大型纵向加筋截断锥壳稳定性的半离散分析

如何计算大型纵向加筋截断锥壳的稳定问题，尚未见到有关报导。本文在沿纵向和环向分别采用Ｈｅｒｍｉｔｅ插值和三角级数插值的基础上，建立了几何非线带筋环单元，进而导出了半离散分析法，并经过实验检验了它的正确与可靠。这样，本文为建立各类工程结构的半离散单元提出了一种新的途径。     

用Voronoi图进行新型自然邻居插值的几何学方法与特性

新的基于Voronoi图的Natural Neighbour插值是自然单元法的数学基础，也是一种新型的几何插值方法，具有与其他传统常用插值不同的构造方法，并表现出一定的优越性。本文介绍了基于Natural Noighbour关系的Sibson插值和non-Sibsonian插值，并与有限元法和无单元法所用的插值方法，就离散插值方案和网格总体特性、形函数支撑域、本征边界条件、空间维数扩展与计算工作量等诸问题进行了比较分析。     

粘弹性问题的插值型无单元伽辽金比例边界法

作为一种最近发展起来的半解析数值方法,插值型无单元伽辽金比例边界法不仅无需基本解,且在处理应力奇异性问题和无限域问题时十分有效．为了更有效地求解粘弹性问题,对插值型无单元伽辽金比例边界法应用于此类问题进行了研究,并发展了相应的算法. 通过时域分段展开,将时空耦合的初边值问题转化为一系列递推形式的边值问题,然后采用插值型无单元伽辽金比例边界法进行自适应计算．在径向保持解析特性的基础上,环向采用无单元伽辽金法离散可简化前处理和后处理工作量．此外,改进的插值型移动最小二乘法形函数具有插值性,有效地解决了本质边界条件不能直接施加的困难．最后给出了数值算例,并验证了所提方法的有效性和正确性.     

Delaunay多边形单元的有理函数插值格式

本文提出了基于Delaunay多边形化的多边形单元有理函数插值格式。给出了Delaunay多边形化的概念和Delaunay多边形单元有理函数插值形函数的计算表达式。与Delaunay三角化网格不同，Delaunay多边形化网格形成对区域的唯一剖分。Delaunay多边形单元有理函数插值是以Delaunay多边形的顶点作为插值点，构造的有理函数形式插值。Delaunay多边形单元有理函数插值克服了有限元方法中难以构造边数大于4单元多项式形式位移插值的困难。有理函数插值形函数在多边形单元的内部是无穷次光滑的，在多边形的边界上是线性的。在三角形单元和矩形单元上，有理函数插值分别等价于有限元的三角形面积坐标插值和四边形双线性插值。给出了Delaunay多边形有理函数插值在圆域温度分布插值近似中的两个算例。     

加锚体自然单元法分析与程序设计

建立了加锚体的自然单元法分析模型。结合自然相邻插值和一维轴力杆单元的劲度矩阵,推导了锚杆支护数值模拟的单元列式,给出了自然单元法分析加锚体的实施步骤和主要程序设计。结构的离散和锚杆的离散完全独立,因此可以自由地加设或拆除锚杆。算例分析表明自然单元法分析加锚体的精度与有限元的相当,但比有限元的实施要方便得多。     

多边形有限单元形函数的比较研究

多边形有限单元形函数有wachspress插值、Laplace插值和平均值插值三种类型.本文对三种多边形有限单元形函数的性质作了比较研究,给出了三种形函数各自的优点和局限性.Waclaspress和Laplace形函数是有理函数形式,而平均值形函数是无理函数形式.三种形函数均满足单位分解性、线性完备性,且在单元边界上呈线性.在三角形单元上,它们都等价于三角形面积坐标插值.在矩形单元上,Wachspress和Laplace形函数等价于双线性多项式插值形函数.Wachspress和平均值形函数适用于任意凸多边形单元,Laplace形函数更适用于圆内接多边形单元.Wachspress形函数不能推广到含有边节点的单元,平均值形函数可以直接推广到含有边节点的单元.数值试验,验证了本文理论分析的结论.     

基于变形场不同离散方法的柔性机器人动力学建模与仿真

研究了基于变形场不同离散方法的柔性机器人动力学建模和仿真问题. 针对多杆空间链式柔性机器人系统,采用假设模态法、有限元法、Bezier 插值方法和B 样条插值方法对柔性杆变形场进行描述,构造统一形式,运用Lagrange 方法,结合4×4 齐次变换矩阵,在计入柔性杆横向弯曲变形引起的纵向缩短的情况下,推导得到多杆空间柔性机器人动力学方程,并编制基于4 种变形场不同离散方法的多杆空间链式柔性机器人仿真软件.通过仿真算例对柔性机器人系统的动力学问题进行研究. 仿真结果表明:有限元法的计算效率较低;假设模态法在处理较大变形问题时其精度低于Bezier 插值方法和B 样条插值方法的精度;作为新的变形体离散方法,Bezier 插值方法和B 样条插值方法可以有效地描述柔性杆的变形场,并能运用到多杆空间柔性机器人动力学建模中.      

多边形有限元研究进展

有限元法是数值求解偏微分方程边值问题的重要方法,采用不规则多边形单元网格, 可以方便有效地模拟材料的力学性能, 又使得区域网格剖分变得灵活方便. 特别是对于复杂的几何形状, 多边形单元网格具有更大的优势. 本文对国内外有关多边形有限元法的最新进展作了初步的总结和评述, 主要以基于位移法的多边形有限元为主.论述了多边形有限元的发展历史, 给出了多边形单元上的Wachspress插值、Laplace插值和重心坐标的一些最新研究成果. 与经典有限元法形函数为多项式形式不同, 多边形单元的形函数为有理函数或者无理函数形式. 多边形单元插值形函数满足线性完备性, 可以再现线性位移场, 像经典有限元法一样直接施加本质边界条件; 插值函数在多边形的边界上是线性的,确保不同单元间的自动协调. 不同单元的插值形函数表达公式形式统一, 方便混合单元网格计算的程序编写. 提出了多边形有限元法今后需要研究的问题.      

高度不规则网格多边形单元的有理函数插值格式

借鉴自然邻点插值法,提出了基于高度不规则网格多边形单元的有理函数插值格式一多边形有理函数插值．给出了多边形有理函数插值形函数的计算表达式．该插值格式以多边形的顶点作为插值点,插值形函数为有理函数形式,克服了传统有限方法中构造边数大于4单元多项式形式位移插值的困难．     

不可压缩N-S方程分步算法稳定性与精度的数值研究

众所周知,LBB条件排除了在不可压缩流动N-S方程空间离散中采用速度u和压力p同阶线性插值的简单单元。基于压力泊松(Poisson)方程的分步算法曾被认为可以绕开LBB条件限制,然而近年来研究表明,并非各种类型的分步算法都能有效地避开LBB条件。本文针对不同雷诺数下的平面Poiseuille流动问题模拟,分析对比了当采用不同类型的u-p单元空间插值时增量与非增量迭代分步算法的稳定性与精度,为合理选择分步算法和u-p插值类型提供了依据和参考。     

Free vibrations of rotating composite conical shells with stringer and ring stiffeners

In this paper, an analytical solution for the free vibration of rotating composite conical shells with axial stiffeners (stringers) and circumferential stiffener (rings), is presented using an energy-based approach. Ritz method is applied while stiffeners are treated as discrete elements. The conical shells are stiffened with uniform interval and it is assumed that the stiffeners have the same material and geometric properties. The study includes the effects of the coriolis and centrifugal accelerations, and the initial hoop tension. The results obtained include the relationship between frequency parameter and circumferential wave number as well as rotating speed at various angles. Influences of geometric properties on the frequency parameter are also discussed. In order to validate the present analysis, it is compared with other published works for a non-stiffened conical shell; other comparison is made in the special case where the angle of the stiffened conical shell goes to zero, i.e., stiffened cylindrical shell. Good agreement is observed and a new range of results is presented for rotating stiffened conical shells which can be used as a benchmark to approximate solutions.     

A new displacement-type stability equation and general stability analysis of laminated composite circular conical shells with triangular grid stiffeners

In this paper,based on the theory of Donnell-type shallow shell,a new displacement-type stability equations is first developed for laminated composite circular conical shellswith triangular grid stiffeners by using the variational calculus and generalized smeared-stiffener theory.The most general bending stretching couplings,the effect of eccentricity ofstiffeners are considered.Then,for general stability of composite triangular grid stiffenedconical shells without twist coupling terms,the approximate formulas are obtained forcritical external pressure by using Galerkin‘s procedure.Numerical examples for a certainC/E composite conical shells with inside triangular grid stiffeners are calculated and theresults are in good agreement with the experimental data.Finally,the influence of someparameters on critical external pressure is studied.The stability equations developed andthe formulas for critical external pressure obtained in this paper should be very useful in theastronautical engineering design.     

投影云纹法在研究加劲板后屈曲平衡路径及后屈曲模态转化过程的应用

本文应用投影云纹法研究受压加劲板的大挠度非线性问题。用投影云纹法测量加劲板后屈曲平衡路径,记录了随着载荷的增加,加劲板后屈曲模态变化的全过程。将云纹图输入微型计算机处理,获得了加劲板的全场位移和全场应力的分布情况。用投影云纹法所测得的结果同理论计算值基本吻合。     

截锥形弹穿甲单加筋板的破坏特性

为准确掌握截锥形弹体垂直穿透单加筋板后的打击深度,需要清楚知道弹体穿甲加筋板后的剩余速度.截锥形弹正穿甲板架,形成与截锥面相同的凿块,面板产生花瓣形破坏,腹板受到锥面的挤压发生塑性变形,翼板发生翻转,在此破坏模型基础上,确定板架的能量消耗方式.穿甲过程中,板架耗能主要通过凿块的剪切变形、凿块的动能、板架的挤压塑性变形、...     

Non-symmetrical large deformation of a shallow thin conical shell

I.IntroductionItisimportanttoresearchnon-symmetricalquestionsofshallowcollicalshellsintheoryoronapplication.Asonekindofpressurevessel'sparts,shallowconicalshellsareverycommonlyusedillellgineerillgpractice,becausethedifficultyofmanul\lctul.illgthemis'small.AlthotlghwelookupmanyChineseandtbreignperiodicalswhicharctlblctobefound,wehavenotyeth'ulldarticlesanddocumentsfornon-symmetricalandnolllinearquestionsofshitllowconictllshells.Oval'rccelltyears,ProlbssorWangXinzhiandhiscolleagueshavedonealot…     

A Donnell type theory for finite deflection of stiffened thin conical shells composed of composite materials

A Donnell type theory is developed for finite deflection of closely stiffened truncatedlaminated composite conical shells under arbitrary loads by using the variational calculusand smeared-stiffener theory.The most general bending-stretching coupling and the effectof eccentricity of stiffeners are considered.The equilibrium equations,boundary conditionsand the equation of compatibility are derived.The new equations.of the mixed-type ofstiffened laminated composite conical shells are obtained in terms of the transversedeflection and stress function.The simplified equations are also given for some commonlyencountered cases.     

开孔平板的剪切稳定性实验

对四边简支和四周边受均匀剪切力的矩形薄平板的屈曲失稳,作了实验分析及数值计算.用作者所设计的剪切试验装置,对一组开孔及开孔后加强的薄平板进行了剪切稳定性试验,求得薄平板失稳时的载荷——挠度曲线及失稳波形,由曲线上拐点来确定平板失稳临界载荷,并将实验结果与有限元数值计算结果作了比较.     

Structural and acoustic response of a finite stiffened conical shell

In this paper, a precise transfer matrix method is presented to calculate the structural and acoustic responses of the conical shell. The governing equations of conical shells are written as a coupled set of first order differential equations. The field transfer matrix of the shell and non-homogenous term resulting from the external excitation are obtained by precise integration method. After assembling the field transfer matrixes, the whole matrix describing dynamic behavior of the stiffened conical shell is obtained. Then the structural and acoustic responses of the shell are solved by obtaining unknown sound pressure coefficients. The natural frequencies of the shell are compared with the FEM results to test the validity. Furthermore, the effects of the semi-vertex angle, driving force directions and boundary conditions on the structural and acoustic responses are studied.     

Stability of imperfect stiffened conical shells

A general procedure is developed for stability of stiffened conical shells. It is used for studying the sensitivity behavior with respect to the stiffener configurations. The effect of the pre-buckling nonlinearity on the bifurcation point, as well as the limit-point load level, is examined. The unique algorithm presented by the authors is an extended version of an earlier one, adapted for determination of the limit-point load level of imperfect conical shells. The eigenvalue problem is iteratively solved with respect to the nonlinear equilibrium state up to the bifurcation point or to the limit-point load level.A general symbolic code (using MAPLE) was programmed to create the differential operators based on Donnell’s type shell theory. Then the code uses the Galerkin procedure, the Newton–Raphson procedure, and a finite difference scheme for automatic development of an efficient FORTRAN code which is used for the parametric study.