轮胎在沙地上牵引特性的新预测模型

本文分析了汽车在松软地面上行驶时轮台的受力状态及轮胎单元与土壤的相互作用方式，揭示了轮胎在松软地面上牵引特性传充预测模型的不足之处，建立了轮胎在沙地上牵引特性的新预测模型，并进行了实验验证。结果表明，采用本文所建立的模型进行预测时，预测值与实测值更接近。     

考虑胎体复杂变形的轮胎非稳态侧偏特性理论模型

本文从肥体的一般变形模式出发，根据胎体的侧向弯曲变形及扭转变形计算出胎面的侧向瞬时变形，从而建立了小幅运动时轮胎非稳态侧偏特性理论模型。考虑胎体的复杂变形之后，模型能真实地反映轮台力学特性和物理实质。     

双质量飞轮式扭振减振器

现代汽车广泛采用的是离合器从动盘式扭振减器，而双质量飞轮式扭振器则是近年来发展起来的一种更为有效的新型扭振减振器。本比较了了双质量飞轮式扭振减器和离合器从动盘式扭振减器的结构、性能及优缺点。     

货车驾驶室结构动力模型修改

本文利用货车驾驶室的测试模态参数来修正其有限元动力分析模型。文中主要论述货车驾驶室模态参数识别、动力分析模型单元组合修正法和货车驾驶室动力模型修改。     

高阶CMAC神经网络及其在水下机器人运动控制中的应用

对高阶ＣＭＡＣ神经网络的结构和工作原理进行了研究,提出了中间层作用函数地址的计算方法,给出了计算高阶基函数的不同方法,利用高阶ＭＣＡＣ神经网络对水下机器人模糊深度控制器进行了学习,仿真结果显示了不同高阶基函数ＭＣＡＣ网络的不同建模能力,证明了中间层作用函数地址的计算方法正确。     

轻量化实景三维模型质量评定方法

以基于实景三维模型的BIM设计为导向,按照土建工程设计各阶段的不同需求,兼顾模型几何精度和纹理质量,提出轻量化实景三维模型数据质量评定方法。解决了轻量化后的实景三维模型数据质量控制的难题,为其广泛应用到BIM设计中打下坚实基础。改变了传统测绘数据成果的交付形式,从勘察测绘环节促使设计人员使用BIM技术,进而加快BIM技术的普及和应用,加强BIM技术应用的深度和广度,最终实现BIM技术在建筑行业全生命周期过程中的普及和推广。     

利用物理模型研究热扩散问题

山东威海华能电厂循环冷却水正态物理模型试验的目的是研究电厂设备冷却水排入海中后对海域及取水口的热污染问题,本文剖析了试验过程,内容包括电厂附近海域的自然条件分析、热扩散理论在模型中的应用、模型设计思想、试验设备量测系统与试验方法以及模型试验中需要探讨的问题。     

Transient responses of a VLFS during landing and take-off of an airplane

The transient elastic deformation of a pontoon-type very large floating structure (VLFS) caused by the landing and take-off of an airplane is computed by the time-domain mode-expansion method. The memory effects in hydrodynamic forces are taken into account, and great care is paid to numerical accuracy in evaluating all the coefficients appearing in the simultaneous differential equations for the elastic motion of a VLFS. The time-histories of the imparted force and the position and velocity of an airplane during landing and take-off are modeled with data from a Boeing 747-400 jumbo jet. Simulation results are shown of 3-D structural waves on a VLFS and the associated unsteady drag force on an airplane, which is of engineering importance, particularly during take-off. The results for landing show that the airplane moves faster than the structural waves generated in the early stage, and the waves overtake the airplane as its speed decreases to zero. The results for take-off are essentially the same as those for landing, except that the structural waves develop slowly in the early stage, and no obstacle exists on the runway after the take-off of airplane. The additional drag force on an airplane due to the elastic responses of the runway considered in this work was found to be small in magnitude.     

A pseudofield model approach to simulate compartment-fire phenomena for marine fire safety design

In order to prevent the spread of marine compartment fires, it is necessary to understand the governing factors or characteristics of fire-spread phenomena. We present a pseudofield model approach to this problem. We first described a field model of turbulent heat convection based on a standard k – turbulence model. Two-dimensional numerical simulations of a two-linked compartment fire were carried out in order to predict the turbulent convection flow induced by the heat released from the fire. Then a more complicated fire-spread problem of multilinked compartment fires was analyzed by means of a zone model, in which the amounts of oxygen consumption and gas generation were solved by a gas-balance equations system. The effect of threshold conditions on fire propagation and the effect of the thickness of the heat insulation were investigated with numerical simulations.