各向异性叠层矩形板大挠度弯曲问题

本文以板的中心挠度为摄动参数,采用摄动方法获得承受均布载荷,四边固定的对称角交叠层板的大挠度弯曲问题的近似解.与文献[12]不同,本文在每一级近似中,应用伽辽金方法求出各级近似解.文中计算了碳纤维复合材料对称角交叠层板的数值结果,绘出了载荷与中心挠度关系曲线以及列出有代表性的几点的应力计算公式.另外,本文研究了玻璃纤维复合材料正交对称叠层方板的大挠度特性,与文献[6]采用有限差分法所得的结果比较表明,采用本文的方法所得结果与试验值吻合得较好.     

直角刚架在撞击作用下的塑性大挠度响应

本文研究了悬臂直角刚架在其自由端受到自身平面内的横向撞击时的塑性动力响应在本文报告的实验中,利用空气炮射出的子弹加载使软钢材料制成的直角刚架产生大挠度塑性变形;同时,依据理想刚塑性材料模型,给出了一个大挠度瞬时模态解。理论分析得到的挠度-载荷曲线与实验结果符合得很好。     

关于冲击载荷下圆柱壳塑性屈曲的两个问题

本文按文献[1]中提出的能量原理,讨论了两个冲击载荷下圆柱壳的塑性屈曲问题,得到了相应的临界冲击速度的计算公式。1.径向冲击下圆柱壳的临界速度问题径向冲击下圆柱壳的塑性屈曲早在文献[2]中就已研究过。但和别的类似问题一样,已有工作主要限于屈曲模态的计算,而对究竟多大的冲击速度下可能发生塑性屈曲的问题,即所谓临界速度问题,并未进行过理论上的分析。其原因我们在[1]中已经指出,即经典的临界速度定义已不适用于此类问题,问题的提法需要重新考虑。     

计入膜力塑性耗散效应的矩形板塑性动力响应

从能量的观点在小挠度理论中引入表征膜力塑性耗散效应的修正因子,基于刚性板块的总体平衡给出矩形板大挠度塑性动力响应的完全运动方程组,分析了理想刚塑性简支和固支矩形板在矩形脉冲和冲击载荷下包括移行塑性铰相的完全大挠度响应过程。解决了当矩形板的挠度达到厚度量级时弯矩、膜力的联合作用问题,理论预报的结果在板的挠度为10倍板厚的量级与实验结果符合良好,改进了只考虑弯矩作用的小挠度理论结果和模态近似估计。     

贮液圆柱容器湿模态的正交性及其在动力响应分析中的应用

1.引言湿模态分析技术近几年来已日益受到人们的重视.文献[1]和[2]用杂交子结构法解大型液固耦合系统的特征值问题,其中就是以湿模态的正交性作为基础.离散形式的湿模态的正交性Daniel曾作了一定程度上的论证;连续体系湿模态的正交性的证明,目前只见到梁式结构.本文从圆柱壳体模型出发,借助Fl?gge运动方程和势流理论,     

理想弹塑性材料中Ⅲ型裂纹扩展的理论阻力曲线

用复变函数中的Cauohy积分公式求出了理想弹塑性材料中小范围屈服条件下Ⅲ型裂纹准静态扩展时裂纹线上塑性区尺寸x_p与应力强度因子K_m的关系式。利用这个关系式将Rice[1]根据临界塑性应变准则建立的x_p(l)的积分方程,l为裂纹扩展量,化为阻力曲线K_R(l)的积分方程.采用文献[2]中的方法得到K_R(l)在不同临界塑性应变下的数值解.结果表明K_R随l的增加而单调增加.最后达到裂纹准静态定常扩展所需要的常数值.     

雷诺数较大时平行圆板间径向扩散层流进口段半径长度

平行圆板间径向扩散流考虑进口段效应时,文献[1]得到了数值解和近似解.本文用文献[2]的方法求得了新的近似解,它比文献[1]的近似解更加准确.     

强脉冲载荷作用下结构塑性大变形的最大挠度直接预测

经过多年的研究,由中国学者提出和研发的膜力因子法和饱和分析方法已被证明是分析和预测冲击、爆炸等强动载荷作用下梁、板等结构件的塑性大变形行为的有力工具.在这两套理论工具相结合所获得的一系列最新成果的基础上,文章提出一种对梁和板在强脉冲作用下的最大挠度的直接预测方法.考虑了膜力和弯矩相互作用的准确屈服条件,同时假定位移场近似地按照与准静态破损机构相似的模态发生变化,该方法直接从膜力因子的表达式出发,依据外载作的功与塑性耗散相等的能量条件,只需要求解初等方程就可以简单明晰地得到梁和板在矩形脉冲作用下的最大挠度,极大地简化了数学推导.与同时考虑准确屈服条件和瞬态响应阶段的完全解以及具有上下界的模态解相比,这一方法能够同样准确但更简单地计入膜力对结构大变形承载能力的效应,为工程设计提供比完全解更简明、比模态解更精准的梁和板最大塑性变形的估算公式;再同改进的脉冲等效技术相结合,这种直接预测方法有望进一步拓展到更复杂的结构件,获得广泛的工程应用.     

置于液面上的刚塑性圆板大挠度动力响应分析

分析了置于无旋不可压理想流体流面上的简支刚塑性圆板受矩形脉冲载荷作用的大挠度动力响应，借助Ｈａｎｋｅｌ变换，将液－固耦合作用为在空气中的圆板塑性动力响应问题，进而求解弯矩和膜力联合作用的大挠度运动方程，得到了中载及高载下各相运动的完全解，并提供了数值算例。     

受端部冲击的悬臂曲梁小变形塑性分析的一种方法

1.引言对悬臂梁的塑性动力响应问题为许多学者研究过,近年来Y_u(余同希)、Symonds及Johnson对圆弧悬臂梁受端部冲击的刚塑性动力响应作了较完整的小变形分析,zhang(张铁光)及Yu(余同希)对同一问题作了刚塑性大变形分析。文献[1]、[4]、[5-7]的共同特点是把运动分为二个阶段,第一阶段移行塑性铰由端部移行到固定端,第二阶段运动为绕根部固定塑性铰的转动。     

Lee's extremum principle and the large deflection response of dynamically loaded plastic structures

An approximate method based on Lee's extremum principle is introduced to study the large deflections of dynamically loaded plastic structures. As an example, the evolutionary mode of an impulsively loaded rigid-perfectly plastic portal frame is determined and then compared with the experimental results [8] and with the large deflection complete solution obtained previously [9]. It is found that the evolutionary modal solution may approach the complete solution if the modes are appropriately chosen.     

Mode II dynamic fields near a crack tip growing in an elastic-perfectly-plastic solid

An asymptotic solution is given for Mode II dynamic fields in the neighborhood of the tip of a steadily advancing crack in an incompressible elastic—perfectly-plastic solid (plane strain). It is shown that, like for Modes I and III (Gao and Nemat-Nasser, 1983), the complete dynamic solution for Mode II predicts a logarithmic singularity for the strain field, but unlike for those modes which involve no elastic unloading, the pure Mode II solution includes two elastic sectors next to the stress-free crack surfaces. This is in contradiction to the quasi-static solution which predicts a small central plastic zone, followed by two large elastic zones, and then two very small plastic zones adjacent to the stress-free crack faces. The stress field for the complete dynamic solution varies throughout the entire crack tip neighborhood, admitting finite jumps at two shock fronts within the central plastic sector. This dynamic stress field is consistent with that of the stationary crack solution, and indeed reduces to it as the crack growth speed becomes zero.     

A note on the problem of pure bending for linear elastic materials with voids

This note concerns the problem of quasi-static pure bending of a beam in the context of the complete theory of linear elastic materials with voids presented in [1]. It is shown here that the solution in the context of the complete theory of [1] is coincident with the pure bending solution of classical elasticity for small time, and that the solution for large time is the bending solution given in [1], a solution which neglected the rate effect in the complete theory of [1]. In between these two limit solutions the rate effect moderates a monotonic transition.     

Finite elastoplastic deformation of an internally pressurized hollow sphere

This paper considers large elastoplastic deformations of an internally pressurized hollow sphere of dilatant soil. A complete analytical solution for the expansion of a hollow sphere is developed. The soil is modelled as an elastic-perfectly plastic material obeying the Mohr-Coulomb yield criterion. A non-associated plastic flow rule is used and therefore the dilation of the material is fully taken into account. Closed form solutions are obtained for the stresses and the elastic-plastic deformations of arbitrary magnitude when a hollow sphere of soil is subjected to constant external pressure and monotonically increasing internal pressure. A selection of numerical results is presented to indicate the effects of various key parameters     

含切口悬臂梁的大变形塑性冲击动力响应

本文分析了含切口的悬臂梁受飞射物撞击的刚塑性动力响应的完全解,推导了考虑几何大变形效应的“双铰模式”的动力学方程,给出了计算方法和计算结果,最后讨论了耗散能的分配和切口对梁最终变形的影响。     

DYNAMIC RESPONSE OF A RIGID,PERFECTLY PLASTIC FREE-FREE BEAM STRUCK BY A PROJECTILE ATANY CROSS-SECTION ALONG ITS SPAN

I. INTRODUCTION The dynamic plastic response of free-free beams subjected to intense dynamic loading is a subject ofinterest for aerospace engineering applications. For example, when a rocket is attacked by a missile, itslarge plastic deformation behav…     

Elastic–plastic and elastic anti-plane shear of two parallel cracks

Two infinite interacting parallel cracks in an elastic–plastic and in an elastic body under anti-plane strain (mode III) loading conditions are considered. The body is subjected to vanishing remote loading and the cracks are traction free. Closed-form solution is found for the elastic–plastic problem in terms of elementary functions, where the shape of the plastic boundary is obtained. The complete stress distribution is obtained in an inverse form i.e. physical coordinates are functions of stresses.     

Large strain responses of elastic-perfect plasticity and kinematic hardening plasticity with the logarithmic rate: Swift effect in torsion

A new Eulerian rate type elastic-perfectly plastic model has recently been established by utilizing the newly discovered logarithmic rate. It has been proved that this model is unique among the objective elastic-perfectly plastic models with all objective corotational stress rates and other known objective stress rates by virtue of the self-consistency criterion: the hypoelastic formulation intended for elastic behaviour must be exactly integrable to deliver a hyperelastic relation. The finite simple shear response of this model has been studied and shown to be reasonable for both shear and normal stress components. On the other hand, a kinematic hardening plasticity model may be formulated by adopting the logarithmic rate. The objective of this work is to further study the large deformation responses of the foregoing two kinds of idealized models, in particular the well-known Swift effect, in torsion of thin-walled cylindrical tubes. A complete, rigorous analysis is made for the orders of magnitude of all stress components. A closed-form solution is obtained for the kinematic hardening plastic case, and an analytical perturbation solution is derived for the elastic-perfectly plastic case. It is shown that the simple idealized kinematic hardening model with the logarithmic rate, which uses only two classical material constants, i.e., the initial (tensile) yield stress and the hardening modulus, may arrive at satisfactory explanation for and reasonable accord with salient features of experimental observation.     

Plastic modal approximations in analyzing beam-on-beam collisions

Dynamic behavior of a moving free–free beam striking the tip of a cantilever beam, as a typical example of collision between two deformable structures, is analysed by employing modal approximation techniques. The applicability of both rigid-plastic and elastic–plastic mode approximations is examined in predicting the energy partitioning between the two colliding beams.Three rigid-plastic modes (RP-Modes) are considered and the Lee’s functional is applied to select the appropriate mode. It is found that one of the beams would absorb all the initial kinetic energy, unless a higher-order RP-mode is adopted.To incorporate the effect of elastic deformation into the modal solution, an elastic, perfectly plastic mode (EP-Mode) approximation for the same problem is proposed. By replacing each of the plastic hinges in the RP-Mode with a nature hinge and an elastic–plastic rotational spring, the fundamental features of the dynamic elastic–plastic behavior of the two colliding beams are revealed. Both beams participate in energy dissipation, while the structural and geometrical parameters greatly influence the energy partitioning. It is shown from numerical examples that the EP-Mode solution provides a fairly good approximation compared with the RP complete solution and finite element simulation.