共查询到18条相似文献,搜索用时 140 毫秒
1.
采用梁函数组合法对功能梯度复合材料矩形板进行动力特性分析,提出了适用于每边任取简支、固定、自由边界之一 (包括36种边界) 、材料功能梯度沿厚度任意分布的矩形板固有频率与振型的解析解一般表达式;在简化情况下,给出了各种边界条件功能梯度矩形板固有频率解的直接显式。所给出的固有频率与振型解的结果可用于功能梯度板的动力分析,工程上应用广泛,简明实用。 相似文献
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板结构与其他构件的装配关系可用不同的边界条件进行模拟,然而针对不同边界条件的板结构进行动力学特性分析,目前缺乏统一的数学建模方法。以混合弹性边界条件下加筋、开孔的板类结构的横向振动为例,利用Rayleigh-Ritz法和模态叠加法求解矩形加筋多孔板在简谐激励下的动力学响应问题。采用将开孔板与加强筋沿交界面进行分离,结合改进的傅里叶级数设定开孔板的横向振动位移函数,利用不同刚度弹簧模拟混合弹性边界,推导加筋矩形开多孔板和边界弹簧系统的动能与势能,求解其在简谐激励下的动力学响应。经对比,理论计算结果与有限元(Finite Element Method,FEM)结果吻合良好。此外,用同样的方法分析不同孔尺寸对结构固有频率和响应的影响。研究发现,可通过改变加筋板的开孔形状、尺寸对结构的振动特性进行调整。研究成果可为混合弹性边界板结构动力分析提供一种新的技术途径,可以简化加筋开孔板结构动力分析的步骤。 相似文献
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基于经典薄板理论和Hamilton原理研究温度影响下Winkler-Pasternak弹性地基上多孔功能梯度材料(FGM)矩形板的自由振动特性。采用Voigt混合幂率模型和孔隙任意分布模型来表征多孔FGM矩形板的材料属性,并考虑多孔FGM矩形板内部均匀温升和材料具有温度依赖特性;应用物理中面推导弹性地基上多孔FGM矩形板自由振动的控制微分方程并进行无量纲化;采用微分变换法(DTM)对无量纲控制微分方程及其边界条件进行变换,引入典型的六种边界在MATLAB统一编程且保证计算精度一致,经过迭代收敛,求解出无量纲固有频率;通过算例研究了边界条件、梯度指数、升温、孔隙率、长宽比、边厚比、无量纲弹性刚度系数和无量纲剪切刚度系数对多孔FGM矩形板振动特性的影响。 相似文献
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复杂边界条件功能梯度板三维分析的细观元法 总被引:2,自引:1,他引:1
发展一种细观分析和宏观计算相结合的计算方法—细观元法。细观元法是使功能梯度构件宏观响应和材料组分的几何、物理、构造参数直接发生关联的分析方法,实现材料细观结构到构件宏观响应的直接过度分析,为解决功能梯度构件宏、细观跨尺度分析提供了一种有力工具。细观元方法不增加结点自由度,却使得功能梯度板件的任意功能梯度变化、各种复杂边界条件得到反映。用细观元法得到了几种具有不同复杂边界条件的功能梯度板件的力学量三维分布形态。 相似文献
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采用谱几何法建立了热环境下功能梯度环板自由振动分析模型。首先,在该模型中假设材料特性与温度相关,且沿结构厚度方向呈现连续梯度变化;其次,通过在边界处设置不同类型的边界弹簧来模拟任意边界条件,并且基于一阶剪切变形理论推导出热环境下功能梯度环板结构的能量方程;然后,利用谱几何法和傅里叶正余弦函数来描述结构位移容许函数,进而采用Rayleigh-Ritz法获得功能梯度环板结构热振特性分析理论模型。通过热环境下功能梯度环板频率特性对比算例发现,该模型具有良好的计算准确性,并且适用于多种边界条件。最后,给出功能梯度环板结构的参数化研究,研究结果表明,环境温度、边界条件、梯度指数的变化均会对结构的热振特性产生影响。 相似文献
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沿板平面变异功能梯度板件的三维动力特性 总被引:1,自引:0,他引:1
功能梯度材料具有复杂的细部结构,其内部构造远比匀质材料复杂,因此其构件动力分析很难求得其解析解。文中建议一种新颖的功能梯度构件动力分析的细观元法。细观力学研究的目的在于建立材料的宏观性能同其组分材料性能及细观结构之间的定量关系,它可揭示不同的材料组合具有不同的宏观性能的内在机制。目前功能梯度板件分析只能处理材料特性沿厚度方向梯度变化,而细观元法则直接从制备时给定的材料组分分布出发计算构件宏观三维动力特性,并给出了沿板平面方向材料特性梯度变化的功能梯度板件三维固有频率及振型的三维分布。 相似文献
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《振动与冲击》2016,(17)
假设矩形板为正交各向异性,材料的物性沿矩形板的宽度方向按幂律连续分布,基于二维线弹性理论,建立了四边弹性约束功能梯度材料(Functionally Graded Material,FGM)矩形板面内自由振动的控制偏微分方程。控制方程为复杂耦合的变系数偏微分方程,采用微分求积法(Differential Quadrature Method,DQM)数值研究了四边弹性约束FGM矩形板面内自由振动的无量纲频率特性。通过设置弹性刚度系数为0或∞,梯度指数为0,问题退化为各种典型边界下矩形板的面内自由振动,与已有的各向同性矩形板自振频率结果进行比较,结果表明分析求解方法行之有效。最后考虑了FGM矩形板边界条件、长宽比、梯度指数及刚度系数对自振频率的影响。 相似文献
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针对三维碳/碳复合材料板件开孔敏感性问题进行了试验与有限元分析。建立了三维碳/碳复合材料代表体积单元(RVE)和完好板件、开孔板件的有限元模型,给出了宏观应力到细观应力的转换方法,并基于此方法,实现了完好板件、开孔板件拉伸破坏过程的数值模拟。进行了三维碳/碳复合材料完好板件和开孔板件的单向拉伸试验,模拟计算结果与试验结果吻合良好。分析了不同宽径比(WTDR)对开孔板件拉伸强度的影响,其中当宽径比达到6时,开孔板拉伸极限强度相比完好板下降11.5%,可以认为如果宽径比不低于6,开孔对板件拉伸极限强度影响较小。该结论可以为碳/碳复合材料开孔板件设计提供指导。 相似文献
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针对任意边界条件下中心开口矩形板的自由振动特性研究问题,引入改进傅里叶级数方法,用改进傅里叶级数形式表示开口矩形板的位移容许函数,该级数形式具有收敛性好、精度高等特点,采用沿边界均匀分布的线性弹簧模拟任意边界条件,并结合位移连续条件和Rayleigh-Ritz能量泛函变分法,对未知傅里叶展开系数求极值将问题转化为求解一个标准特征值方程问题,通过求解方程可得到中心开口矩形板的固有频率及其对应振型;对不同边界组合不需重新推导公式,只需改变模拟弹簧刚度值即可,提高了效率,最后通过数值算例与有限元方法的计算结果进行对比分析以验证文中方法的有效性和精确性。 相似文献
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Based on Reddy's higher-order shear deformation plate theory, this article presents an analysis of the nonlinear dynamic response and vibration of imperfect functionally graded material (FGM) thick plates subjected to blast and thermal loads resting on elastic foundations. The 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. Numerical results for the dynamic response and vibration of the FGM plates with two cases of boundary conditions are obtained by the Galerkin method and fourth-order Runge–Kutta method. The results show the effects of geometrical parameters, material properties, imperfections, temperature increment, elastic foundations, and boundary conditions on the nonlinear dynamic response and vibration of FGM plates. 相似文献
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In this article, an analytical method for buckling analysis of thin functionally graded (FG) rectangular plates is presented.
It is assumed that the material properties of the plate vary through the thickness of the plate as a power function. Based
on the classical plate theory (Kirchhoff theory), the governing equations are obtained for functionally graded rectangular
plates using the principle of minimum total potential energy. The resulting equations are decoupled and solved for rectangular
plate with different loading conditions. It is assumed that the plate is simply supported along two opposite edges and has
arbitrary boundary conditions along the other edges. The critical buckling loads are presented for a rectangular plate with
different boundary conditions, various powers of FGM and some aspect ratios. 相似文献
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A Reissner's mixed variational theorem (RMVT)-based finite rectangular prism method (FRPM) is developed for the three-dimensional (3D) analysis of sandwich functionally graded material (FGM) plates subjected to mechanical loads, in which the edge conditions of the plates are such that one pair of opposite edges is simply supported and the other pair may be combinations of free, clamped or simply supported edges. The sandwich FGM plate considered consists of two thin and stiff homogeneous material face sheets combined with an embedded thick and soft FGM core, the material properties of which are assumed to obey the powerlaw distributions of the volume fractions of the constituents. In this formulation, the plate is divided into a number of finite rectangular prisms, in which the trigonometric functions and Lagrange polynomials are used to interpolate the y-direction and x-ζ plane variations of the primary field variables of each individual prism, respectively. Because an h-refinement process is adopted to yield the convergent solutions in this analysis, the prism-wise either linear or quadratic function distribution through the x-ζ plane is assumed for the related field variables. A unified formulation of these FRPMs with freely-chosen orders for assorted field variables is presented. It is shown that these quadratic FRPM solutions of simply supported, multilayered composite plates and sandwich FGM ones are in excellent agreement with the exact 3D solutions available in the literature, and those of multilayered composite plates with various boundary conditions closely agree with the solutions obtained using the ANSYS commercial software. 相似文献
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F. Aryana H. Bahai R. Mirzaeifar A. Yeilaghi 《International journal for numerical methods in engineering》2007,70(12):1409-1429
This paper proposes a method for calculating the required changes in the physical properties of plates made of functionally graded materials (FGM) in order to achieve the desired eigenfrequency shifts in the structure. A finite element formulation based on the classical laminated plate theory (CLPT) is presented for an FGM plate with integrated piezoelectric layers. Using this formulation, an efficient method based on the first‐order and second‐order approximations in Taylor expansion is expressed to calculate the corresponding changes in the plate modal properties due to changes in parameters which characterize the structure's dynamic behaviour. An initial sensitivity analysis is carried out to identify the regions within the structure where modifications are most effective on the structure's dynamic characteristics. The proposed algorithm is applied to a case study with two different boundary conditions and the results are validated against exact solutions. The influence of structural modifications on dynamic response of the plate is also studied using the Newmark‐β method. Copyright © 2006 John Wiley & Sons, Ltd. 相似文献
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Dynamic stability of laminated FGM plates based on higher-order shear deformation theory 总被引:2,自引:0,他引:2
This paper conducts a dynamic stability analysis of symmetrically laminated FGM rectangular plates with general out-of-plane supporting conditions, subjected to a uniaxial periodic in-plane load and undergoing uniform temperature change. Theoretical formulations are based on Reddys third-order shear deformation plate theory, and account for the temperature dependence of material properties. A semi-analytical Galerkin-differential quadrature approach is employed to convert the governing equations into a linear system of Mathieu–Hill equations from which the boundary points on the unstable regions are determined by Bolotins method. Free vibration and bifurcation buckling are also discussed as subset problems. Numerical results are presented in both dimensionless tabular and graphical forms for laminated plates with FGM layers made of silicon nitride and stainless steel. The influences of various parameters such as material composition, layer thickness ratio, temperature change, static load level, boundary constraints on the dynamic stability, buckling and vibration frequencies are examined in detail through parametric studies.This work was fully supported by grants from the Australian Research Council (A00104534) and from the Research Grants Council of the Hong Kong Special Administrative Region, China (Project No. CityU 1024/01 E). The authors are grateful for this financial support. 相似文献