一个改进的平面梁单元

根据有限单元法基本原理 ,提出了一个变截面平面梁单元 ,推导了其单元钢度矩阵。这一改进的梁单元用于分析梁高呈线性变化及二次抛物线变化的矩形截面梁 ,将得到准确解。文中给出了一个变截面悬臂梁算例 ,计算表明 ,这一改进的梁单元使变截面梁的分析大大简化     

关于规定荷载下柱截面设计方法的探讨

桁架和柱的设计中,常碰到压杆的稳定问题,这一问题在不知杆的截面尺寸情况下,是以试算的方法确定杆的临界力,然后确定截面尺寸.本文给出了常见型钢杆件、松元木杆件受压时稳定问题的图解法,设计者可依据其荷载、支承情况迅速地查出所需截面尺寸或型钢型号.     

矩形截面杆的翘曲正应力

矩形截面杆的翘曲正应力申向东，康德基（内蒙古农牧学院水利系，呼和浩特０１００１８）杆在平面弯曲时，因剪切使横截面翘曲而产生的正应力，这里称为翘曲正应力，在材料力学教材中一般未给出计算表达式。本文用材料力学的一般方法求得了矩形截面杆在任意分布荷载作用下...     

多约束膜结构截面优化及在MSC/Nastran上的程序实现

将准则法和数学规划法相结合，借助满应力准则将应力约束转化为动态尺寸约束，利用单位虚载荷法将位移约束转化为设计变量的显式表达式建立优化模型，然后用数学规划法求解；采用无量纲设计变量实现设计变量连接，对膜结构的厚度进行优化设计；根据对偶理论，应用对偶规划精确映射原问题，再按泰勒展式建立对偶问题的二阶近似。为了提高优化效率，采用射线步调整结构性态，运用粗选有效约束技术筛选约束，并采用主、被动变量循环确保收敛稳定。以MSC／Nastran软件作为结构分析的求解器，以MSC／Patran软件作为开发平台，完成了膜结构截面优化程序。对膜结构的单变位、多变位的结构优化问题进行了优化计算，并与MSC／Nastran优化模块的计算结果进行比较。算例结果表明程序的可靠性、高效性和稳定性以及理论算法的优越性。     

FLOW STRUCTURE FORMATION AND EVOLUTION IN CIRCULATING GAS-FLUIDIZED BEDS

The occurrence of heterogeneous flow structures in gas-particle flows seriously affects the gas-solid contacting and transport processes in high-velocity gas-fluidized beds. Particles do not disperse uniformly in the flow but pass through the bed in a swarm of clusters. The so-called “core-annulus“ structure in the radial direction and “S“ shaped axial distribution of solids concentration characterize the typical flow structure in the system. A computational study, using the discrete particle approach based on molecular dynamics techniques, has been carried out to explore the mechanisms underlying formation of the clusters and the core-annulus structure. Based on energybudget analysis including work done by the drag force, kinetic energy, rotational energy, potential energy, and energy dissipation due to particle-particle and particle-wall collisions, the role of gas-solid interaction and inelastic collisions between the particles are elucidated. It is concluded that the competition between gas-solid interaction and particle-particle interaction determines the pattern formation in high-velocity gas-solid flows: if the gas-solid interaction (under elevated pressure) dominates, most of particle energy obtained by drag from the gas phase is partitioned such that particle potential energy is raised, leading to a uniform flow structure. Otherwise, a heterogeneous pattern exists, which could be induced by both particle -particle collisions and gas-solid interaction. Although both factors could cause the flow instability, the non-linear drag force is demonstrated to be the necessary condition to trigger heterogeneous flow structure formation. As gas velocity increases and goes beyond a critical value, the fluid-particle interaction suppresses particle collisional dissipation, and as a consequence a more homogeneous flow regime is formed.     

螺旋细杆的均匀扭转振动

讨论螺旋细杆的特殊形式扭转振动，即均匀扭转振动．以非圆截面杆和有原始曲率的圆截面杆为研究对象．杆作均匀扭转振动时各截面有相同的扭角变化规律，且杆中心线的几何形状不受振动过程的影响．研究表明，扭振来源于杆截面的非对称性及杆的原始曲率．杆的扭振规律与单摆运动相似，其动力学方程存在精确解．圆环杆的均匀扭振为螺旋杆的倾角为零时的特例．     

波纹钢屋盖结构板件相关屈曲的试验研究与分析

拱型波纹钢屋盖结构的受力机理异常复杂，波纹、加工制作过程中产生的变形和残余应力等初始缺陷在理论分析中很难精确定量描述。论文对波纹钢屋盖结构梯形截面板组进行了轴心和偏心压力作用下稳定承载能力的试验研究，并与理论结果进行了比较分析，试验与理论结果吻合较好。试验结果表明波纹板组具有较高的局部屈曲承载能力，但几乎无屈曲后承栽能力，与平板板组屈曲特性相比有显著差异。     

Experimental and FEM study of windshield subjected to high speed bird impact

Both experimental and finite element model (FEM) results are presented for the dynamic strength behavior of windshield subjected to bird impact. The experimental data taken from a series of high speed photographs are compared with the numerical results predicted by using FEM in which the windshield was modeled entirely with solid elements and the bird body was approximately simulated by an elastic-plastic material with failure element behavior. Effective plastic strain and element pressure were adopted as the failure criteria and once the pressure or the effective plastic strain of an element reached the critical value, the element would lose the tensile resistance capability completely. The deflection and stress distribution in the windshield were obtained. It is shown that the result from the finite element analysis agrees with those from the full-scale bird impact test. The project supported by the National Natural Science Foundation of China (10272011)     

185℃试件栅转移方法研究碳／双马复合材料层板的固化残余层间剪切…

本文采用１８５℃试件栅转移方法和云纹干涉法的载波技术，研究了碳／双马复合材料层板（－４５／９０／４２２／９０／－４５２／９０／４５／０／－４５／４５）２Ｓ的固化残余层间剪切应变，并给出剪应变沿铺层截面的分布。     

非均质变截面弹性直杆纵向自由振动的渐近解法

本文研究弹性模量、横截面积和单位杆长质量均按指数规律变化的非均质变截面弹性直杆的纵向自由振动问题,提出了一种既能保证一定精度,计算又很简单的非均质变截面弹性直杆纵向自振频率及振型的渐近解法,导出了“1”级近似解的具体计算公式,最后给出了两个算例,并与精确解进行了比较。