脱层梁屈曲的高阶剪切理论

脱层的存在将会大大降低层合结构的屈曲载荷。该文将含任意位置脱层的两端固支梁分成多段子层,用厚度的三次多项式模拟脱层梁屈曲时子层的轴向位移,利用变分原理和欧拉方程导出了脱层梁的屈曲方程和定解条件,并用状态空间方法进行求解。通过与一阶剪切理论和经典理论的比较,指出了它们各自的适用范围;考虑了脱层梁三种不同的屈曲模态。分析了脱层长度、深度、位置和材料的铺层方向对脱层梁屈曲载荷的影响;最后给出了多处简单脱层的屈曲分析。     

基于高阶梁理论的功能梯度材料自由振动分析

本文基于一种新型的高阶梁理论,研究了功能梯度材料梁的自由振动问题。首先对该新型高阶梁理论进行了介绍,然后对该理论进行了有限元实现,并利用Hamilton原理推导得到了离散的动力学平衡方程,构造了2节点8自由度的C1型高阶梁单元。参照文献作了均质悬臂梁的模态分析,验证了该梁单元的精度。然后利用该单元进行功能梯度梁的模态分析,并构造了一种材料相关性很弱的无量纲固有频率。由该无量纲固有频率引入了功能梯度梁与均质梁固有频率之间的转换关系,并通过算例分析了该转换关系的适用条件。     

反应烧结Si3N4陶瓷断裂韧性的实验研究

本文对反应烧结氦化硅 Si_3N_4陶瓷的断裂韧性进行实验研究,用三种不同试件进行了测试,这三种试件是:山形切口双悬臂粱试件,山形切口三点弯曲梁试件和直穿透切口三点弯曲梁试件.用有限元方法分析了直穿透切口三点弯曲梁切口宽度对应力强度因子的影响,结合断裂载荷测定值估算了材料的断裂韧性值,指出直切口无预制裂纹试件的测定值必须用有限元法进行修正才能得到正确结果.     

多孔功能梯度材料Timoshenko梁的自由振动分析

基于Timoshenko梁理论研究多孔功能梯度材料梁(FGMs)的自由振动问题.首先,考虑多孔功能梯度材料梁的孔隙率模型,建立了两种类型的孔隙分布.其次,基于Timoshenko梁变形理论,给出位移场方程、几何方程和本构方程,利用Hamilton原理推导多孔功能梯度材料梁的自由振动控制微分方程,并进行无量纲化,然后应用微分变换法(DTM)对无量纲控制微分方程及其边界条件进行变换,得到含有固有频率的等价代数特征方程.最后,计算了固定-固定(C-C)、固定-简支(C-S)和简支-简支(S-S)三种不同边界下多孔功能梯度材料梁自由振动的无量纲固有频率.将其退化为均匀材料与已有文献数据结果对照,验证了正确性.讨论了孔隙率、细长比和梯度指数对多孔功能梯度材料梁无量纲固有频率的影响.     

深梁理论的研究现状与工程应用

综述了深梁理论、截面剪切修正系数计算理论、深梁线性与几何非线性有限元、深梁材料非线性分析、深梁振动理论、深梁稳定理论、箱梁结构分析中弯曲、剪力滞、畸变分析时考虑剪切变形影响的计算理论、钢腹板桥梁考虑剪切变形的研究成果、弹性地基深梁、深梁理论在工程结构中的应用等. 提出了杆系结构的静力、振动和稳定分析方法都可用Timoshenko 深梁理论进行重建和重写.     

功能梯度材料梁自由振动的线性与非线性振动

基于数值模拟和理论分析两种方法,研究了功能梯度材料(functional gradient materials,FGM)梁自由振动下的线性与非线性振动问题。通过解析法求解了FGM梁在经典理论下以及一阶剪切理论下的力学行为,得到了FGM梁在简支和固端约束下的固有频率。理论分析了不同边界条件、不同梁理论下、梯度指数、长细比等因素对于FGM梁固有频率的影响;不论经典梁理论还是一阶剪切理论,随着梯度指数的增加,FGM梁的固有频率都随之减小。通过ABAQUS仿真模拟,得到FGM梁数值模拟下的非线性固有频率。将理论解与数值解进行对比,完善力学模型。在多种理论下,利用解析法和数值模拟的方法,给出FGM梁结构振动响应的线性与非线性解。     

基于近场动力学的梁结构振动特性分析方法研究

基于欧拉梁理论推导了两自由度梁的常规态型近场动力学（Peridynamics,PD）模型,并提出一种新的自由边界条件施加方法,对不同边界条件的PD梁进行了模态分析,与局部梁的有限元结果进行了对比,验证了模型的收敛性,分析了PD非局部参数对固有频率的影响。结果表明,当近场作用域内物质点密度较小时,PD梁模型非局部性较弱,与局部梁的有限元结果接近,随着物质点密度逐渐增大,非局部作用增强,PD梁的固有频率逐渐降低;当尺度参数趋于零时,PD梁的固有频率收敛到局部梁的有限元解,PD梁退化为局部梁。研究表明,本文提出的PD梁模型和自由边界施加方法适用于分析梁的振动特性,为采用PD方法分析梁结构的动力特性提供了参考。     

梁在几种典型载荷作用下的弹性力学求解方法

梳理了针对梁在典型载荷作用下三种代表性求解方法,基于均布载荷作用下梁问题的解答,给出了梁受梯度分布载荷作用下的求解方法。将梁模型与复合材料力学相关联,加深了学生对弹性理论的理解。基于叠加原理,给出了具有复杂受载情况下梁的分析方法,拓展了学生对理论应用的认识,具有一定的工程应用价值和教学实践意义。     

固体力学中的统一分析梁与有限节线法

针对现有梁理论不能解决的杆状类工程结构构件和结构体系,本文提出了一种新的梁模型——统一分析梁与一种新的数值分析方法——有限节线法。利用统一分析梁和有限节线法不仅可以解决任意杆状类结构构件或结构体系的力学分析问题,而且当问题的性质与传统梁理论的前提条件一致时,会得出同样精度的解答。算例计算结果证明了统一分析梁的合理性与有限节线法的正确性。     

作大范围运动弹性梁刚—柔耦合动力学建模

利用弹性梁的变形理论和 Hamilton力学原理对作大范围运动弹性梁的刚 -柔耦合动力学建模理论进行了研究。分析了大范围运动对弹性梁的横向振动和纵向振动的影响 ,得到了大范围运动与弹性梁的中线耦合变形之间的耦合作用对该系统动力学性质有显著的影响 ,从而提出了作大范围运动弹性梁的刚柔耦合动力学模型     

Vibration analysis of a stepped laminated composite Timoshenko beam

The goal of this study is to investigate the vibration characteristics of a stepped laminated composite Timoshenko beam. Based on the first order shear deformation theory, flexural rigidity and transverse shearing rigidity of a laminated beam are determined. In order to account for the effect of shear deformation and rotary inertia of the stepped beam, Timoshenko beam theory is then used to deduce the frequency function. Graphs of the natural frequencies and mode shapes of a T300/970 laminated stepped beam are given, in order to illustrate the influence of step location parameter exerts on the dynamic behavior of the beam.     

Coupled bending and torsional vibration of nonsymmetrical axially loaded thin-walled Bernoulli–Euler beams

The dynamic transfer matrix is formulated for a straight uniform and axially loaded thin-walled Bernoulli–Euler beam element whose elastic and inertia axes are not coincident by directly solving the governing differential equations of motion of the beam element. Bernoulli–Euler beam theory is used, and the cross section of the beam does not have any symmetrical axes. The bending vibrations in two perpendicular directions are coupled with torsional vibration and the effect of warping stiffness is included. The dynamic transfer matrix method is used for calculation of exact natural frequencies and mode shapes of the nonsymmetrical thin-walled beams. Numerical results are given for a specific example of thin-walled beam under a variety of end conditions, and exact numerical solutions are tabulated for natural frequencies and solutions calculated by the other method are also tabulated for comparison. The effects of axial force and warping stiffness are also discussed.     

Dynamic stability analysis of shear-flexible composite beams

Dynamic stability behavior of the shear-flexible composite beams subjected to the nonconservative force is intensively investigated based on the finite element model using the Hermitian beam elements. For this, a formal engineering approach of the mechanics of the laminated composite beam is presented based on kinematic assumptions consistent with the Timoshenko beam theory, and the shear stiffness of the thin-walled composite beam is explicitly derived from the energy equivalence. An extended Hamilton’s principle is employed to evaluate the mass-, elastic stiffness-, geometric stiffness-, damping-, and load correction stiffness matrices. Evaluation procedures for the critical values of divergence and flutter loads of the nonconservative system with and without damping effects are then briefly introduced. In order to verify the validity and the accuracy of this study, the divergence and flutter loads are presented and compared with the results from other references, and the influence of various parameters on the divergence and flutter behavior of the laminated composite beams is newly addressed: (1) variation of the divergence and flutter loads with or without the effects of shear deformation and rotary inertia with respect to the nonconservativeness parameter and the fiber angle change, (2) influence of the internal and external damping on flutter loads whether to consider the shear deformation or not.     

Axial-flexural coupled vibration and buckling of composite beams using sinusoidal shear deformation theory

A finite element model based on sinusoidal shear deformation theory is developed to study vibration and buckling analysis of composite beams with arbitrary lay-ups. This theory satisfies the zero traction boundary conditions on the top and bottom surfaces of beam without using shear correction factors. Besides, it has strong similarity with Euler–Bernoulli beam theory in some aspects such as governing equations, boundary conditions, and stress resultant expressions. By using Hamilton’s principle, governing equations of motion are derived. A displacement-based one-dimensional finite element model is developed to solve the problem. Numerical results for cross-ply and angle-ply composite beams are obtained as special cases and are compared with other solutions available in the literature. A variety of parametric studies are conducted to demonstrate the effect of fiber orientation and modulus ratio on the natural frequencies, critical buckling loads, and load-frequency curves as well as corresponding mode shapes of composite beams.     

Generalized variational principle of dynamic analysis on naturally curved and twisted box beams for anisotropic materials

An incomplete generalized variational functional for naturally curved and twisted composite box beams with complete constrained boundaries at two ends is established by means of Lagrange multiplier method. The equations of motion governing the dynamic behavior of the beams and corresponding boundary conditions are derived from the stationary condition of the functional. The non-classical influences relevant to the beams are those due to transverse shear deformations, torsion-related warping and several elastic couplings that can arise in composite beams. In order to demonstrate the correctness of the theory developed the natural frequencies and normal mode shapes of the beams under in-plane free vibration are evaluated and compared with the results using PATRAN’s beam elements.     

Free vibration characteristics of sectioned unidirectional/bidirectional functionally graded material cantilever beams based on finite element analysis

Advancements in manufacturing technology, including the rapid development of additive manufacturing (AM), allow the fabrication of complex functionally graded material (FGM) sectioned beams. Portions of these beams may be made from different materials with possibly different gradients of material properties. The present work proposes models to investigate the free vibration of FGM sectioned beams based on onedimensional (1D) finite element analysis. For this purpose, a sample beam is divided into discrete elements, and the total energy stored in each element during vibration is computed by considering either the Timoshenko or Euler-Bernoulli beam theory. Then, Hamilton's principle is used to derive the equations of motion for the beam. The effects of material properties and dimensions of FGM sections on the beam's natural frequencies and their corresponding mode shapes are then investigated based on a dynamic Timoshenko model (TM). The presented model is validated by comparison with three-dimensional (3D) finite element simulations of the first three mode shapes of the beam.     

Initial value method for free vibration of axially loaded functionally graded Timoshenko beams with nonuniform cross section

Free vibration of nonuniform axially functionally graded Timoshenko beams subjected to combined axially tensile or compressive loading is studied. An emphasis is placed on the effect of tip and distributed axial loads on the natural frequencies and mode shapes for an inhomogeneous cantilever beam including material inhomogeneity and geometric non-uniform cross section. The initial value method is developed to determine the natural frequencies. The method’s effectiveness is verified by comparing our results with previous ones for special cases. Natural frequencies of standing/hanging Timoshenko beams are calculated for four different cross sections. The influences of shear rigidity, taper ratio, gradient index, tip force, and axially distributed loading on the natural frequencies of clamped-free beams are discussed. Material inhomogeneity and geometric non-uniform cross-section strongly affect higher-order vibration frequencies and mode shapes.     

Free vibration analyses of axially loaded laminated composite beams based on higher-order shear deformation theory

The dynamic stiffness matrix method is introduced to solve exactly the free vibration and buckling problems of axially loaded laminated composite beams with arbitrary lay-ups. The Poisson effect, axial force, extensional deformation, shear deformation and rotary inertia are included in the mathematical formulation. The exact dynamic stiffness matrix is derived from the analytical solutions of the governing differential equations of the composite beams based on third-order shear deformation beam theory. The application of the present method is illustrated by two numerical examples, in which the effects of axial force and boundary condition on the natural frequencies, mode shapes and buckling loads are examined. Comparison of the current results to the existing solutions in the literature demonstrates the accuracy and effectiveness of the present method.     

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研制和开发了曲梁以及复合曲梁测量应力的创新实验装置, 通过该实验的设计、开发和应用,可以验证它的创新性和综合性,找出曲梁、复合曲梁与直 梁的诸多不同之处. 把该实验用于测试由钢制成的、钢与铜两种材料制成的,具有直角梯形 截面的简支梁在拱顶处受垂直集中力作用时的正应力和切应力,计算结果表明,理论解和实 验值吻合得很好.     

GEOMETRICALLY NONLINEAR FINITE ELEMENT MODEL OF SPATIAL THIN-WALLED BEAMS WITH GENERAL OPEN CROSS SECTION

Based on the theory of Timoshenko and thin-walled beams, a new finite element model of spatial thin-walled beams with general open cross sections is presented in the paper, in which several factors are included such as lateral shear deformation, warp generated by nonuni- form torsion and second-order shear stress, coupling of flexure and torsion, and large displacement with small strain. With an additional internal node in the element, the element stiffness matrix is deduced by incremental virtual work in updated Lagrangian （UL） formulation. Numerical examples demonstrate that the presented model well describes the geometrically nonlinear property of spatial thin-walled beams.