排水型方尾船加装尾板前后振动性能分析

采用大型通用有限元分析软件和流体边界元方法,对某排水型方尾船加装尾板前后的总体振动特性和尾部振动响应进行了分析计算和比较,得出了加装尾板对该型船总体振动特性和尾部振动响应影响很小的结论.     

一种金属橡胶元件建模方法研究

用理论和试验相结合的手段研究金属橡胶弹性元件的动力学建模,提出一种新的建模方法,用此方法建立了基于迟滞回线拟和分解的高次弹性复合阻尼模型。该模型用非线性刚度和非线性复合阻尼机理构造,模型中的参数由试验数据辨识。用所建模型重构恢复力-位移迟滞回线,结果表明该模型能很好描述这类非线性振动系统的特性。     

稀土永磁减振器特性的数值模拟分析

简要介绍了目前稀土永磁减振器的研究现状和单质量稀土永磁减振器的结构与工作原理,运用大型有限元软件ANSYS对稀土永磁减振器的工作过程进行数值模拟,分析其在工作过程中的磁通密度、磁力线分布、力学特性以及它们之间的相互关系。研究表明:稀土永磁减振器具有较好的非线性减振效果;ANSYS在模拟稀土永磁减振器工作过程时,能形象直观的反映其在工作过程中的各种特性参数。     

基于缸盖振动的燃油喷射系统故障诊断

对V型12缸柴油机缸盖振动燃烧段信号与缸内压力进行了时域对比,分析了失火时的缸盖振动响应,研究了供油规律随转速变化情况。分析表明缸盖振动中包含喷油器针阀落座的振动响应,研究了基于短时能量动态双阈值端点检测提取针阀落座响应时间特征的方法,利用振动信号的峰值加速度来表征针阀落座的强度。在不同工况及不同状态下提取了针阀落座时间及强度的振动特征,结果表明：振动特征能够有效反映针阀的工作情况,可以用于燃油喷射系统故障的诊断。     

残余应力作用下脆性膜/基材料的断裂行为

假定膜内的残余拉应力足以使膜发生开裂,利用膜/基材料中含弹性界面层的剪滞模型,研究了脆性膜/基材料在残余应力作用下的开裂行为特征,探讨了膜内正应力、膜/基界面切应力的分布规律,获得了膜的裂纹密度与残余应力大小之间的解析表达式。在裂纹密度、材料的力学和几何参数确定的情况下,该解析表达式可以用来评估残余应力的大小。最后,分析了膜的裂纹密度与残余应力、膜的厚度、弹性模量、断裂强度以及界面层的切变模量之间的内在关联,绘出了这些参数影响膜裂纹密度的变化曲线。     

基于振动分析的坦克柴油机汽缸燃烧压力检测方法

针对在坦克实车上不易直接测量柴油机汽缸压力的问题,提出了一种通过测量柴油机汽缸盖振动信号来间接检测汽缸燃烧压力的方法。在某型坦克柴油机上同步测量了汽缸燃烧压力、汽缸盖振动信号和变速箱振动信号,利用自适应滤波方法滤除了汽缸盖振动信号中包含的变速箱振动信号形成的噪声干扰,利用配气相位从时间域分离出由气体燃烧压力激发的振动信号,利用Hilbert变换和小波分解方法分别提取了振动信号和压力信号的特征波形。建立了RBF神经网络模型,以汽缸盖振动信号的包络作为网络输入,实现了汽缸燃烧压力的间接检测。     

关联维数在梁式结构损伤检测中的应用

为探索有效实用的结构损伤检测方法,运用分形理论直接对结构振动信号进行关联维数分析,通过度量系统输出的奇异性来识别结构的局部损伤,提出了基于振动响应关联维数的结构损伤检测方法.简支梁损伤算例结果表明,该方法能够准确地检测出梁式结构单个和多个不同程度的损伤位置,同时关联维数指标变化值会随着损伤程度的增加而增大.与曲率模态指...     

Noise and vibration measurements in a Viking military vehicle

Noise and whole-body vibration measurements were made in a Viking military vehicle to determine the variation that should be expected during repeat measures, the effect of speed (up to 60 km/h in 5 km/h increments), and during travel over different types of terrain (comprising concrete road, gravel track and rough cross-country). Measurements were made at various crew positions (including the driver and commander) in both the front and the rear cabs in the vehicles. Three translational axes of vibration were measured in each seat. Two speeds were investigated over road (35 km/h and 55–60 km/h) and gravel (20 km/h and 35 km/h) surfaces. The effect of varying speed of the vehicle on the measured noise and vibration magnitudes was also investigated. The highest sound pressure level (L_Aeq) of 104 dB(A) was measured at the commander’s standing position during travel over concrete road at 55 km/h. Higher noise levels occurred for a standing commander compared with when sitting on the seat. A maximum single axis frequency-weighted vibration magnitude of 1.0 m/s² r.m.s. was measured on the driver’s seat during travel over track at 35 km/h. Higher vibration magnitudes occurred during travel over track compared with travel over road. Both noise and vibration exposure of crew within the Viking vehicle increased with increasing speed of the vehicle.     

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.