复合材料对称层合板单向拉伸与面内剪切下的三维应力分析

本文给出了单向拉伸与面向剪切载荷下复合材料对称层合板中心区域的应力和应变沿板厚的数值计算分布规律。计算结果表明，在斜交对称辅层的层合板中心区域层间界面附近存在着层间边界层效应。层间界面处纤维走向的突变导致局部的三维应力状态和很强的应力集中。     

Discussion on“General Solutions of Axial Symmetrical Ring Shells”

There is one point to be mentioned about the decay constant of homogeneoussolution in the paper“General Solutions of Axial Symmetrical Ring Shells”(No.3.1980 of this Journal).There is an infinite number of rootsλ.The general form ofthese roots is     

中细柔性圆环壳整体弯曲的一般解及在波纹管计算中的应用（I）—基本方程和一般解

讨论了圆环壳在横向载荷作用下的整体弯曲问题，提出了中细柔性圆环壳的概念、基本方程和一般解。本文称粗细比（子午线曲率半径与子午线曲率中心到回转轴的距离之比）小于1／3的圆环壳为中细圆环壳；方程的推导基于E.L.Axelrad的柔性壳理论；所得的解含有处理边界问题所必须的积分常数并且在全域内处处收敛；本解能方便地用于有关波纹管的计算。全文共分4个部分：（I）基本方程和一般妥；（Ⅱ）Ω型波纹管的计算；（Ⅲ）C型波纹管的计算；（Ⅳ）U型波纹管的计算。     

CALCULATION OF STRESSES AND DEFORMATIONS 0F BELLOWS BY INITIAL PARAMETER METHOD OF NUMERICAL INTEGRATION

-By reducing the boundarg value problem in stressanalysis of bellows into initial value problem,thispaper presents a numerical solution of stress distri-bution in semi-circular arc type bellows based uponthe toroidal shell equation of V.V.Novozelov.Throughout the computation.S.Gill’s method ofextrapolation is used.The stresses and deformationsof bellows under axial load and internal pressure arecalculated,the results of which agree completely withthose derived from the general solution of Prof.ChienWei-zang.The extrapolation formula presentedin this paper greatly promotes the accuracy of dis-crete calculation.The computer program in BASIC language of wang2200 VS computer is included in the appendix.     

PERTURBATION INITIAL PARAMETER METHOD FOR SOLVING THE GEOMETRICAL NONLINEAR PROBLEM OF AXISYMMETRICAL SHELLS

In the previous paper[7],the author presented a System of First-Order DifferentialEquations for theproblem of axisymmetrically loaded shells of revolution with small elastic.strains and arbitrarily large axial deflections.and a Method of Variable-CharacteristicNondimensionization with a Scale of Load Parameter.On this basis.by taking theweighted root-mean-square deviation of angular deflection from linearity as perturbationparameter.this paper pressents a perturbation system of nondimensional differentialequations for the problem,thus transforms the geometrical nonlinear problem into severallinear problems.This paper calculates these linear problems by means of the initialparameter method of numerical integration.The numerical results agree quite well with theexperiments.     

GENERAL SOLUTION OF THE OVERALL BENDING OF FLEXIBLE CIRCULAR RING SHELLS WITH MODERATELY SLENDER RATIO AND APPLICATIONS TO THE BELLOWS (Ⅳ)-CALCULATION FOR U-SHAPED BELLOWS

ＩｎｔｒｏｄｕｃｔｉｏｎＵ＿ｓｈａｐｅｄｂｅｌｌｏｗｓａｒｅｕｓｕａｌｌｙｓｅｅｎｉｎｔｈｅｐｉｐｅｌｉｎｅｓｙｓｔｅｍ (Ｆｉｇ .1) ,ｗｈｉｃｈａｒｅｕｓｅｄｔｏｃｏｍｐｅｎｓａｔｅｆｏｒｔｈｅａｘｉａｌｍｏｖｅｍｅｎｔ,ｔｈｅｒｏｔａｔｉｏｎａｎｄｔｈｅｄｅｆｌｅｃｔｉｏｎｏｆｔｈｅｐｉｐｅｌｉｎｅｓｄｕｅｔｏｔｈｅｔｈｅｒｍａｌａｃｔｉｏｎ ,ｔｈｅｂａｓｅｕｎｅｑｕａｌｓｅｔｔｌｅｍｅｎｔｓａｎｄｔｈｅｉｎｓｔａｌｌａｔｉｏｎｅｒｒｏｒｓ.Ｔｈｅａｘｉｓｙｍｍｅｔｒｉｃａｌｄｅｆｏｒｍａｔｉｏ…     

GENERAL SOLUTION OF THE OVERALL BENDING OF FLEXIBLE CIRCULAR RING SHELLS WITH MODERATELY SLENDER RATIO AND APPLICATIONS TO THE BELLOWS (Ⅰ)-GOVERNING EQUATION AND GENERAL SOLUTION

ＩｎｔｒｏｄｕｃｔｉｏｎＴｈｅｔｈｅｏｒｙｏｆｆｌｅｘｉｂｌｅｓｈｅｌｌｓ,ｅｓｔａｂｌｉｓｈｅｄｂｙＥ .Ｌ .Ａｘｅｌｒａｄ[1,2 ]( 1 976,1 987) ,ｉｓａｓｉｍｐｌｉｆｉｅｄｔｈｅｏｒｙｆｏｒｔｈｉｎｓｈｅｌｌｓ,ｉｎｗｈｉｃｈｓｈｅｌｌｓｏｆｒｅｖｏｌｕｔｉｏｎａｒｅｆｏｒｍｕｌａｔｅｄｉｎｍｅｒｉｄｉｏｎａｌｄｉｒｅｃｔｉｏｎｂｙｂｅｎｄｉｎｇｔｈｅｏｒｙｏｆｔｈｅｓｈｅｌｌｓａｎｄｂｙｔｈｅｍｅｍｂｒａｎｅｔｈｅｏｒｙｉｎｔｈｅｃｉｒｃｕｍｆｅｒｅｎｔｉａｌｄｉｒｅｃｔｉｏｎ .ＴｈｅＡｘｅｌｒ…     

摄动初参数法解轴对称壳几何非线性问题

作者在文[7]中提出轴对称壳任意大挠度问题的一阶微分方程组和以载荷变量为尺度的变特征无量纲化方法。在此基础上,本文选取挠角非线性偏差的加权均方根作摄动参数,给出该问题的无量纲摄动微分方程组。从而把非线性问题转化为n个线性问题来解决。本文采用数值积分的初参数方法对摄动后的各阶线性问题进行了计算。摄动结果与实验[4]相符合。     

环壳理论与直交异性板理论在计算三圆弧波纹膜片上的比较

有人用直交异性板的理论计算[1]波纹板(膜片)的弹性位移,所得结果曾与实验对照比较满意.但是并没有人认真分析波纹数目、形状对直交异性板的弹性位移和应力分布的数量上的影响,以致未能对用直交异性板理论计算波纹板的范围作明确的说明.以前只是较一般地说,直交异性板理论用于计算波纹数目较多的膜片弹性特性(弹性位移与外力的关系)较满意,计算应力误差较大.本文利用环壳理论[2][3]分析了对称和不对称三圆弧波纹膜片的位移与应力,并与直交异性理论所得结果比较,明确了直交异性板理论的应用范围.     

Complex equations of flexible circular ring shells overall-bending in a meridian plane and general solution for the slender ring shells

ＩｎｔｒｏｄｕｃｔｉｏｎＥｑｕａｔｉｏｎｓｆｏｒｃｉｒｃｕｌａｒｒｉｎｇｓｈｅｌｌｓａｒｅｄｉｆｆｉｃｕｌｔｔｏｓｏｌｖｅ．Ｔｈｅｒｅｓｅａｒｃｈｏｆｔｈｉｓｐｒｏｂｌｅｍｓｔａｒｔｅｄａｔｔｈｅｂｅｇｉｎｎｉｎｇｏｆｔｈｉｓｃｅｎｔｕｒｙ．Ｉｎｔｈｅｌａｔｅ１９７０ｓａｎｄｅａｒｌｙ１９８０ｓ,Ｗ．Ｚ．Ｃｈｉｅｎ（１９７９,１９８０,１９８１）［１～３］ｒｅｂｕｉｌｔｔｈｅｃｏｍｐｌｅｘｅｑｕａｔｉｏｎｓｏｆａｘｉｓ＿ｓｙｍｍｅｔｒｉｃａｌｌｙｌｏａｄｅｄｒｉｎｇｓｈｅｌｌｓｐｒｅｓｅｎｔｅｄ…