基于压电曲壳单元的结构振动最优控制

曲壳结构已广泛应用于航空航天、航海等领域,结构微小的振动会极大地影响部件性能,抑制曲壳结构的振动就很必要。提出了压电曲壳结构的振动最优控制模型,利用空间曲壳单元理论及多点约束方程实现曲壳基结构壳元和压电壳元的耦合,推导了压电曲壳结构动力学有限元方程,并结合线性二次型最优控制理论,实现了压电作动器对曲壳结构的振动最优控制。数值算例表明,对曲壳结构进行动力分析和振动控制时,在达到同样精度及控制效果的情况下,与平壳相比,曲壳单元及作动器所需数目要少得多。     

考虑自平衡条件T形曲梁的静力学特性分析

为了准确分析T 形曲梁的静力学特性,该文考虑了剪滞翘曲应力自平衡条件、剪力滞后和剪切变形等因素的影响. 同时为了更好地反映T 形曲梁翼板的位移变化,4 个广义位移函数被引入,分析中以能量变分原理为基础建立了T 形曲梁静力学特性的控制微分方程和自然边界条件. 算例中,分析了剪滞翘曲应力自平衡条件、不同载荷形式和曲梁半径R 等因素对T 形曲梁静力学特性的影响,该文解析解与有限元数值解吻合更好,说明了该文方法的有效性.     

雷达回波资料反演海洋波导中观测值权重的确定

提出采用一种与电磁波传播损耗相类似的指数衰减形式来描绘观测值权重随距离的变化,结合标准的统计反演算法来测试不同的观测值权值对反演速度与精度的影响.结果表明,指数衰减形式能较好地描绘观测值权值随距离的变化情况;其中衰减指数的选取是关键.合理地选取衰减指数可较好地改进反演的速度与精度.对于不同频率的电磁波,最优衰减指数是各不相同的. 关键词： 海洋波导 观测值权重 衰减指数 反演算法     

爱因斯坦与物理观念的突破

介绍了爱因斯坦在某些重要的物理观念的突破中所作出的伟大贡献．这些重要观念涉及时空理论、量子论、宇宙学和规范理论．     

A novel electromagnetism‐assisted imprinting technology to replicate microstructures onto a large‐area curved surface using a flexible magnetic mold

Replication of microstructures from a mold onto a curved surface is difficult. The conformal contact between the mold and the substrate has to be ensured. The present study proposes an innovative mechanism, which employs an electromagnetic disk to provide magnetic force and a PDMS flexible mold with a layer compounded magnetic powder. This mechanism provides not only the gradual contact from center to edge to avoid air entrapment but also conformal contact between the mold and the substrate during the imprinting operation. A system based on this electromagnetic soft imprinting technology has been implemented, and imprinting to replicate microstructures from the mold onto a curved surface has been carried out. The results reveal that the PDMS magnetic mold and the electromagnetic disk‐controlled magnetic force can successfully perform the imprinting and accurately replicate the microstructures onto the large‐area, curved surface glass. The PDMS flexible magnetic mold incorporated with the magnetic disk can be employed to achieve the conformal contact between the mold and the substrate. In addition, due to the low surface free energy of the PDMS, the de‐molding without sticking can be easily accomplished. Copyright © 2008 John Wiley & Sons, Ltd.     

A semi-analytic solution for multiple curved cracks emanating from circular hole using singular integral equation

This paper provides an elastic solution for an infinite plate containing multiple curved edge cracks emanating from a circular hole. A fundamental solution is suggested, which represents a particular solution for a concentrated dislocation in an infinite plate with the traction free hole. The generalized image method and the concept of the modified complex potentials are used in the derivation of the fundamental solution. After using the fundamental solution and placing the distributed dislocations at the prospective sites of cracks, a singular integral equation is formulated. The singular integral equation is solved by using the curve length method in conjunction with the semi-opening quadrature rule. By taking an additional point dislocation at the hole center, the number of the unknowns is equal to the number of the resulting algebraic equations. This is a particular advantage of the suggested method. Finally, several numerical examples are given to illustrate the efficiency of the method presented. Numerical examinations are carried out and sufficient accurate results have been found.     

带通道插件管道流磁流体动力学效应的数值模拟

采用二维完全发展流模型对聚变反应堆包层带通道插件和压力平衡槽隙的矩形磁流体管流的MHD效应进行数值模拟,分析速度分布,MHD压降随哈德曼数以及通道插件的电导率的变化规律.与无插件磁流体管流相比,带绝缘通道插件管流MHD压降显著降低,MHD压降随哈德曼数的增加而减小,通道插件材料的电导率增加MHD压降系数减小.压力平衡槽隙处的回流与通道插件的电导率有关.在宏观上计算结果与实验结果和简化理论结果一致.     

柔性曲梁多体系统的研究现状和展望

本文对近几年来柔性多体系统建模理论的研究进展进行了评述, 详细阐述了曲梁结构多体系统动力学研究的理论背景和工程意义. 结合连续介质力学和多体系统动力学理论, 介绍了平面曲梁、空间曲梁应变位移场的描述以及几何非线性问题研究现状. 通过国内外文献及已有的研究, 综述了现有曲梁的离散化方法, 以及这些方法对于定曲率、变曲率曲梁的适用性. 然后, 总结了曲梁刚柔耦合动力学建模和数值计算中的难点问题, 介绍了平面曲梁、空间曲梁实验研究的现状. 最后, 综合全文, 提出了目前研究存在的难点问题, 以及计划解决这些难点问题的方法.      

密切曲面锥乘波体——-设计方法与性能分析

介绍了密切曲面锥(osculating curvedcone, OCC)乘波体的设计方法, 并对密切曲面锥乘波体的流场结构及气动特性进行了分析. 密切曲面锥方法采用具有直线激波和等熵压缩波系的曲面锥作为基准流场, 在定义乘波体激波型线(inlet capture curve, ICC)和前缘捕获型线(front capture tube, FCT)后, 采用密切轴对称和流线追踪技术, 设计生成密切曲面锥乘波体. 采用数值方法对设计的密切曲面锥乘波体进行了模拟, 理论设计结果和数值模拟结果一致. 对密切曲面锥乘波体和密切锥乘波体进行了比较, 密切曲面锥乘波体克服了密切锥乘波体压缩量不足及容积率偏小的缺点.