流场中填充吸声材料夹层板结构的声振耦合特性

采用等效流体模拟吸声材料,建立了外部流场作用下填充吸声材料夹层板结构的声振耦合模型,应用波动分析方法研究结构中声的透射特性,分析了入射声波入射角和方位角、流场流速和流向、夹层结构几何尺寸等参数对填充吸声材料夹层板结构声振耦合特性的影响。仿真计算表明吸声材料提高了双层板结构的隔声性能;隔声性能随着面板厚度和夹层厚度的增加而提高,随着入射角和方位角的增大而减小;在计算频段内(0~5000Hz),逆流入射时传声损失随着马赫数的增大而减小,顺流入射时却随着马赫数的增大而增大。     

《圆锥壳结构声振耦合特性分析》

通过利用LMS virtual.lab中的Acoustic BEM模块实现了FE/BE 声振耦合模型的仿真计算,且计算结果通过了混响噪声实验验证。在此基础之上,分析圆锥壳结构的声振耦合特性,并与不考虑声场的结构响应的情况进行了比较分析。结果表明声场的存在影响结构的响应幅值与分布,且耦合程度在不同频率下表现出不同特性。     

复合材料加筋板计及热效应的声-固耦合分析EI北大核心CSCD

高超声速飞行器在服役时会面临高温、振动和噪声等环境,声-固耦合是其设计环节备受关注的问题之一。针对飞行器典型复合材料加筋板,采用有限元-边界元法从三种工况开展加筋板的声-固耦合分析,即仅考虑高温对材料力学性能的影响(工况一)、仅考虑热应力对结构刚度的影响(工况二)、同时考虑二者的影响(工况三)。结果表明:高温引起的材料力学性能改变降低了板的固有频率,使响应峰值升高并向低频处移动;附加热应力的存在整体上降低了板的固有频率并改变了模态振型,引起响应峰值频率向高频处移动,并在整体上抑制了加速度响应;同时考虑二者的影响时,应力响应显著增大,加速度响应显著减小,且响应峰值频率位于工况一与工况二之间;高温对声压响应影响不大。     

考虑声振耦合的平板结构声振特性优化研究

研究多个动力吸振器优化结构的声振特性。根据Hamilton变分原理建立多个动力吸振器—平板—介质系统的声振耦合动力学方程,给出简支边界条件下耦合方程的解;以吸振器的质量、刚度、阻尼和位置为设计变量,以平板结构表面平均振速级和辐射声功率级为优化目标,采用遗传算法进行优化研究。研究表明:在一定频段内,单个动力吸振器能够降低优化目标10 d B左右,采用多个动力吸振器能够控制结构较宽频带的噪声;对于水下结构,可采用两个动力吸振器进行优化,但不能将空气中吸振器的优化结果直接用于水下结构。研究结果可为动力吸振器的减振降噪设计提供理论依据。     

复合材料大变形任意加筋板单元

本文构造了用于复合材料偏心加筋板状结构大变形分析的任意加筋板单元。在此模型中,肋骨可放置在板单元内任意位置和任意方向,因而在网格划分时,可不必顾及肋骨的具体位置。在板和肋骨的基本方程中,引用Von-Karman大变形理论计及大变形的影响,按照 Mindlin-Reissoner一阶剪切变形理论考虑横向剪切变形。任意加筋板单元具有和常规板单元相同的自由度。数值计算表明本文的有限元模型具有很高的精度。     

复合材料蜂窝夹层板结构的多工况优化设计研究

以复合材料蜂窝夹层板结构作为研究对象,建立了多工况优化模型,对众多的材料设计变量进行必要的取舍,通过优化分析确定复合材料蜂窝夹层板面板各分层的厚度以及蜂窝芯层的厚度等,使结构满足相应的频率约束、屈曲约束,以及强度约束、位移约束和尺寸限制等,同时达到结构的重量最轻。采用序列二次规划法对某卫星的承力筒结构进行了优化设计,优化结果表明:在满足其振动特性以及静力学特性的条件下,复合材料蜂窝承力筒的各面板层厚度以及蜂窝芯层的厚度均有所减小,减重效果显著,较好地实现了复合材料蜂窝夹层板结构的多工况优化设计。     

复合环境激励下的声振耦合分析

基于有限元和边界元理论,建立了仪器舱典型结构的耦合模型,分析了声振耦合对结构响应的影响。当典型结构经受随机振动+混响声场复合环境激励时,采用随机分析的原理,用谱分析的分析方法定性的分析结构的动力响应情况,推导了节点响应谱密度的计算公式,解决了Sysnoise软件同时对声振复合环境进行数值模拟的问题。仿真结果表明：声振耦合影响结构的响应,且在各频率上影响程度不同,在低频时较弱,相当于附加阻尼的效果,随着频率的升高,耦合程度随之加强,改变了结构的响应分布;对声振复合环境数值模拟,在低频部分,随机振动激起的响应占主要部分,随着频率的升高,混响声场激起的响应占主要部分,混响声场激起的模态数也要多于随机振动激起来的。     

声子晶体夹层板结构的隔声性能研究

格栅夹层板材料由于其拥有耐冲击性能良好、比强度大和比刚度高等优点,已在实际工程中得到了广泛的应用.虽然格栅夹层板结构在高频段具有优良的隔声性能,但在中低频段受质量定律的限制,使得其隔声性能并不理想.声子晶体作为一种周期性的结构,因其特殊的带隙特性,使特定频率的弹性波无法在结构中传播,因而具有优良的抑制噪声传播的性能;将...     

雨滴冲击下薄板结构声振特性研究

为了研究降雨冲击船体结构所产生的振动和噪声对舱室乘客舒适性的影响,开展降雨模型冲击薄板结构的声振特性研究。单雨滴冲击外部结构所致声振分析是降雨冲击下声振特性研究的基础,因此,以薄板结构为目标对象,建立单雨滴冲击和连续雨滴冲击的载荷模型,利用Comsol软件研究薄板结构在雨滴冲击下声振耦合特性,分析雨滴参数和结构特征对辐射声功率影响。研究发现：雨滴大小对结构的声振特性影响显著;结构刚度对结构在雨滴连续冲击下产生的声功率级响应分布有明显影响;雨滴作用下结构的加筋类型与是否加筋对其产生的振动声辐射有显著影响,且选取合适的结构加筋方式有利于降低结构的振动声辐射;不同材质的薄板结构在雨滴冲击下的辐射声功率略有差异。研究结果对于预测舱室结构在降雨作用下产生的声能大小和对噪声进行控制具有参考价值。     

基于Virtual.Lab Acoustics的蜂窝夹层板结构传声特性分析

针对蜂窝夹层板进行传声特性仿真计算分析。基于声学间接边界元理论,利用有限元软件Patran进行夹层板的三维实体建模和模态分析,采用声学软件Virtual.Lab Acoustics计算结构的传声性能,得到场点声压分布、构件两侧声压级差和结构隔声量曲线。在此基础上系统地探讨面板厚度和密度以及芯层高度、壁厚及壁长五个设计参量对蜂窝夹层板传声性能的影响。结果显示,面板厚度与芯层高度对结构在低频段尤其是刚度控制区域的隔声性能影响显著。     

Flutter of Thermally Buckled Composite Sandwich Plates

A high precision high order triangular plate element is developed for the linear flutter analysis of thermally buckled composite sandwich plates. Due to uneven thermal expansion in the two local material directions, the buckling mode of the plate may be shifted from one pattern to another for certain fiber orientation or plate aspect ratio as the aerodynamic pressure is present. This buckle pattern change alters the frequencies and modes of the plate and that in turn changes the flutter coalescent modes. Numerical results show that temperature has a destabilizing effect on the flutter boundary but the aerodynamic pressure has a stabilizing effect on the buckling boundary.     

Buckling Analysis of Composite Sandwich Plates with Flexible Core Using Improved High-Order Theory

A new improved high-order theory is presented for global and local buckling analysis of sandwich plates with soft orthotropic core. Continuity conditions for transverse shear stresses at the interfaces as well as the conditions of zero transverse shear stresses on the upper and lower surfaces of plate are satisfied. Overall buckling loads, as well as wrinkling loads, are obtained for various sandwich plates. Effect of geometrical parameters and material properties of face sheets and core are studied on the overall buckling and face wrinkling of sandwich plates.     

Three-dimensional Finite Element Buckling Analysis of Honeycomb Sandwich Composite Shells with Cutouts

This paper investigates the buckling response of honeycomb sandwich composite shells with cutouts under axial compression. The Wilson's incompatible solid Finite Element (FE) is used around cutouts to obtain the detail stress distribution there. While to reduce the computational expense, a special multilayered relative degrees-of-freedom (DOF) shell FE is used to model the regions far from the cutouts. The efficiency and accuracy of this modeling scheme are illustrated by two benchmarks. Then parametric studies are carried out to reveal how the buckling response is influenced by the area, the shape and the orientation of cutouts.     

Computation of Laminated Composite Plates using Integrated Radial Basis Function Networks

This paper reports a meshless method, which is based on radial-basis-function networks (RBFNs), for the static analysis of moderately-thick laminated composite plates using the first-order shear deformation theory. Integrated RBFNs are employed to represent the field variables, and the governing equations are discretized by means of point collocation. The use of integration rather than conventional differentiation to construct the RBF approximations significantly stabilizes the solution and enhances the quality of approximation. The proposed method is verified through the solution of rectangular and non-rectangular composite plates. Numerical results obtained show that the method achieves a very high degree of accuracy and a fast convergence rate.     

基于灵敏度分析的复合材料层合板优化设计

工程结构中的复合材料层合板的几何参数往往具有随机性质.如何研究随机参数层合板的灵敏度,并对参数进行优化分析,这对正确估计结构设计的可靠性有着非常重要的意义.根据层合板的一阶剪切理论,采用样条有限元法,推导并建立了层合板的振动方程,刚度矩阵,质量矩阵,比例阻尼矩阵以及求解反对称层合板响应灵敏度的计算公式,在基于灵敏度分析的基础上,进行了复合材料层合板的基频分析和优化设计,并用网格法计算最佳铺层角.数值算例验证了算法的有效性.     

Static Response of Geometrically Nonlinear Laminated Composite Plates Having Uncertain Material Properties

The effect of uncertainty in material properties on the transverse bending of laminated composite plate is investigated. The transverse shear and large rotations have been included in the system equation in the framework of higher order shear deformation theory. The analysis uses Green–Lagrange nonlinear strain displacement equations to model geometric nonlinearity. The stochastic finite element analysis is performed using a direct iteration approach to handle deterministic geometric nonlinearity and perturbation approach to handle the randomness in the material properties. Mean and variance of the transverse deflection have been obtained by employing a C⁰ isoparametric nonlinear finite element model.     

Stability Analysis of Laminated Soft Core Sandwich Plates Using Higher Order Zig-Zag Plate Theory

C₀ finite element model based on higher order zig-zag plate theory is used to study the stability analysis of laminated sandwich plates. The in-plane displacement field is obtained by superposing a global cubically varying displacement field on a zig-zag linearly varying displacement field with different slope in each layer. The transverse displacement assumes to have a quadratic variation within the core and constant in the faces. The conditions regarding transverse shear stress at layer interfaces and top and bottom are satisfied. Numerical examples covering different features of laminated sandwich plates are presented to illustrate the accuracy of the model.     

Modeling and Re-Examination of Nonlinear Vibration and Nonlinear Bending of Sandwich Plates with Porous FG-GPLRC Core

In this article, an inhomogeneous model is proposed to predict the material properties of porous GPL-reinforced composite (GPLRC) and to predict the mechanical responses of a sandwich plate which consists of top and bottom metal face sheets and a porous GPLRC core. The GPLRC core is assumed to be multilayers, and each layer may have different values of porosity coefficient to achieve a piece-wise functionally graded pattern. Young's moduli along with shear modulus of porous GPLRC core are predicted by a generic Halpin-Tsai model in which the porosity is included. Thermo-mechanical properties of both metal face sheets and porous GPLRC core are assumed to be temperature-dependent. The governing equations of motion for porous sandwich plates are solved by applying a two-step perturbation approach to obtain the analytical solutions for the two cases of nonlinear vibration and nonlinear bending of porous sandwich plates. Numerical studies are performed to compare the results obtained from the present model and the equivalent isotropic model (EIM). The results reveal that, for most cases, the difference of natural frequencies between two models is over 30%, and the vibration frequency–amplitude curves and the bending load–deflection curves are underestimated by using the EIM.     

The Nonlinearly Viscoelastic Response of a Wood-Thermoplastic Composite

This study considers the time-dependent response of a woodthermoplastic composite. The extruded material under considerationconsists of wood flour embedded in a high-density polyethylene (HDPE)matrix. The characterization study is based on a series of creep andrecovery tests. Stiffness reduction (i.e. damage) and permanentdeformation was observed in the material when the creep stress amplitudeexceeded a threshold value. The damage and permanent strains were foundto depend on creep stress amplitude and duration. The permanentdeformation was more efficiently accommodated by considering the coupontotal strain, however. A nonlinearly viscoelastic model is presentedthat incorporates damage and permanent deformation effects. Damage wasmodeled by considering an effective stress. The model is shown tocompare favorably with the experimental creep/recovery data as well astwo-step load history verification tests.