树脂柱对复合材料夹层板屈曲及动力学性能的影响分析

应用有限元软件ANSYS,分析树脂柱对点阵增强型复合材料夹层板力学性能的影响.对夹层板建立物理模型,采用8节点SOLID45实体单元,计算夹层板的屈曲、自由振动以及受冲击荷载时的瞬态动力响应.研究了树脂柱的材性及分布对夹层板屈曲载荷及自振频率的影响,讨论了瞬态冲击荷载作用下树脂柱对降低竖向动力位移的正面作用.结果显示,树脂柱的存在对夹层板的力学性能有一定影响,其中树脂柱的材性对夹层板屈曲及动力学特性的影响有限,而树脂柱的疏密程度对点阵增强型复合材料夹层板的力学性能有着明显的改进作用.     

几何参数对旋转薄壁圆柱壳振动特性的影响

摘 要: 本文基于Love壳体理论对旋转薄壁圆柱壳的自由振动特性进行分析,讨论几何参数对圆柱壳振动特性的影响。针对五种边界条件,分别分析厚度与半径之比、半径与长度之比对旋转薄壁圆柱壳固有频率特性的影响;探讨半径与长度之比对系统振型比的影响。分析结果表明：圆柱壳固有频率随着厚度与半径之比的增加而单调增加,增加幅度较小。半径与长度之比对圆柱壳固有频率与振型比的影响显著,且随其增大固有频率及振型比均不单调变化。由此可知,细长圆柱壳的振动特性与短粗圆柱壳的振动特性差异显著,研究结果为圆柱壳的动力学分析提供理论依据。     

主动约束层阻尼圆柱壳动力学分析的新传递矩阵法

基于作者最近导出的被动约束层阻尼(PCLD)圆柱壳的一阶整合矩阵微分方程,结合压电材料本构关系和比例微分负增益反馈控制策略(PD),建立了一种求解主动约束层阻尼(ACLD)圆柱壳动力学问题的新传递矩阵方法。提出的ACLD圆柱壳的一阶矩阵微分方程,采用了简化的机电耦合模型。通过对ACLD圆柱壳自由振动及其在地震激励作用下的动力学响应分析,表明ACLD圆柱壳的阻尼特性和减振效果相对于PCLD圆柱壳具有明显优势,并且发现采用周向分块敷设ACLD,且施加与结构变形中的占优模态相匹配的控制电压分布方式对地震激励的抑制效果更好。     

功能梯度点阵夹层结构抗爆性能数值仿真研究

为进一步提高点阵夹层结构的抗爆性能,提出了面板上薄下厚,芯层上细下粗(正向梯度化)的功能梯度点阵夹层结构,利用ANSYS/LS-DYNA有限元软件对新结构的抗爆性能进行了数值模拟研究。分别探讨了面板梯度化、芯子梯度化对结构抗爆性能的影响,并对功能梯度点阵夹层结构的各尺寸参数做单因素分析。结果表明,同时考虑面板和芯子的正向梯度化能大幅度提高点阵夹层结构吸能,面板正向梯度化对吸能的贡献比例高于芯子梯度化。此外,由单因素分析可知,上下面板厚度、芯层厚度以及芯杆与下面板之间的夹角对抗爆性能影响很大,芯杆上下截面边长对抗爆性能的影响相对较小。     

薄壁圆柱壳在流体脉动激励下的振动特性分析

摘要：为深入研究薄壁圆柱壳在流体脉动激励下的运动特性,应用Donnell简化壳理论,考虑阻尼、结构非线性和附加质量的影响,建立了薄壁圆柱壳在流体脉动激励下的非线性振动方程。基于Galerkin方法将偏微分方程转化为方便求解的常微分方程,利用多尺度法求解了系统主共振的一次近似解,得到了系统稳态响应的转迁集与分岔图,并通过奇异性分析,得到了系统工作稳定性和可靠性的结构参数区域。对薄壁圆柱壳在流体作用下的振动特性进行了数值模拟和实验研究,考察了阻尼系数、脉动频率、液体深度等对系统动力学特性的影响。研究表明,考虑阻尼、结构非线性和附加质量的非线性振动方程更能体现薄壁圆柱壳在流体脉动激励下完整的动力学特性,同时系统中存在多种分岔行为。     

新型矩形蜂窝夹芯夹层加筋圆柱壳抗水下爆炸冲击载荷分析

提出了一种新型矩形蜂窝夹芯夹层加筋圆柱壳结构形式。分析了其在水下爆炸冲击载荷下的动力响应特征及     

层合薄壁圆柱壳1:1内共振研究

针对一端固定,一端自由的层合薄壁圆柱壳模型,根据Donnell’s非线性简化壳理论建立其非线性振动方程。采用Galerkin方法对非线性振动方程进行离散化,应用平均法对系统包含两个相邻轴向模态的非线性振动响应进行了解析分析,与数值模拟进行了比较,并得到了不同参数对层合薄壁圆柱壳复杂的振动响应的影响。结果表明,1）由于所选的两个相邻轴向模态频率相距较近,能量在两个模态之间相互传递,系统存在1:1内共振现象;2）系统复杂的振动响应受激振力大小和非线性项的影响比较大,而对于阻尼不敏感。     

非轴对称移动载荷下有限长圆柱厚壳的动力响应

本文在介绍圆柱厚壳应力与位移理论分析发展的前提下,建立了有限长圆柱厚壳在非轴对称移动载荷作用下的三维力学模型,假设沿厚度方向径向剪切应变二次分布、径向正应变线性分布,且建立了为满足边界条件待定的位移表达式,采用Heaviside函数和Dirac函数表达移动和作用变化着的移动载荷的基础上,用最小势能原理建立了该圆柱厚壳的动力学微分方程组,应用Galerkin法和修正的Runge–Kutta–Fehlberg法,求得了非轴对称移动载荷作用下的圆柱厚壳的动力响应。通过具体算例,对有限长圆柱厚壳的位移响应和应力状态进行了分析,并将动态响应的理论解与ANSYS数值解进行了对比,从而相互印证了解的可靠性。     

轻质弱辐射的阻尼夹芯复合材料圆柱壳的优化设计

基于三维弹性理论,对阻尼夹芯复合材料圆柱壳在简谐点力作用下的振动声辐射进行优化研究。建立了以总质量、基频和模态阻尼为优化目标的多目标函数优化模型,对纤维层和芯层厚度分布和铺层方式进行优化设计;经与其他文献及"有限元+边界元"法得到的结果对比,验证了三维弹性理论的计算结果的有效性;分析了三明治夹芯圆柱壳的振动和声辐射的影响因素,发现芯层中面线位置高于整壳中面线时有利于提高基频,降低声辐射功率;且随着铺层角的增加,固有频率呈抛物线型变化趋势,模态阻尼比则逐渐减小。经优化设计,声功率一阶共振频率向高频方向偏移20 Hz,最大声功率降低11.66 dB,200 Hz以下的低频段,声功率峰值密度明显降低。     

流体绕流不同方向振动圆柱换热特性数值分析

基于Fluent动网格及UDF编程技术对二维流场中振动圆柱的换热特性进行了研究,分析了来流速度及圆柱振动方向对其换热特性的影响。数值计算结果表明,相比于静止圆柱换热,当圆柱的最大振动速度远大于来流速度时,其振动强化传热效果显著;随着流速的增大,振动圆柱的强化传热效果降低,当流速为圆柱最大振动速度的4倍时,圆柱传热效果仅增强1.2%。另外,对相等流速下的圆柱沿不同方向的振动换热特性研究表明,振动方向对圆柱强化换热的影响不显著。     

复合材料夹层板芯层内树脂柱对性能的影响

应用商业有限元软件ANSYS,将芯层树脂柱和泡沫分开划分单元,对含有树脂柱的点阵增强型复合材料夹层板建立物理模型,进行弹性力学分析。研究了树脂柱分布和材料特性对芯层与面层间的应力分布以及板竖向位移的影响,分析了树脂柱对于增强面层和芯层间抗剥离能力的作用。结果显示,树脂柱的存在增加了夹层板的抗弯刚度,树脂柱的材料特性和疏密程度对夹层板上芯层与面层层间的应力分布有一定的影响。     

Blast resistance and energy absorption of foam-core cylindrical sandwich shells under external blast

The early time, through-thickness stress wave response of a foam-core, composite sandwich cylindrical shell under external blast is examined in this paper. Solutions for the transient response of the facesheets were derived as stress waves propagated through an elastic–plastic, crushable foam core. These solutions were found to be in good agreement with results from finite element analysis. The blast response of the composite sandwich cylindrical shell was shown to be affected by the magnitude and duration of the pressure pulse. High amplitude, low duration (impulsive) pressure pulses induced the greatest energy absorption. Low amplitude, long duration pressure pulses caused minimal energy absorption. The amount of energy absorbed increased and the failure load decreased with increasing core thickness. Sandwich shells with foams of varying density, compressive modulus and crushing resistance were also examined. The sandwich shells with the foam of the highest density, compressive modulus and crushing resistance (Divinycell HCP100) were found to be the most blast resistant to failure even though no energy was absorbed by them. Per unit weight, however, the shells with a lighter, less stiff and strong, Divinycell H200 foam core were more blast resistant to failure than shells with a Divinycell HCP100 foam core.     

Analysis of Laminated and Sandwich Composite Structures Using Solid-like Shell Elements

A new solid-like shell element was formulated which is suitable for analysis of laminated and sandwich composite structures. Then, a multiscale analysis technique was implemented to the shell element formulation so that micro-level stresses and strains (i.e. stresses and strains in reinforcing fibers and the binding matrix) in those structures can be computed. The shell element has three displacement degrees of freedom per node like a 3-D solid element. Therefore, the shell elements can be stacked easily on top of one another like 3-D solid elements in order to represent multiple layers through the thickness of laminated and sandwich structures. The effect of a thin resin or adhesive layer in laminated and sandwich composite structures was investigated on both static and the dynamic responses of the structures using the developed shell elements. The study showed an apparent effect of the resin/adhesive layer even though it is very thin. As a result, the present shell element can be used effectively to include those thin layers in finite element analysis models of laminated and sandwich composite structures.     

缝合泡沫夹层复合材料低速冲击数值模拟及实验

在ABAQUS分析平台中建立了缝合泡沫夹层复合材料在低速冲击下的动力学有限元模型,采用杆单元模拟缝线树脂柱的作用,基于Hashin破坏准则模拟层板面内损伤,通过各向同性硬化本构模型利用等效塑性变形模拟泡沫夹芯损伤演化。针对相同铺层的缝合和未缝合泡沫夹层结构,模拟了相同冲击能量下的低速冲击响应过程及面板、泡沫的损伤情况,数值结果与实验结果吻合较好,证明了该方法的有效性和准确性。研究结果表明,在低速冲击下,泡沫夹层结构引入缝线后虽然降低了泡沫缓冲吸能的作用,使得面板表面受到较大的冲击破坏,但增强了整体刚度,增大了面板抵抗弯曲变形的能力,减小了内部面板的损伤,使其在改善复合材料面板易分层缺陷的同时还依然拥有优良的面内性能。     

水下冲击载荷用下复合材料圆柱壳的弹性响应

研究了平面阶跃冲击波作用下沉浸无限长复合材料圆柱壳的瞬态响应。首先推导了基于Flugge薄壳理论的复合材料圆柱壳的控制运动方程,然后采用反射尾流虚源法建立流体-结构的相互作用,最后采用有限差分法来求解平面冲击波作用下无限长复合材料圆柱壳的控制运动微分方程。详细考察了复合材料纤维方向和壳的半径对复合材料圆柱壳的无因次中面应变、第0阶模态径向位移和第1阶模态径向速度的影响。     

Transient response of a submerged cylindrical foam core sandwich panel subjected to shock loading

Predicting the dynamic response of submerged vehicles subjected to hydrostatic pressure and underwater shock loading is of great interest to many structural designers and engineers for improving material and configuration design in recent years. In this paper, the finite element method is used to evaluate the dynamic response of a submerged cylindrical foam core sandwich panel subjected to shock loading. The sandwich panel consists of a foam core surrounded by fiber-reinforced laminates. The effect of fluid–structure coupling is included in the finite element analysis whereas the fluid is assumed to be compressible and inviscid. Time histories of circumferential stress for different composite plies are presented in graphical form and the effects of core type on circumferential stress and velocity of stand-off point are also investigated. Additionally, the distribution of pressure in fluid domain and the deformation of cylindrical foam core sandwich panel are estimated. To the best of the authors’ knowledge, the specialized literature addressing the dynamic response of submerged cylindrical foam core sandwich panel to underwater shock loading is rather scanty. This work is likely to fill a gap in the specialized literature on this topic.     

明胶鸟弹撞击复合材料蜂窝夹芯板试验

开展明胶鸟弹撞击复合材料蜂窝夹芯板试验,研究夹芯结构在软体高速冲击下的损伤形式,分析相关因素对结构动态响应结果的影响。通过CT扫描对复合材料蜂窝夹芯板内部进行检测可知,面板出现分层、基体开裂、纤维断裂、凹陷、向胞内屈曲等损伤形式,蜂窝芯出现芯材压溃、与面板脱粘的损伤形式;分析复合材料蜂窝夹芯板后面板的动态变形过程及撞击中心处位移-时间数据可知,复合材料蜂窝夹芯板在撞击过程中出现由全局弯曲变形主导和局部变形主导的两种变形模式;通过对比不同工况下的复合材料蜂窝夹芯板损伤程度可知,复合材料蜂窝夹芯板损伤程度随鸟弹撞击速度的增加而增大;蜂窝芯高度为10 mm的复合材料蜂窝夹芯板较蜂窝芯高度为5 mm的复合材料蜂窝夹芯板的损伤程度大;初始动能较大的球形鸟弹较圆柱形鸟弹对复合材料蜂窝夹芯板造成的冲击损伤程度更大。      

聚脲弹性体夹芯防爆罐抗爆性能研究

应用ANSYS/LS-DYNA有限元软件对三种防爆罐在1.2kgTNT爆炸载荷作用下的动态响应过程进行数值模拟。研究了无夹层、聚脲弹性体夹层和橡胶夹层防爆罐的抗爆性能。分析了不同夹层对防爆罐整体变形的影响,并分析了聚脲弹性体和橡胶夹层的吸能特性。通过聚脲弹性体夹层防爆罐在爆炸载荷作用下的变形试验研究,验证了数值计算结论的可靠性。结果表明,在相同爆炸载荷作用下,无论是在变形还是在能量吸收方面,聚脲弹性体夹层防爆罐都要优于无夹层防爆罐和橡胶夹层防爆罐;冲击波在聚脲弹性体传播过程中衰减幅度最大。     

Influences of shear stresses on the dynamic instability of exponentially graded sandwich cylindrical shells

The aim of present study is to investigate the dynamic instability of exponentially graded (EG) sandwich cylindrical shells under static and time dependent periodic axial loadings using the shear deformation theory (SDT). The modified Donnell-type dynamic instability equations of EG sandwich cylindrical shells based on the SDT are deduced. Then are reduced to Mathieu-Hill equation and by solving the expressions for the boundaries of instability regions of EG sandwich cylindrical shells are obtained. The similar expressions for EG single-layer shell, ceramic-rich shell and metal coated sandwich cylindrical shell on the basis of SDT and classical shell theory (CST) are obtained in a special case. The numerical illustrations concern the influences of compositional profiles of coating layers, shear stresses and geometrical parameters of sandwich cylindrical shells on the boundaries of instability regions. As a check on the accuracy of the present study, the values of the lower and upper boundaries of instability regions are compared with those in the literature.