销钉耳片连接件接触应力分析的能量解法

针对光滑无间隙的钉孔接触情况,根据圣维南原理,以耳片孔为中心取出一圆形区域,采用叠加原理将受力状态分解为对称和反对称状态,利用正交完备的三角级数和勒让德级数构造这两种受力状态的位移场.假设接触表面的载荷分布模态,由最小势能原理确定位移函数中的待定系数,得到耳片孔边的位移场和应力场.本文计算结果与有限元数值解比较显示:两...     

均匀热荷载作用下层合简支梁的弹性力学解

基于二维热弹性力学理论,研究均匀热荷载作用下层合简支梁的弹性力学解.首先导出均匀温度场中满足控制微分方程和两端简支边界条件的单层梁的弹性力学解,然后利用层间界面位移和应力必须连续的条件,递推得到底层梁与顶层梁间的位移和应力关系.最后根据层合梁上下表面的边界条件确定待定系数,带回递推公式得到整个层合梁的应力和位移分布.本文方法的计算结果有很好的收敛性.与有限元软件的结果对照说明了本文方法的精确性.最后,研究了不同的变温对层合简支梁的位移和应力的影响,结果显示每个层间界面在x方向的应力是不连续.随着温度的升高,梁的最大位移相应地增大.温度越高,位移沿厚度变化的速率越大.     

均布荷载作用下功能梯度简支梁弯曲的解析解

利用应力函数半逆解法,研究了均布载荷作用下、材料属性在厚度上任意变化的功能梯度简支梁弯曲的解析解,给出了各向应力应变与位移的解析显式表达式.首先根据平面应力状态的基本方程,得出了功能梯度梁的应力函数应满足的偏微分方程,并根据应力边界条件得出了各应力分布的表达式;进而根据功能梯度材料的本构方程和位移边界条件,得出了应变和位移的分布.最后,通过将本文的解退化到均质各向同性梁并与经典弹性解比较,证明了本文理论的正确性,并求解了材料组分呈幂律分布的功能梯度梁的应力和位移分布,分析了上下表层材料的弹性模量比λ与组分材料体积分数指数n对应力和位移分布的影响.     

航空材料梁弹塑性弯曲的近似封闭解

本文将材料的应力-应变曲线表示成包含奇次指数的幂函数多项式.将直梁弯曲正应力展成勒让德函数项级数,构造了一个包含无限多个待定系数的静力许可场.用余能原理确定其系数.给出了两种材料、两种截面、三种载荷梁的计算结果.结果表明:级数收敛性很好。从而,给出了相当精确的近似封闭解.     

考虑横法向热应变的C~0型整体-局部高阶层合梁理论

通过考虑横法向热变形,本文建立了预先满足层间应力连续的C0型整体-局部高阶层合梁理论,并用于分析复合材料层合梁热膨胀和热弯曲问题。虽然考虑了横法向应变,不增加额外的位移变量。此理论位移场不含有横向位移一阶导数,便于构造多节点高阶单元。基于虚功原理推导了复合材料层合梁平衡方程,并分析了简支多层复合材料梁热膨胀和热弯曲问题。数值结果表明,建立的模型能准确分析复合材料层合梁热膨胀和热弯曲问题,忽略横法向应变的理论分析热膨胀问题误差较大。     

界面裂纹问题的解析—变分解法及其在复合材料盖板胶接件中的应用

本文根据穆斯海里什维利求解各向同性平面问题与列赫尼兹基求解各向异性平面问题的广义复变函数理论与本征函数展开法,分析了复合材料盖板胶接件的分层问题,得到了精确满足所有基本方程、裂纹表面边界条件与层间连续条件的位移场与应力场本征展开式.进而利用分区广义变分原理满足裂纹表面以外的边界条件并由此确定应力强度因子.     

粘弹层合板的稳态振动和层间应力

应用混合分层理论和Ressiner混合变分原理，在板厚方向取二次位移插值函数和三次、四次横向应力插值函数推导出粘弹层合板的动力学方程，得出简支粘弹层合板稳态振动的解。不仅得出与三层弹性板精确的自振频率吻合良好的解，而且对于粘弹层合板，所计算的自振频率和结构损耗因子也与三维结果吻合较好。计算了自由阻尼层合板对应的低阶法向位移响应幅值和层问横向应力的幅值。结果表明，较高的层间横向正应力是低频稳态振动中引起粘弹层合板分层破坏的主要因素，采用适当模量和厚度的粘弹性材料将有效地降低粘弹层合板的层间横向正应力的幅值。     

压电层合梁静动力学分析的高精度梁单元

给出了一个对复合材料压电层合梁进行数值分析的高精度压电层合梁单元。基于Shi三阶剪切变形板理论的位移场和Layer-wise理论的电势场,用力-电耦合的变分原理及Hamilton原理推导了压电层合梁单元列式。采用拟协调元方法推导了一个可显式给出单元刚度矩阵的两节点压电层合梁单元,并应用于压电层合梁的力-电耦合弯曲和自由振动分析。计算结果表明,该梁单元给出的梁挠度和固有频率与解析解吻合良好,并优于其它梁单元的计算结果,说明了本文所给压电层合梁单元的可靠性和准确性。研究结果可为力-电耦合作用下压电层合梁的力学分析提供一个简单、精确且高效的压电层合梁单元。     

考虑界面损伤层合梁板的层间应力分析

基于精确应力分析的广义六自由度板理论，应用变分原理和损伤力学中 的应变等效原理，考虑复合材料铺设层内和层间界面处的损伤效应，建立了具两种损伤模式 的复合材料层合板的三维非线性平衡微分方程，且运用有限差分法对考虑损伤简支层合梁板 的层间应力进行了求解.     

扩展的Hellinger-Reissner原理及特殊层合杂交应力元

建立了一种非匀质材料新的、扩展的Hellinger-Reissner原理,发展了当一个单元域划分为不同材料特性子域、其元内应力场沿子域表面不连续、且位移场在子域表面也急剧变化时,一个非匀质有限元刚度列式便利方法。这种列式亦可用于对每层横向剪应变均独立处置的厚层板。基于此变分原理建立了新的具有一个无外力圆柱表面的层合杂交应力元,单元各层独立假定的应力场通过以自然坐标表示的非协调位移为权函数使齐次平衡方程变分满足的理性方法及严格满足给定圆柱面上无外力条件得到,位移场在元间及层间连续条件则分别通过Lagrange乘子进行了松弛。数值算例表明：这类新型元可有效地分析具有多类圆柱形槽孔的厚、中厚及薄层板自由孔边应力分布。     

NONLINEAR THREE-DIMENSIONAL ANALYSIS OF COMPOSITELAMINATED PLATES

ＮＯＮＬＩＮＥＡＲＴＨＲＥＥ－ＤＩＭＥＮＳＩＯＮＡＬＡＮＡＬＹＳＩＳＯＦＣＯＭＰＯＳＩＴＥＬＡＭＩＮＡＴＥＤＰＬＡＴＥＳ￥(江晓禹，张相周，陈百屏)ＪｉａｎｇＸｉａｏｙｕ；（ＳｏｕｔｈｗｅｓｔｅｒｎＪｉａｏｔｏｎｇＵｎｉｖｅｒｓｉｔｙ，Ｃｈｅｎｇｄｕ６...     

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.     

复合材料叠层梁和金属梁的固有振动特性

对根据三种梁理论得到的金属梁和复合材料叠层梁的固有振动特性进行了对比性的研究对常用的三种梁理论在弹性碰撞分析中的应用进行了分析和比较     

Global Constraints for Stress Constrained Materials: The Problem of Saint Venant

Based on the global constraint principle of Antman and Marlow, a new solution of Saint Venant's problem is proposed. The solutions for the six fundamental cases of loading in terms of stress are obtained with relative ease and converge to the classical Saint Venant's solution as the length of the beam is increased. It is also shown that the assumptions of a special technical rod theory are coherent with the requirements of the global constraint theory for the Saint Venant cylinder.     

含椭圆刚性核有限大复合材料层板弯曲应力分析Bending problem of a finite composite laminated plate with elliptical rigid inclusions

基于经典的复合材料层板理论,将有限大复合材料层板等效成各向异性弹性平板。采用复变函数理论中的Faber级数分析方法,使用最小二乘边界配点法,对含多椭圆刚性核有限大各向异性板弯曲问题进行应力分析,得到了该问题的级数解形式,分析了含椭圆刚性核层板在弯曲载荷下的应力分布,并讨论了形状和结构参数对应力分布的影响。结果表明,本文方法对于分析含多个椭圆形刚性核有限大薄板弯曲应力问题非常有效,该方法具有精度高及计算方便等优点。     

A BEM solution to transverse shear loading of composite beams

In this paper a boundary element method is developed for the solution of the general transverse shear loading problem of composite beams of arbitrary constant cross-section. The composite beam consists of materials in contact, each of which can surround a finite number of inclusions. The materials have different elasticity and shear moduli with same Poisson’s ratio and are firmly bonded together. The analysis of the beam is accomplished with respect to a coordinate system that has its origin at the centroid of the cross-section, while its axes are not necessarily the principal ones. The transverse shear loading is applied at the shear centre of the cross-section, avoiding in this way the induction of a twisting moment. Two boundary value problems that take into account the effect of Poisson’s ratio are formulated with respect to stress functions and solved employing a pure BEM approach, that is only boundary discretization is used. The evaluation of the transverse shear stresses is accomplished by direct differentiation of these stress functions, while both the coordinates of the shear center and the shear deformation coefficients are obtained from these functions using only boundary integration. Numerical examples with great practical interest are worked out to illustrate the efficiency, the accuracy and the range of applications of the developed method. The accuracy of the proposed shear deformation coefficients compared with those obtained from a 3-D FEM solution of the ‘exact’ elastic beam theory is remarkable.     

粘弹性夹心夹层结构卸载后的裂纹持续扩展现象研究

以聚氨酯弹性体钢夹层板为研究对象,对其进行了三点弯曲实验,对不同类型试件的实验结果进行了总结。实验发现,在加载过程中,在弯曲挠度超过一定程度时,夹层板结构的角点位置出现开裂,由于层间强度不足和夹心材料的粘弹性性质,卸载后裂纹会在一段时间内沿层间继续发生扩展,最后导致整个面板发生脱粘或夹心撕裂。针对这一现象,以弹性地基梁理论为基础,计算了上下面板的挠度差异,并使用层间粘结强度来分析试件的临界状态,获得了软夹芯试件和硬夹芯试件的临界破坏的裂纹长度。结果表明,使用层间粘结强度分析方法,获得的结果都能够描述聚氨酯弹性体钢夹层板的层间延迟破坏的特点。     

An analytic solution of transversal oscillation of quintic non-linear beam with homotopy analysis method

non-linear vibration analysis of beam used in steel structures is of particular importance in mechanical and industrial applications. To achieve a proper design of the beam structures, it is essential to realize how the beam vibrates in its transverse mode which in turn yields the natural frequency of the system. Equation of transversal vibration of hinged–hinged flexible beam subjected to constant excitation at its free end is identified as a non-linear differential equation. The quintic non-linear equation of motion is derived based on Hamilton’s principle and solved by means of an analytical technique, namely the Homotopy analysis method. To verify the soundness of the results, a comparison between analytical and numerical solutions is developed. Finally, to express the impact of the quintic nonlinearity, the non-linear responses obtained by HAM are compared with the results from usual beam theory.     

Size-dependent free vibration analysis of composite laminated Timoshenko beam based on new modified couple stress theory

A micro-scale free vibration analysis of composite laminated Timoshenko beam (CLTB) model is developed based on the new modified couple stress theory. In this theory, a new anisotropic constitutive relation is defined for modeling the CLTB. This theory uses rotation–displacement as dependent variable and contains only one material length scale parameter. Hamilton’s principle is employed to derive the governing equations of motion and boundary conditions. This new model can be reduced to composite laminated Bernoulli–Euler beam model of the couple stress theory. An example analysis of free vibration of the cross-ply simply supported CLTB model is adopted, and an explicit expression of analysis solution is given. Additionally, the numerical results show that the present beam models can capture the scale effects of the natural frequencies of the micro-structure.