检索规则说明:AND代表“并且”;OR代表“或者”;NOT代表“不包含”;(注意必须大写,运算符两边需空一格)
检 索 范 例 :范例一: (K=图书馆学 OR K=情报学) AND A=范并思 范例二:J=计算机应用与软件 AND (U=C++ OR U=Basic) NOT M=Visual
作 者:张羽飞[1] 杜敬涛[1] 杨铁军[1] 朱明刚[1] 刘志刚[1]
机构地区:[1]哈尔滨工程大学动力与能源工程学院,黑龙江哈尔滨150001
出 处:《哈尔滨工程大学学报》2015年第11期1448-1453,1531,共7页Journal of Harbin Engineering University
基 金:国家自然科学基金资助项目(11202056);中央高校基本科研业务费专项资金资助项目(HEUCF120301)
摘 要:目前板结构振动特性的计算分析大多数都是基于经典板理论或者其他高阶近似理论,为了深入理解其振动特性,对于一些厚度比较大的板,采用三维弹性理论来进行分析十分必要。在空间坐标系中沿3个坐标轴方向的位移场使用三维改进傅里叶级数法来建模,通过计算系统拉格朗日函数的极值即可计算出描述位移场的所有未知系数。将本文计算结果与文献结果和NASTRAN软件计算的有限元结果进行比较,最大偏差不超过1.4%,结果吻合良好。结果表明:本文方法能够准确预测三维弹性矩形厚板结构的振动特性,且无论矩形板的边界条件是否对称,都能使用该方法来简便地获得固有频率、振型以及强迫响应。Most current studies of vibration characteristics of plate structures are based on the classical plate theory or other high-order approximation theories. In order to get a deep understanding of thick plate vibration characteris- tics, it is of critical importance to analyze the vibrations using the three-dimensional elasticity theory. In this paper, a three-dimensional improved Fourier series method is first proposed to construct three vibrating displacement fields in a thick rectangular plate with various boundary conditions. All the unknown coefficients were then determined from the extrema of system Lagrangian constructed completely from 3-D elasticity theory. Finally, numerical exam- ples were given to validate the current method through comparison with results from other approachs, and finite ele- ment analysis (FEA) using NASTRAN. Good agreement was observed between the two sets of solutions, the largest deviation was less than 1.4%. The results show that the proposed method is able to accurately capture the vibration characteristics for 3-D rectangular plate structures. Natural frequencies, mode shapes, and forced response of thick plates can be easily obtained whether the boundary condition is symmetrical or not.
关 键 词:三维弹性理论 矩形厚板 任意边界条件 改进傅里叶级数法
分 类 号:O327[理学—一般力学与力学基础]
正在载入数据...
正在载入数据...
正在载入数据...
正在载入数据...
正在载入数据...
正在载入数据...
正在载入数据...
正在链接到云南高校图书馆文献保障联盟下载...
云南高校图书馆联盟文献共享服务平台 版权所有©
您的IP:13.59.149.79