Slamming and Green Water Loads on Bow-Flare Ship in Regular Head Waves Investigated by Hydroelasticity Theory and Experiment

With the development of ships towards large scale, high speed and light weight, ship hydroelastic responses and slamming strength issues are becoming increasingly important. In this paper, a time-domain nonlinear hydroelasticity theory is developed to predict ship motion and load responses in harsh regular waves.Hydrostatic restoring force, wave excitation force and radiation force are calculated on the instantaneously wetted body surface to consider the nonlinear effects caused by large amplitude motions of ship in steep waves. A twodimensional(2 D) generalized Wagner model and a one-dimensional(1 D) dam-breaking model are used to estimate the impact loads caused by bow flare slamming and green water on deck, respectively; the impact loads are coupled with the hydroelastic equation in time-domain. Moreover, segmented model tests are carried out in a towing tank to investigate the wave and slamming loads acting on the hull sailing in harsh regular head waves and also validate the numerical results.     

基于Hyperworks的半挂车车架结构分析与改进

<正>在设计车架过程中,车架材料主要应用QH70钢或16Mn低碳钢等,全铝制车架出现得非常少,在满足车架的强度刚度的情况下,铝制车架相比钢制车架能够减轻     

军用UUV的发展与应用前景展望

UUV作为一种独具特色的水下作战力量,正在成为一种新的作战平台,受到各国海军的关注。文章在详细论述了uUV发展现状及其使命任务的情况下,结合潜艇武器系统的特点就军用UUV的组成、布放与回收、作战使用模式以及需要解决的关键技术进行了详细的论述,并展望了其未来发展前景。     

飞机巡航阶段尾涡遭遇安全性多参数评估方法

分析了飞机遭遇尾涡后的响应机理，综合考虑飞机滚转阻尼特性及操纵品质等因素，建立了飞机滚转角加速度计算模型；因飞机遭遇尾涡后飞行轨迹及飞行姿态发生改变，选择了多个扰动参数评估尾涡遭遇安全性，建立了飞机动力学参数计算模型；为确定尾涡遭遇可接受安全水平，基于国内现行尾流间隔标准，统计了中低空典型机型组合的尾流遭遇受扰参数计算数据；分析了高空尾涡流场演化特性，计算了高空巡航状态下的尾流安全间隔，分析了不同因素对飞行安全的影响。研究结果表明:与中低空相比，高空尾涡流场的初始强度大，持续距离长，飞行高度超过9 000 m后，尾涡消散随高度的增大而加快；当前机为超级重型机、重型机，现行尾流间隔无法保证飞行安全，需增加安全间隔1.4~2.1 km，飞行高度分别超过13 800、14 400 m后，尾涡遭遇严重度降低；当前机为一般重型机时，尾流安全间隔可缩减1.5 km以提高空域利用效率；当前机为中型机时，尾涡遭遇安全性较高，但此时受最小雷达间隔限制，无法进一步缩减前后机间距；后机的飞行速度越低，发生尾涡遭遇的严重程度越高；在后机初始滚转坡度角由0增加到10°的过程中，尾涡安全间隔增加1.3 km，增加幅度约为8.61%。可见，采用多个受扰参数能有效评估高空尾涡遭遇严重程度。