三边简支一边自由混凝土矩形薄板的热弯曲

基于薄板的小挠度理论和叠加原理,考虑横向变温情况,将温度作用下的三边简支一边自由矩形薄板看作是面内温差作用下的四边简支矩形薄板和自由边上挠度作用下的三边简支一边自由矩形薄板的叠加,得到了温度作用下三边简支一边自由混凝土矩形薄板的挠度和弯矩解析解.首先通过在自由边界上试设具有待定参数的挠度函数,采用李维解法推导出三边简支一边自由矩形薄板在自由边界挠度作用下的挠度方程;其次利用横向变温作用下四边简支矩形薄板的求解得到待定参数;再采用叠加原理得出横向变温作用下三边简支一边自由矩形薄板的挠度和弯矩解析解;最后利用MATLAB编制程序得到了横向变温作用下三边简支一边自由矩形薄板的计算系数用表,为工程结构中三边简支一边自由混凝土矩形薄板在热环境下的设计计算提供了理论依据.     

横向磁场中软铁磁薄板的物理非线性混沌振动

对处于横向均匀磁场中四边简支的软铁磁矩形薄板,在横向均布载荷作用下,考虑物理非线性和磁弹性耦合作用,由伽辽金法推导出磁弹性振动微分方程,求得了系统的异宿轨道参数方程,并根据Melnikov函数方法,推导并求解了振动系统异宿轨道的MelnikOV函数,给出了判断该系统发生Smale马蹄变换意义下混沌振动的条件和混沌判据.     

矩形薄板弹性稳定的一般解

本文求得了矩形薄板稳定屈曲微分方程的一般解,可以求解任意边界矩形薄板的稳定问题。以两邻边自由或平夹,另两边简支正方形板为例求解了四边匀压的临界载荷及其挠度.     

Maxwell模型薄板的自由振动

本文利用Ｍａｘｗｅｌ粘弹性模型建立了粘弹性薄板的振动微分方程，给出四边简支粘弹性矩形薄板的固有频率解析解．对粘弹性矩形薄板的振动特性进行了讨论     

应用混合变量余能原理求解不同载荷作用下四边简支矩形板的弯曲

由功的互等定理导出了弯曲矩形板混合变量的总余能,应用混合变量余能原理求解四边简支矩形板弯曲问题,给出了四边简支矩形板的混合变量余能表达式,求解了不同载荷作用下四边简支矩形板的弯曲问题,并将计算的不同载荷作用下的挠度和弯矩值与ANSYS有限元的计算值比较,给出了一种求解四边简支矩形板的新方法。     

变厚度矩形板

在薄板的小挠度理论中,四边固定的矩形板是个难题。如果再加上“变厚度”这一因素,则难度将更大。本文用二重有限付里叶变换研究在任意荷载作用下的四边简支或四边固定的变厚度矩形板。同时,作为一些特例,本文顺便给出其他多种边界条件下问题的解。     

变厚度矩形薄板的一般解

本文应用“两步级数展开”法构造了任意变厚度各向同性弹性矩形薄板的一般理论解。文中研究了四边简支、四边固支以及两对边简支另两边含自由边的矩形板的一般解和一些特例。最后,用数值算例证实了本文方法的有效性。     

四边简支各向同性矩形厚板的插值矩阵法解

针对强厚度矩形板四边简支情况,论文根据状态变量法思想,基于三维弹性理论基本方程,以3个位移分量及3个应力分量按双三角级数展开,将三维弹性力学控制方程转化为常微分方程边值问题.尽管一些各向异性弹性矩形厚板早已由状态空间法获得分析解,可是各向同性厚板的分析解至今难以获得,因为状态空间解法中特征方程有重根问题而不易于收敛.论文提出采用插值矩阵法直接对常微分方程进行求解,获得各向同性矩形厚板在四边简支边界条件下三维理论的位移和应力解,并与有限元精细结果进行比较,证明了本文解的准确性.     

横观各向同性弹性半空间地基上四边自由各向异性矩形薄板弯曲解析解

选用更具广泛性的横观各向同性弹性半空间地基模型,来分析四边自由各向异性矩形地基板的弯曲解析解．将异性薄板的弯曲控制方程,与基于横观各向同性弹性半空间地基位移解建立的板与地基变形协调方程相结合,先按对称性分解,然后用三角级数法,得出横观各向同性弹性半空间地基上四边自由各向异性矩形薄板的弯曲解析解,包括地基反力、板的挠度及内力的解析表达式．该解析解克服了数值法的弊端,取消了对地基反力的假设,板的内力及地基反力求解更切实际．算例结果与文献结果吻合良好,证明本文方法的可行性．     

冲击荷载下钢化夹层玻璃薄板的动力学响应研究

针对工程材料中的钢化夹层玻璃受风沙冲击问题，利用重三角级数构造了冲击荷载作用下四边简支弹性矩形夹层薄板的挠度函数，依据积分变换方法求解挠度函数系数，并基于薄板小挠度弯曲理论得到四边简支条件下矩形钢化夹层玻璃薄板的应力与应变函数，利用Matlab编程对其分布规律计算，研究钢化夹层玻璃受冲击的动力学特性。结果表明：在不同冲击高度下，冲击力、位移响应均呈先增加后减小的趋势，且由于冲击惯性效应致使位移响应分为接触加载期、接触卸载期、脱离后期；应力波在玻璃内对称向四周传播且不断衰减致使位移场、应变场、应力场均呈对称分布，且冲击荷载对冲击点的影响最大；钢化夹层玻璃薄板冲击点区域下表面受拉而出现拉破坏，边界区域受压出现压破坏，而上表面的破坏情况则恰好相反。该研究结果为研究夹层玻璃受冲击破坏机理提供了重要依据。     

Modified Mindlin plate theory and shear locking-free finite element formulation

The basic equations of the Mindlin theory are specified as starting point for its modification in which total deflection and rotations are split into pure bending deflection and shear deflection with bending angles of rotation, and in-plane shear angles. The equilibrium equations of the former displacement field are split into one partial differential equation for flexural vibrations. In the latter case two differential equations for in-plane shear vibrations are obtained, which are similar to the well-known membrane equations. Rectangular shear locking-free finite element for flexural vibrations is developed. For in-plane shear vibrations ordinary membrane finite elements can be used. Application of the modified Mindlin theory is illustrated in a case of simply supported square plate. Problems are solved analytically and by FEM and the obtained results are compared with the relevant ones available in the literature.     

球壳轴对称弯曲问题共轭二阶挠度微分方程

提出球壳轴对称弯曲问题共轭二阶挠度微分方程并给出了初等函数解. 球壳微分方程是薄壳理论三大壳之一旋转壳的典型方程. 共轭二阶挠度微分方程是球 壳中微分方程形式最简单的, 是人们最喜爱的挠度微分方程. 挠度微分方程满足边 界条件非常简单, 使球壳的计算得到很大的简化.     

On the truth of nanoscale for nanobeams based on nonlocal elastic stress field theory： equilibrium, governing equation and static deflection

This paper has successfully addressed three critical but overlooked issues in nonlocal elastic stress field theory for nanobeams： （i） why does the presence of increasing nonlocal effects induce reduced nanostructural stiffness in many, but not consistently for all, cases of study, i.e., increasing static deflection, decreasing natural frequency and decreasing buckling load, although physical intuition according to the nonlocal elasticity field theory first established by Eringen tells otherwise？ （ii） the intriguing conclusion that nanoscale effects are missing in the solutions in many exemplary cases of study, e.g., bending deflection of a cantilever nanobeam with a point load at its tip; and （iii） the non-existence of additional higher-order boundary conditions for a higher-order governing differential equation. Applying the nonlocal elasticity field theory in nanomechanics and an exact variational principal approach, we derive the new equilibrium conditions, do- main governing differential equation and boundary conditions for bending of nanobeams. These equations and conditions involve essential higher-order differential terms which are opposite in sign with respect to the previously studies in the statics and dynamics of nonlocal nano-structures. The difference in higher-order terms results in reverse trends of nanoscale effects with respect to the conclusion of this paper. Effectively, this paper reports new equilibrium conditions, governing differential equation and boundary condi- tions and the true basic static responses for bending of nanobeams. It is also concluded that the widely accepted equilibrium conditions of nonlocal nanostructures are in fact not in equilibrium, but they can be made perfect should the nonlocal bending moment be replaced by an effective nonlocal bending moment. These conclusions are substantiated, in a general sense, by other approaches in nanostructural models such as strain gradient theory, modified couple stress models and experiments.     

求解阶梯连续梁的通用方程

考虑阶形变化截面及不等跨度的情况,建立了求解多跨连续梁变形的通用方程．根据挠曲微分方程并采用奇异函数求解,给出了分析此类连续梁位移的边界参数方程．该参数方程中含有若干待定的初参数和支反力．进一步导出计算变刚度不等跨连续梁位移的递推格式．最后考虑了位移协调条件及平衡条件而得到求解支反力的代数方程组．其计算的实例表明该方法适于编程运算．     

Refined differential equations of deflections in axial symmetrical bending problems of spherical shell and their singular perturbation solutions

This paper deals with the research of accuracy of differential equations of deflections.The basic idea is as follows.Firstly,considering the boundary effect the meridianmidsurface displacement u=0,thus we derive the deflection differential equations;secondly we accurately prove that by use of the deflection differential equations or theoriginal differential equations the same inner forces solutions are obtained;finally,weaccurately prove that considering the boundary effect the meridian surface displacementu=0 is an exact solution.In this paper we give the singular perturbation solution of thedeflection differential equations.Finally we check the equilibrium condition and prove theinner forces solved by perturbation method and the outer load are fully equilibrated.Itshows that perturbation solution is accurate.On the other hand,it shows again that thedeflection differential equation is an exact equation.The features of the new differential equations are as follows:1.The accuracies of the new differentia     

Large deflection of a rectangular magnetoelectroelastic thin plate

Based on the von Karman plate theory of large deflection, we derive the nonlinear partial differential equation for a rectangular magnetoelectroelastic thin plate under the action of a transverse static mechanical load. By employing the Bubnov-Galerkin method, the nonlinear partial differential equation is transformed to a third-order nonlinear algebraic equation for the maximum deflection where a coupling factor is introduced for determining the coupling effect on the deflection. Numerical results are carried out for the thin plate made of piezoelectric BaTiO₃ and piezomagnetic CoFe₂O₄ materials. Some interesting results are obtained which could be useful to future analysis and design of multiphase composite plates.     

冰载荷下不锈钢复合板挠度特性分析

以复合板中面的挠度响应作为不锈钢复合板抗冲击性能的评价指标,基于能量法和经典层合板理论,考虑层间结构参数设计,通过横向载荷下的弯曲平衡微分方程,建立冰载荷下不锈钢复合板挠度响应简化解析模型。该分析模型将整个动态响应分析过程分为冰载荷计算分析和动力学方程求解两个阶段。分析了冰载荷模型的面倾角、冲击速度和碰撞位置对冰载荷的影响,确定极端工况参数,汇总接触面的节点力数据;分析了层厚比对挠度响应的影响规律;基于LS-DYNA有限元仿真以及数值算例分析,对比挠度响应仿真结果和解析计算值,验证了本文简化解析模型的准确性,研究结果对不锈钢复合板抗冲击性能分析和评估具有一定的参考价值。     

DETERMINATION OF THE CRITICAL DEFLECTION OF A SLENDER COLUMN1)

本文使用严格的边界条件,对理想弹性压杆的临界力重新定义。采用挠曲线近似微分方程方法和能量法给出了临界力的极限表达形式,解决了细     

柔性套管约束下轴心受压杆件的屈曲分析

针对柔性套管约束杆件,研究了轴压杆件与约束杆件点、线接触时的约束屈曲．在小挠度变形假设下,根据轴压杆件与约束杆件满足变形协调条件的二阶平衡微分方程,推导了轴压杆件挠度、轴向位移、接触反力的计算公式,并且由轴向压力唯一确定了线接触的长度．算例分析表明：当约束杆件刚度较小时,轴压杆件弯曲产生的轴向位移较大；当约束杆件刚度较大时,轴压杆件弯曲产生的轴向位移较小,该轴向位移与文献中的大挠度解吻合很好,从而得出小挠度变形假设是合理的．