任意支承条件下连续板系结构的有限板块解法

本文基于薄板小挠度弯曲理论，构造出板元内部解析，边界挠度和边界法向弯矩以带补充项的付氏级数逼近，同时考虑域内多点支承作用的板元位移函数，给出了一处适用于任意支承条件下连续板系结构的有限板块法求解格式。数值计算结果表明：本文的方法具有良好的计算精度和计算效率，适于工程应用。     

受轴对称分布荷载的厚度按指数函数变化的圆薄板的大挠度

本文用配点法计算厚度按指数函数变化的圆薄板的大挠度。荷载为轴对称分布荷载及均布边缘力矩。边界可为弹性支承。受均布荷载,在固定夹紧边条下,向摄动法的结果作了比较。     

用边界元法求解薄板大挠度弯曲问题

本文提出一个用边界元法求解薄板大挠度弯曲问题的方法,利用此方法计算了部分算例。其中:圆板、椭圆板的计算结果与已有文献的结果进行了比较,实践证明:本文提出的方法是十分满意的;对于椭圆板情形,本文的结果比Nash,W,A,的结果更接近于实验值。 本文提出了处理域积分的半解析半数值法(HAN)并首次计算了半圆板、半椭圆板及正三角形板的大挠度弯曲问题,这些问题的解还未见到有关文献讨论过。     

用配点法计算受轴对称分布荷载的圆形大挠度板

本文以幂函数多项式作位移函数,用配点法计算了受轴对称分布荷载的圆形大挠度板。文中考虑了固定夹紧、可移夹紧、铰链支承、简单支承等四种边界条件。在计算例题中,荷载采用多项式形式、余弦函数形式的分布荷载以及均布边弯矩荷载或者由它们组合而成的荷载。通过上百个例题的计算,表明此法具有精度高、收敛快等优点。本文还将其所得的结果同用摄动法等得到的结果进行了比较。     

用加权余量法分析固支圆板和环板在Mises屈服条件下的极限荷载

应用加权余量法求出了承受线性荷载的固支圆板和承受均布荷载的内边界支承环板在 Mises屈服条件下的极限荷载的近似值 ,并与最大弯矩极限条件结果进行了比较 ,说明本文计算结果较合理。     

阶梯型截面Timoshenko梁边界支承的线性静力识别方法

研究了阶梯型截面Timoshenko梁边界支承刚度的挠度识别法和挠度-应变识别方法.利用Heaviside函数,得到了任意载荷作用下阶梯型截面Timoshenko梁弯曲变形的解析通解,并利用解析通解中的待定常数给出了梁边界支承刚度的表达式.基于阶梯型截面Timoshenko梁挠度和梁表面轴向应变的测量值,利用最小二乘法,得到确定弯曲通解中待定常数的线性代数方程组,进而分别建立了挠度识别法和挠度-应变识别方法,分析了测量点数目和位置以及梁变截面位置等对两种识别方法误差敏感度的影响,给出了挠度或轴向应变的最佳测量方案.通过数值试验,考察了两种识别方法的可靠性和适用性,结果表明:挠度-应变识别方法对系统测量误差具有较好的鲁棒性,适用于实际工程中梁构件边界支承刚度的识别.     

环板在局部线性荷载作用下的塑性极限分析的计算方法探讨

本文结合环板在线性荷载作用下的塑性极限分析问题,给出一种简便的计算方法,即奇异函数法。文中用此法计算了具有外边界或内边界支承的环板的极限荷载,并画出几何参数对极限荷载的影响曲线。所得的结果具有良好的规律性而且是比较合理的。     

具有域内支承的中厚板的边界元法分析

本文借助简化的Reissner理论,利用边界元法对具有域内支承的中厚板进行了分析。建立了相应的边界积分方程,导出了各基本解,讨论了域内支承柱对板的支承情况,编制了计算程序并给出部分算例。     

边缘弹性约束圆薄板的大挠度分析

本文用微分求积法对边缘受弹性约束的弹性圆薄板进行了大挠度分析，详细研究了不同轴对称载荷情况下，边缘面内约束刚度和转动约束刚度对圆板挠度及应力的影响；给出了完全自由或完全固定边界支持计算模型的条件。所得计算结果结论对于工程设计具有一定的指导意义。     

考虑轴力二阶效应悬臂梁的支承及裂纹参数识别

建立了轴向压力作用下悬臂裂纹梁边界支承和裂纹损伤程度识别方法．首先,将悬臂梁边界非完整支承等效为竖向和扭转弹簧、梁中开裂纹等效为内部扭转弹簧,利用Laplace变换,得到了边界弹性支承、考虑轴向压力二阶效应、具有任意裂纹数目Euler-Bernoulli悬臂梁弯曲挠度的解析解．其次,提出了边界弹性支承弹簧柔度和裂纹等效扭转弹簧柔度的识别方法．最后,通过数值试验,考察了轴向压力,裂纹深度以及测量误差等对识别结果的影响,说明了本文考虑轴向压力二阶效应的悬臂梁边界支承弹簧柔度及裂纹等效扭转弹簧柔度识别方法的适用性和可靠性,结果表明：相比于应变测量误差,挠度测量误差对裂纹损伤程度识别结果影响更加敏感,且轴向压力对裂纹损伤程度识别影响较小,因此,应严格控制挠度的测量误差．同时,边界支承扭转弹簧柔度的识别误差大于其竖向弹簧柔度识别误差．这些结果为实际工程中边界非完整支承悬臂裂纹梁的参数识别提供了指导．     

钢筋混凝土双肢剪力墙静力弹塑性分析

建立了由墙肢单元模型、连粱单元模型和连接单元模型组成的钢筋混凝土双肢剪力墙的静力弹塑性分析计算模型。墙肢单元采用以有限元为基础的宏模型;按是否出现对角线剪切破坏,分别建立短连粱计算模型和长连粱计算模型;为计及连粱与墙肢连接界面的相对位移,建立用复合弹簧模拟的连接单元计算模型;给出了确定模型参数的方法。对有关文献的短连粱和长连粱双肢剪力墙试件进行了静力弹塑性分析,分析结果与试验结果符合较好。     

On the application of mixed method to solve solids of revolution with discrete fixed supports

In this paper, the force method of statically indeterminate structure mechanics is used to treat the solids of revolution with discrete fixed supports. The reactionary forces of discrete fixed supports are considered as statically indeterminate unknown variables. The force-method canonical equations, in which the coefficient matrix and the right-hand vector are computed by semi-analytical finite element method, are solved. Then the finite element solution of solid of revolution with discrete fixed supports is calculated with the external loads superposed from the assigned external loads and the reactionary forces of discrete supports.     

Influence of boundary conditions relaxation on panel flutter with compressive in-plane loads

The influence of boundary conditions relaxation on two-dimensional panel flutter is studied in the presence of in-plane loading. The boundary value problem of the panel involves time-dependent boundary conditions that are converted into autonomous form using a special coordinate transformation. Galerkin's method is used to discretize the panel partial differential equation of motion into six nonlinear ordinary differential equations. The influence of boundary conditions relaxation on the panel modal frequencies and LCO amplitudes in the time and frequency domains is examined using the windowed short time Fourier transform and wavelet transform. The relaxation and system nonlinearity are found to have opposite effects on the time evolution of the panel frequency. Depending on the system damping and dynamic pressure, the panel frequency can increase or decrease with time as the boundary conditions approach the state of simple supports. Bifurcation diagrams are generated by taking the relaxation parameter, dynamic pressure, and in-plane load as control parameters. The corresponding largest Lyapunov exponent is also determined. They reveal complex dynamic characteristics of the panel, including regions of periodic, quasi-periodic, and chaotic motions.     

A general super element for a curved beam

Corrugated panels have gained considerable popularity in a range of engineering applications, particularly in morphing skin applications. The optimum design of these structures needs simple models of the corrugated panels that may be incorporated into multi-disciplinary system models. Considering the geometric and mechanical properties of the corrugated panel, a generic super element of a corrugated core unit cell with elastomeric coating for morphing structures is investigated in this paper. The super element captures the small deformation of a 2D thin curved beam with variable curvature and is based on an exact analytical equivalent model which avoids any homogenization assumption. The stiffness matrix of a general curved beam element for a corrugated unit cell with elastomeric coating is derived. Different geometries are investigated to verify the accuracy and efficiency of the presented super element. The super element uses the geometric and mechanical properties of the panel as variables that may be applied for further topology optimization studies. The parametric studies of different corrugation shapes demonstrate the suitability of the proposed super element for application in further detailed design investigations.     

金字塔栅格夹心夹层板动力响应分析

本文将金字塔形栅格夹心夹层板假设成均匀夹心夹层板,应用Reissner夹层板理论,对其自振频率以及在简谐荷载下的强迫振动进行了研究,并以简支板为例,得到其解析解,通过与有限元分析进行比较,两者结果吻合良好。并把金字塔形栅格夹层板与同质量实体板进行比较,得出金字塔形栅格夹层板具有更好动力性能。     

Geometrically non-linear analysis of arbitrary elastic supported plates and shells using an element-based Lagrangian shell element

In the present paper, the ELF (element-based Lagrangian formulation) 9-node ANS (assumed natural strain) shell element was combined with the spring element for geometrically non-linear analysis of plates and shells sustained by arbitrary elastic edge supports that are subjected to variation in loading.This particular spring element serves as tool for modeling an arbitrary elastic edge support with 6 DOF (degrees of freedom). The elastic edge support was modeled by combining different spring models. The ANS method was used to overcome shear and membrane locking problems inherent in some thin plate and shell problems. In the formulation of the ELF characteristic arrays, the expression of element strains was adopted in the framework of the element natural coordinates. The non-linear analysis results of idealized edge supports were validated against the reference solutions available in the literature. As a result of the numerical test, the combination of the ELF 9-node shell element and spring element shows an exceptional performance for non-linear analysis of plates and shells under elastic edge supports.     

半潜式钻井平台管道钢构支架极限强度研究

钢构支架是半潜式钻井平台管道支吊架的主要类型之一,钢构支架的极限强度是管道系统正常工作的重要保障。研究结构极限强度的方法有理论分析、有限元数值仿真和实验分析。在分析极限理论的基础上由静力法计算四种钢构支架试件的极限载荷;利用MSC软件对试件极限载荷进行数值仿真分析,并对有限元模型化技术进行讨论;对试件进行实验极限载荷测试,对比分析了三种方法测得的极限载荷。结果表明,三种分析方法计算得到结构的极限载荷基本一致,对于结构形式较为简单的结构通过理论分析可以得到简化解析解析解;数值仿真分析中采用合理的有限元模型化技术(结构有限元模型、边界、约束等)可得到精度较高的计算结果。     

Delamination in sandwich panels due to local water slamming loads

We study delamination in a sandwich panel due to transient finite plane strain elastic deformations caused by local water slamming loads and use the boundary element method to analyze motion of water and the finite element method to determine deformations of the panel. The cohesive zone model is used to study delamination initiation and propagation. The fluid is assumed to be incompressible and inviscid, and undergo irrotational motion. A layer-wise third order shear and normal deformable plate/shell theory is employed to simulate deformations of the panel by considering all geometric nonlinearities (i.e., all non-linear terms in strain–displacement relations) and taking the panel material to be St. Venant–Kirchhoff (i.e., the second Piola–Kirchhoff stress tensor is a linear function of the Green–St. Venant strain tensor). The Rayleigh damping is introduced to account for structural damping that reduces oscillations in the pressure acting on the panel/water interface. Results have been computed for water entry of (i) straight and circular sandwich panels made of Hookean materials with and without consideration of delamination failure, and (ii) flat sandwich panels made of the St. Venant–Kirchhoff materials. The face sheets and the core of sandwich panels are made, respectively, of fiber reinforced composites and soft materials. It is found that for the same entry speed (i) the peak pressure for a curved panel is less than that for a straight panel, (ii) the consideration of geometric nonlinearities significantly increases the peak hydrodynamic pressure, (iii) delamination occurs in mode-II, and (iv) the delamination reduces the hydroelastic pressure acting on the panel surface and hence alters deformations of the panel.     

大开口复合材料加筋壁板稳定性分析

运用大型有限元软件Patran/Nastran分析了大开口复合材料加筋壁板的稳定性,并对不同加筋方式下壁板屈曲特征值和屈曲模态图进行了比较。结果表明:补强提高了大开口复合材料壁板的稳定性,但往往无法达到很好的效果,需要通过加筋改善其稳定性;加筋复合材料壁板稳定性较原有模型有较大提高;加筋大开口复合材料壁板屈曲特征值随筋条距开口中心距离的增加而减小,其屈曲分界线均位于筋条布置处;纵筋大开口复合材料加筋壁板一阶屈曲特征值为2.13,而横筋只达到1.08;纵筋布置对复合材料壁板稳定性影响明显高于横筋布置,可在实际工程应用中适当增加纵筋的布置。     

Stability of a thin panel with added elements in a supersonic gas flow

Thin elastic panels subjected to compression in the median plane and to supersonic gas flow are considered. An element is attached to the panel by an elastic spring and linear dashpot. The stability of the initial planar state of the panel is studied as a function of the main control parameters—such as the gas velocity and membrane force—and the parameters of the attached element. The evolution of the stability regions in the control-parameter plane is considered. Special attention is paid to compound bifurcation points and stabilization islets. Institute of Machine Science, Russian Academy of Sciences, Moscow, Russia. Translated from Prikladnaya Mekhanika, Vol. 35, No. 12, pp. 3–10, December, 1999.