有关超载车辆危害公路桥梁的浅析与思考

总结了超载车辆对各种公路桥梁的危害种类及其原因,并提出一些建议以供思考应用。     

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概要介绍了中国公路水路运输的基本能力和面临的主要挑战.分析了在未来中国国民经济持续快速增长，工业化、城市化进程加速形势下交通需求的主要特征，强调了要在科学发展观指导下加强对交通服务新理念的认识.针对建立综合运输体系问题，文章强调除了依托工程实践和科技创新增强系统整合与街接外，协调的体制、高效的机制更为重要.借鉴发达国家交通发展战略调整的经验，本文还提出了中国公路水路交通发展的战略目标以及重点行动.     

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对面向ATMS共用信息平台的数据预处理技术进行了探讨.介绍了面向ATMS的共用信息平台的含义以及作用，探讨了面向ATMS共用信息平台的数据预处理技术，从故障识别，故障修复来对动态交通数据预处理方法进行了研究.该研究对于面向ATMS共用信息平台数据预处理提供了依据.     

沉箱孤立墩式结构整体稳定性一般规律

大型原油码头多采用墩式蝶型布置,一般情况下波浪作用是控制沉箱墩式结构整体稳定性的主要外荷载。作为设计波要素,通常选取最大波高及其对应的波周期或最大波周期及其对应的波高进行结构计算,但经多组波要素对比计算表明,并非最大波高或最大波周期为控制工况。参考数模分析群桩系数随波周期变化的成果,研究了作用于小尺度墩柱上的波浪作用随波周期和波高的变化以及沉箱孤立墩式结构整体稳定性的一般规律。     

自主水下航行器发展概述

自主水下航行器（AUVs）因其应用于海洋勘探而逐渐成为一个有趣的研究对象。波浪滑翔机是一种行驶于波浪表面的无人滑行器（SUV）,它借助海洋能来推动自己,这对于典型的AUVs所采用的电机供能以及昂贵的锚链系统浮标供
　　能来说,是一种技术上的重大跨越。该文讨论了最有效率的AUVs类型。第一部分为每一种类型的发展历程,第二部分为它们各自的技术特点。此外,波浪滑翔机作为应用于海洋部门的一种新型水下机器人,文中简要地给出它的过去,现在以及未来的发展概述。研究波浪滑翔机的意义在于证明它的效率以及实用性,进而取代诸多的AUVs来实现各种实际应用。而研究结果也表明波浪滑翔机确实可以应用于众多领域。对于海洋检测而言,相比于其他AUVs,波浪滑翔机提供了更廉价,更经济,更环保的作业模式,同时也不需要缆绳、船舶等海上作业服务。     

自主水下机器人下潜困难问题的数值仿真与试验研究

自主水下机器人在近水面运动时,受到文丘里效应产生向上吸力的影响,使得潜器初始下潜困难,近水面的深度保持能力也受到影响。为了研究水下潜器近水面下潜困难问题,文章运用计算流体力学（CFD）软件对某AUV主体周围流场进行近水面数值模拟。模拟结果表明,影响升力和抬头力矩的主要因素是初始的下潜深度和速度。水域试验表明随着初始下潜深度的增加,AUV 的下潜将变得越来越容易,这与模拟结果相一致。     

水下航行体降噪艉翼填角的数值模拟与试验研究

为降低水下航行体噪声,研究了艉翼填角的降噪效果。分析了水下航行体艉翼接合部马蹄涡影响螺旋桨伴流场的特征,认为马蹄涡对水下航行体噪声产生了不利影响。针对某无人水下航行体(UUV)设计了一种艉翼填角,运用CFD方法对该艉翼填角优化螺旋桨伴流场的效果进行了数值模拟,结果显示伴流场轴向速度的周向不均匀度系数下降35%-62%。将艉翼填角应用于该UUV,开展航行辐射噪声测量试验,结果显示艉翼填角使UUV航行噪声总声源级降低3.4 d B,尤其对低频噪声抑制较好。     

Differences in single heavy vehicle crashes at intersections and midblocks

The objective of this research is to identify the factors differentiating between single heavy vehicle collisions at intersections and midblocks by using a binary logit model. Our results show that single vehicle crashes involving heavy vehicle at intersections are more likely to occur on main roads and highways, whereas crashes at midblocks are more likely to occur on divided two‐way roads, roads with special facilities or features (e.g. bridge) and roads with a higher percentage of heavy vehicle traffic. Intersection crashes are also more likely to involve vehicles that are turning left or right, resulting in angle crashes and vehicle overturn, whereas midblock crashes are more likely to involve vehicles on higher posted speed roads. Copyright © 2017 John Wiley & Sons, Ltd.     

Vehicle rollover avoidance by application of gain-scheduled LQR controllers using state observers

Many researches have been conducted in the area of control applied to vehicle dynamics, aiming at reducing the possibility of the occurrence of the type of accident known as rollover. In this research, based on a common nonlinear model and its linearisation, a method for properly selecting matrices for solving the Riccati equation considering different speeds was proposed. The method showed in which ways speed really influences the choice of controller gains. By developing the dynamic equations for the yaw- and roll-coupled motions and modelling of controllers and state observers, it is possible to compare the efficacy of this control strategy using both linear and nonlinear simulations using Matlab. Significant results were obtained regarding the reduction of the rollover coefficient for a double-lane change manoeuvre at different speeds, thus indicating advantages of using this controller in practical cases.     

Quasi steady-state aerodynamic model development for race vehicle simulations

Presented in this paper is a procedure to develop a high fidelity quasi steady-state aerodynamic model for use in race car vehicle dynamic simulations. Developed to fit quasi steady-state wind tunnel data, the aerodynamic model is regressed against three independent variables: front ground clearance, rear ride height, and yaw angle. An initial dual range model is presented and then further refined to reduce the model complexity while maintaining a high level of predictive accuracy. The model complexity reduction decreases the required amount of wind tunnel data thereby reducing wind tunnel testing time and cost. The quasi steady-state aerodynamic model for the pitch moment degree of freedom is systematically developed in this paper. This same procedure can be extended to the other five aerodynamic degrees of freedom to develop a complete six degree of freedom quasi steady-state aerodynamic model for any vehicle.