新型避振穴研究

本文提出了一处新型避振穴。由于摒弃了橡胶弹性元件，该避振穴的结构简单，施工与维护方便。还介绍了模型试验结果，阐述了减振原理与应用前景。     

汽车接近角,离去角和纵向通过角的测量

介绍了日本汽车标准化协会（JASO）对汽车接近角、离去角和纵向通过角的定义。按照该定义，可以用简单的测量工具测得若干个长度尺寸，然后代入按几何关系推导出的公式中求得上述三个角度的精确值，既提高了测量精度，又便于各车型之间这些参数的比较。     

城市单轨交通系统

介绍了单轨交通特别是日本单轨交通的发展情况，分析了单轨交通跨座型车辆和悬挂型车辆的特点；最后，阐述了重庆市的城市轨道交通规划，举出了单轨交通跨座型车辆的一些主要参数。     

集装箱船弯扭耦合振动分析

本文基于薄壁结构力学基本理论，提出了一种适合于大开口集装箱船弯扭耦合振动分析的薄壁梁有限元模型。该模型考虑了翘曲、剪切及剖面转动的影响，以及货舱大开口和抗扭箱（甲板梁）引起的结构不连续性。其例中，计算结果与三维有限元分析结果、模型试验结果相当吻合，而薄壁梁有限元的计算效率要高得多，算例还表明抗扭箱（甲板梁）对提高集装箱船的抗扭刚度有十分重要的意义。     

水下航行体通气超空泡的实验研究

为了研究超空泡的减阻效果,保证在较低流速下生成超空泡,在水洞中开展了水下航行体通气超空泡的实验研究.采用通气的方法在较低水速下(V=7-15 m/s)生成人工通气超空泡,通过改变通气率和弗洛德数,获得了不同条件下通气空泡的长度,给出了通气空泡长度与通气率及弗洛德数的经验公式.研究表明,来流速度不变时,空泡长度随通气率的增加而增加,空泡长度一定时,通气率随弗洛德数的增加而减少;重力场造成了空泡形态的严重不对称,通过比较相同空化数下自然空泡与通气空泡的长度,定量地给出了弗洛德数对通气空泡长度的影响.当Fr=43.74时,重力场对通气空泡长度的影响几乎可以忽略.     

船尾桨前垂向整流鳍的减振机理研究及其应用

文章认为在船尾型线设计中若不考虑横剖线的UV度、各水线去流角大小等对船体振动的不利影响,很可能会导致艉部水流异常;螺旋桨盘面处非定常及分布不均匀的艉流将直接导致船体剧烈振动.针对发生了该类有害振动的船舶,介绍一种安装于船尾的垂向整流鳍.通过引用水动力不平衡导致螺旋桨激振力产生的基本原理,探讨垂向整流鳍整流使螺旋桨盘面处原艉流场发生有利改变的实质,揭示船尾桨前垂向整流鳍的减振机理.以实例说明该整流鳍在消除该类振动方面的突出效果.     

Three-dimensional vortex-induced vibrations of a circular cylinder predicted using a wake oscillator model

This paper reports a numerical study based on a wake oscillator model, to determine the three-dimensional vortex-induced vibration (VIV) responses on a flexible cylinder with pinned-pinned boundary conditions subjected to a uniform flow. Four different aspect ratios have been selected for the study. The coupling equations of the structural oscillator models and wake oscillator models in both the cross-flow (CF) and in-line (IL) directions have been solved using a standard central difference method of the second order. The structural displacement, structural frequency, response wave pattern, response trajectory, and lift force coefficient, for four aspect ratios, have been compared. The numerical results establish that, for a small aspect ratio, the CF displacements have absolute standing wave behaviors without travelling wave behaviors, and the IL displacements have dominant standing wave behaviors with slight travelling wave behaviors. Further, the VIV trajectory is repeatable and displays figure-eight shapes. However, for a large aspect ratio, the CF displacements display identical characteristics with the IL displacements for a small aspect ratio, and the IL displacements for a large aspect ratio are simultaneously dominated by standing and travelling wave behaviors. Moreover, the VIV trajectory is apparently aperiodic and shows chaotic shapes.     

Experimental investigation on vortex-induced force of a Steel Catenary Riser under in-plane vessel motion

A method to identify vortex-induced forces and coefficients from measured strains of a Steel Catenary Riser (SCR) undergoing vessel motion-induced Vortex-induced Vibration (VIV) is proposed. Euler–Bernoulli beam vibration equations with time-varying tension is adopted to describe the out-of-plane VIV responses. Vortex-induced forces are reconstructed via inverse analysis method, and the Forgetting Factor Least Squares (FF-LS) method is employed to identify time-varying vortex-induced force coefficients, including excitation coefficients and added mass coefficients. The method is verified via a finite element analysis procedure in commercial software Orcaflex. The time-varying excitation coefficients and added mass coefficients of an SCR undergoing vessel motion-induced VIV are investigated. Results show that vessel motion-induced VIV is excited at the middle or lower part of the SCR and in the acceleration period of in-plane velocity, where most of the excitation coefficients are positive, while during the deceleration period, the excitation coefficients becomes too small to excite VIVs. Parameter γ [1] has strong correlation with excitation coefficients. In addition, time-varying tensions contribute significantly to the variations of added mass coefficients under the condition that the ratio of dynamic top tension to pretension exceeds the range of 0.7–1.3. Moreover, chaotic behaviors are observed in vortex-induced force coefficients and are more evident with the increase of vessel motion velocity. This behavior may attribute to the randomness existing in in-plane velocity and its coupling with out-of-plane vibrations.     

三体船粘压阻力预报方法

三体船快速性的研究是三体船新船型开发技术的支撑。通过模型试验与数值模拟相结合的方法,对不同航速下三体船的粘压阻力进行计算。试验研究采用将三体船侧体分别放置在船中、船前部和船后部3个不同的纵向位置以及距船中心线3个距离不同的横向位置,测量9个侧体位置下三体船在静水中的总阻力。运用第八届ITTC公式计算摩擦阻力系数,进而算出剩余阻力系数。通过数值模拟的方法,基于细长体理论对三体船兴波阻力系数进行计算,再根据三因次换算方法计算粘压阻力系数。得出不同构型下三体船在静水中的粘压阻力系数,并作出其随Fr数变化的曲线,观察在侧体位置不同的情况下,三体船的粘压阻力系数随航速变化的规律。根据所得粘压阻力系数曲线,提出初步预报三体船粘压阻力系数的一种简单方法。     

板式无砟轨道交通引起的环境振动数值分析

利用已研究出的高速铁路动荷载,采用粘弹性边界,运用有限元法建立轨道-路基-大地二维动力分析模型,分析板式无砟轨道交通引起的振动在大地中的传播特性。计算分析表明:地表的振动强度随着离轨道中心线的距离增加而逐渐衰减。离轨道中心线近处,地表振动较强,而且加速度主要频段在20 Hz以上;离轨道中心线较远处,振动较小,加速度主要频段在10 Hz以下。随着离轨道中心距离的增加,加速度幅值随之减小,而且地表20 Hz以上的振动衰减得较快,10 Hz以下的振动衰减得较慢。