Static and free vibration analyses of functionally graded porous variable-thickness plates using an edge-based smoothed finite element method

The main purpose of this paper is to present numerical results of static bending and free vibration of functionally graded porous (FGP) variable-thickness plates by using an edge-based smoothed finite element method (ES-FEM) associate with the mixed interpolation of tensorial components technique for the three-node triangular element (MITC3), so-called ES-MITC3. This ES-MITC3 element is performed to eliminate the shear locking problem and to enhance the accuracy of the existing MITC3 element. In the ES-MITC3 element, the stiffness matrices are obtained by using the strain smoothing technique over the smoothing domains formed by two adjacent MITC3 triangular elements sharing an edge. Materials of the plate are FGP with a power-law index (k) and maximum porosity distributions (Ω) in the forms of cosine functions. The influences of some geometric parameters, material properties on static bending, and natural frequency of the FGP variable-thickness plates are examined in detail.     

Quasi-steady aerodynamic characteristics of Terminal Sensitive Bullets with short cylindrical portion

The aerodynamic characteristics are vital for short cylindrical Terminal Sensitive Bullets(TSB)with low aspect ratio,especially in terminal trajectory.Currently,there is little research in terms of the TSB and short cylinder with two free ends,and particularly in this trajectory,where the scanning angle β and roll angle α vary over a broad range between 0° and 180°.In this work,wind tunnel experiments are first conducted to learn the effects of Reynolds number and scanning angle on aerodynamic parameters for short cylinder with aspect ratio L/D = 1.Similar to infinite cylinder,for the short cylinder with two free ends,the drag crisis phenomenon still exists in the critical regime 1.7 × 105 ≤ Re ≤ 6.8 × 105.Then 3D simulations are performed to demonstrate the aerodynamic characteristics of short cylinder and TSB over a broad range of Re,L/D,α and β.The sensitivity analysis of time step and grid are presented as well.When β=0°,for short cylinder,the drag crisis phenomenon was also observed in the simulation,but not as obvious as in the wind tunnel test.In some attitudes,there is an obvious Kármán vortex in the wake of short cylinder and TSB.The correlation between time-averaged aerodynamic coefficients and L/D,Re,α&β is discussed.The vortex shedding frequency and shear layer behavior are obtained for quasi-steady and unsteady flow.Finally,the effect of end's shape on drag reduction and vortex shedding frequency is analyzed.     

水下声探测系统载体振动干扰分析及抑制方法

针对水下探测系统载体振动对目标回波信号的微多普勒特征谱产生干扰的问题,从干扰产生的基本原理出发,推导了干扰的近似乘性表达式。在获取振动干扰数据的条件下,提出了针对乘性干扰的干扰抑制算法,并针对推导干扰乘性表达式时的近似条件,分析了近似算法带来的误差。仿真结果表明,该方法可有效抑制水下探测系统平台振动对目标回波信号的微多普勒特征谱产生的干扰,并且在绝大多数情况下,由算法带来的误差可以忽略不计。     

舰船管路橡胶减振器的应用

简要分析了管路橡胶减振器对刚性管路的隔振原理,提出了几种通过改变管路布置形式而达到对管路各自由度上减振的方法,阐述了在实际应用中如何调整橡胶隔振器的固有频率而达到对舰船管路良好的隔振.     

小波理论在大型空间智能结构振动控制中的应用

采用最优控制理论设计智能结构主动振动控制器,针对大型空间智能结构的低频和密频的特性,基于小波尺度函数变换,设计了智能结构的传感器、致动器;最后通过针对某大型空间智能桁架结构的仿真,表明该控制方法是行之有效的。     

强迫振动法大跨度桥梁节段模型气动导数辨识

研制了桥梁节段模型颤振导数测定的二维强迫振动实验装置,采用变频调速技术实现对振动频率的控制,模型惯性力、气动力的测量采用了特殊设计的测力元件,模型运动用压电式加速度计进行测量。实验时,模型分别作单自由度的竖弯或扭转的简谐运动,通过测量模型所受到的气动力及模型位移,应用谱分析方法和非线性曲线拟合算法实现了对八个颤振气动导数的辨识,并通过平板模型实验数据与Theodorsen理想平板数据及国外文献数据对比对实验装置及辨识算法进行了检验。     

潜艇纵向振动计算及振动特性

采用有限元方法建立了潜艇纵向振动分析有限元模型,求出了某艇在水面巡航状态的纵向振动模态.发现潜艇耐压壳纵向振动除具有典型的“活塞”式振动特征外,还具有众多与“一维梁”纵向振动不同的特性.     

利用振动信号诊断发动机气门间隙异常故障

提出了利用气缸盖表面振动信号诊断发动机配气机构气门间隙异常故障的方法,分析了气缸盖表面振动响应与气门机构状态的关系。通过实验和计算,从气缸盖表面的振动信号得到气门间隙异常状态的信息。在此基础上,提出了一种简单有效的时域分析诊断方法。     

舰船尾部振动的水弹性模型

采用三维水弹性理论导出了舰船尾部振动的流固耦合运动方程式;用三维结构混合有限元和三维流体边界元建立了舰船尾部振动的水弹性分析离散模型．提出了中型水面舰艇尾部整体振动的预报方法;编制了相应的计算机程序．对两型舰艇的尾部振动进行了分析计算,结果表明,预报值与实测值比较吻合．研究结果可对中型水面舰艇的减振降噪设计提供预报手段,从而改善舰船的尾部振动环境．     

基于神经网络和模糊综合评判的梁故障诊断研究

设计了一个简单的人工智能故障诊断系统模型,它包括知识库、模糊推理、神经网络和控制模块等。模糊推理模块利用模糊综合评判方法进行故障的预诊,神经网络模块采用竞争学习方法完成故障的确诊。文中对悬臂梁的单一故障和复合故障等七种模式进行了诊断分析,均获得了正确的诊断结果。