余弦分布压力下矩形薄板的屈曲

针对不同支承条件,两对边受半余弦非线性分布压力下弹性矩形薄板的屈曲问题,进行了分析研究。对于只产生对称变形的矩形薄板,基于辛弹性力学的平面矩形域理论,给出了精确的面内应力分布。运用Galerkin法分析计算了半余弦分布压力下矩形薄板的屈曲载荷。根据各种不同支承矩形薄板弯曲的位移边界条件,借助于符号运算软件Maple,编写了相应的用户计算程序。对九种不同支承组合下的弹性矩形薄板进行了计算,得到了不同长宽比矩形薄板的屈曲载荷系数。通过与已有文献结果的比较表明,该文求解方法是有效和精确的。基于所给出的结果,可望为解决矩形薄板在非线性分布载荷下的屈曲分析提供一种新的研究方法。     

矩形薄板面内非线性分布载荷下的辛弹性力学解

用辛弹性力学理论,根据平面矩形域本征向量展开解法,得到了对应于零本征值和非零本征值的本征向量解,以及含待定常数的面内应力分布通解,依据必须满足的应力边界条件,利用符号运算软件Maple,导出了矩形薄板在半余弦分布载荷作用下的面内应力表达式。为了验证方法的有效性和所得到的公式的正确性,具体分析了正方形薄板在两种非线性形式载荷——半余弦和抛物线分布载荷作用下的例子。算例结果与微分求积法及其有限元法得到的数值结果极其相近。基于所给出的结果,可望为工程应用中的屈曲分析提供合理的前期准备。     

弹性压应力波作用下矩形薄板动力屈曲解析解

根据板的非线性动力平衡方程和压缩波前附加约束方程,基于双特征参数法和应力波理论,求解了矩形薄板在面内轴向冲击载荷作用下动力屈曲位移的解析解。揭示了矩形薄板动力屈曲过程中板的厚宽比、屈曲模态、冲击载荷大小和临界屈曲长度之间的关系。求得的屈曲模态与之前文献中用差分解得出的结果吻合良好。     

三边简支一边固支矩形薄板动力屈曲解析解

根据板的动力平衡方程和压缩波前附加约束方程,基于双特征参数法和应力波理论,求解了三边简支一边固支矩形薄板在面内轴向冲击载荷作用下动力屈曲位移的解析解。揭示了矩形薄板动力屈曲过程中板的厚宽比、屈曲模态、冲击载荷大小和临界屈曲长度之间的关系。计算结果表明,由于横向惯性效应的存在,动力屈曲的临界载荷要比静力屈曲的大得多。     

热声载荷下薄壁结构非线性振动响应分析及疲劳寿命预测

基于时域分析法研究了金属薄壁结构在热声载荷下的非线性振动响应特性,并采用四种应力寿命模型预测了薄板梁的热声疲劳寿命。以典型薄板梁为研究模型,首先研究了单一噪声激励下薄板梁的时域响应特性及热载荷对其响应特性的影响机理,并仿真分析了薄板梁在热声激励下的非线性响应特性。在此基础上,运用雨流法统计了薄板梁根部的应力响应,并基于Miner线性累积损伤理论采用Goodman、Morrow、Walker和修正Walker应力寿命模型预测了薄板梁在不同工况下的热声疲劳寿命。研究结果表明：薄板梁的热模态基频在其热声疲劳问题中起主导作用;薄板梁热屈曲后的非线性跳变响应将增大应力幅值,从而严重削弱结构的预期寿命;噪声载荷是影响屈曲前薄板梁热声疲劳寿命的主要因素,而热载荷是影响屈曲后热声疲劳寿命的主要因素。因此在薄壁结构抗热声疲劳设计中必须重点考虑热声载荷联合作用的影响。     

固定边载流矩形板的磁弹性效应分析

针对在电磁场和机械场耦合作用下的载流矩形板的二维磁弹性问题进行了研究.在给出矩形薄板的磁弹性非线性运动方程、几何方程、物理方程、电动力学方程和Lorentz力表达式的基础上,建立了差分格式和线性化迭代方程,给出了这些方程的数值解系统,并以固定边矩形板为例,计算了该板在电磁场和机械载荷耦合作用下的应力及变形,研究了侧向电...     

横向磁场中对边简支对边固支矩形薄板的分岔与混沌

研究了力磁耦合作用下对边简支对边固支矩形薄板的分岔与混沌问题。在给出横向稳恒磁场和载荷共同作用下的矩形薄板的非线性磁弹性耦合运动学方程的基础上,得到了对边简支对边固支的矩形薄板的磁弹性振动方程。用Melnikov函数法给出该系统发生混沌运动的条件,并用数值方法求解该系统振动方程。通过具体算例,得到了系统的分岔图、Lyapunov指数图,并给出了相应位移波形图、相平面轨迹图、庞伽莱截面图。分析了电磁场参量及外载荷对系统运动状态的影响。     

均布载荷作用下圆薄板的自由振动

本文讨论了均布载荷作用下圆薄板在非线性弯曲静平衡构形附近的微幅自由振动。静平衡问题采用文献［２］给出的精确解，在此基础上用修正迭代法求解，得到了其固有频率－载荷特征关系。     

矩形薄板在面内撞击下动力屈曲的实验研究

利用Hopkinson压杆系统对矩形薄板在面内撞击下的动力屈曲进行了实验研究。结果表明矩形薄板存在屈曲后强度,在屈曲发生后面内载荷可以继续增加,通过记录屈曲发生的时间求得临界屈曲长度,并对实验模型进行了理论分析。对比分析结果表明,当压应力波向前传播一定距离后矩形薄板发生局部屈曲,得到的临界屈曲长度与理论计算结果吻合良好。     

横向磁场中机械载荷作用梁式薄板的非线性主共振

研究了磁场环境中受机械载荷作用梁式薄板的非线性主共振问题。在给出薄板的非线性电磁弹性耦合运动基本方程及电磁力表达式的基础上，得到了横向稳恒磁场和机械载荷共同作用下梁式薄板的振动方程。应用伽辽金积分法，并进行无量纲化处理，进一步导出了相应的非线性振动微分方程。采用平均法对主共振问题进行了求解，得到了稳态运动下的幅频响应方程。通过算例给出了几种情况下的幅频响应曲线图和时间历程图，分析了板厚和磁场对系统振动的影响。     

Thermomechanical postbuckling analysis of functionally graded plates and shallow cylindrical shells

Summary. In this paper, an analytic solution is provided for the postbuckling behavior of plates and shallow cylindrical shells made of functionally graded materials under edge compressive loads and a temperature field. The material properties of the functionally graded shells are assumed to vary continuously through the thickness of the shell according to a power law distribution of the volume fraction of the constituents. The fundamental equations for thin rectangular shallow shells of FGM are obtained using the von Karman theory for large transverse deflection, and the solution is obtained in terms of mixed Fourier series. The effect of material properties, boundary conditions and thermomechanical loading on the buckling behavior and stress field are determined and discussed. The results reveal that thermomechanical coupling effects and the boundary conditions play a major role in dictating the response of the functionally graded plates and shells under the action of edge compressive loads.     

Dynamic response of initially stressed functionally graded rectangular thin plates

This paper deals with the dynamic response of initially stressed functionally graded rectangular thin plates subjected to partially distributed impulsive lateral loads and without or resting on an elastic foundation. Material properties are assumed to be temperature-dependent, and graded in the thickness direction according to a simple power law distribution in terms of the volume fractions of the constituents. The plate is assumed to be clamped on two opposite edges and the remaining two edges may be simply supported or clamped or may have elastic rotational edge constraints. The formulations are based on classical small deflection plate theory, and account for the plate–foundation interaction effects by a two-parameter model (Pasternak-type). A one-dimensional differential quadrature approximation and the Galerkin procedure are employed in the free vibration analysis, and the Modal Superposition Method is used to determine the transient response of the plate structure. A parametric study is carried out. Effects of constituent volume fraction index, foundation stiffness, plate aspect ratio, the shape and duration of impulsive load, as well as the initial membrane stresses on the dynamic response of FGM plates are studied. Comprehensive numerical results for silicon nitride/stainless steel rectangular plates are presented in dimensionless tabular and graphical forms.     

点载静力梁函数在求解矩形薄板自振特性中的应用

本文选择一组点载静力梁函数作为基函数，应用李兹法近似求解矩形薄板的自振特性，计算了多种边界条件下各种长宽比的矩形薄板的自振频率，与其它方法相比，本文方法具有很好的精度和收敛性，且计算非常简单直接。     

Nonlinear transient response of orthotropic thin rectangular plates on elastic foundations

This paper presents geometrically nonlinear transient analysis of rectilinearly orthotropic thin rectangular plates resting on Winkler and Pasternak foundations for uniformly distributed step function and sinusoidal pulse loadings. The orthogonal point collocation method in the space domain and Newmark-β scheme in the time domain are employed. Immovable clamped and simply-supported plates are analysed. An approximate method is used to predict the maximum dynamic response to step loads from the results for static loads and is found to yield sufficiently accurate results.     

Buckling analysis of orthotropic thin rectangular plates subjected to nonlinear in-plane distributed loads using generalized differential quadrature method

In the present work, buckling analysis of orthotropic thin rectangular plates with uniform thickness resting on Pasternak foundation are investigated for eight types of boundary conditions: SSSS, CCCC, SCSC, SSSC, SSCC, CCCF, SSFC, and CFCF. Based on classical plate theory, governing differential equation in buckling are solved numerically using generalized differential quadrature method (GDQM) to obtain critical buckling loads and corresponding modes. The kinds of nonlinear loading are presented in six cases including symmetrical and unsymmetrical distribution. In addition, the effects of aspect ratio, orthotropic moduli ratio and coefficients of foundation on the buckling load are illustrated. The present work is the first attempt to consider the influence of the nonlinearity of distributed in-plane bi-directional loading in determination of buckling load and representation of the corresponding shape modes. Some numerical examples are provided to demonstrate good accuracy of the GDQ method to evaluate the critical buckling load in case of nonlinear distributed bi-directional compressive loads. As shown, profile of distributed in-plane loading plays an important role on buckling behavior of the rectangular plate.     

Numerical analysis of dynamic buckling of rectangular plates subjected to intermediate-velocity impact

This paper numerically investigates the dynamic buckling of thin imperfect rectangular plates subjected to intermediate-velocity impact loads. From numerical results obtained, a dynamic buckling and a dynamic yielding critical condition are defined, and the corresponding critical dynamic loads are estimated. Numerical model employed in the present study is validated by experimental data reported earlier. Results from parametric study indicate that initial imperfection and load duration have significant influence on the dynamic buckling of the plates. The smaller the initial imperfection and the load duration, the higher the dynamic buckling critical loads of the plates. Moreover, different hardening ratios of plate material also affect the elastic–plastic dynamic buckling properties of the plates. If the plate buckles plastically, the dynamic buckling load increases as the hardening ratio of plate material increases. Unlike thin plates under high-velocity impact that buckling always occur after load application, plates under intermediate-velocity impact analyzed in the present study all buckle during the loading phase.