplished by use of the warping-beam superelement that linearizes the regions of non-uniform torsion in the thin-walled beam. Examples of space frame structures constructed of thin-walled composite material I-beams are presented to demonstrate the method. Results of analyses using the proposed method are compared with those obtained from two-dimensional finite element models.