海上单桩风力发电平台简化设计

采用在欧洲已经进行商业化运作的独立桩双段结构，桩基础采用带有过渡段的单桩。塔架上的风力发电机采用丹麦Vestas公司的V80风力发电机。参考DNV-OS-J101和API-RP-2A中的工作应力设计法，进行结构静力、桩基础的承载力，涡激振动、疲劳寿命，结构动力学等分析。静力分析分析极端环境下的组合工况；桩基础主要计算桩的轴向承载力和校核水平承载力，并采用有限元模型模拟桩土相互作用；涡激振动分析主要考虑不同风速下塔架的升力以及引起的横向振动；疲劳分析根据涡激振动分析的结果利用S-N曲线对基础寿命进行了评估；动力学分析求出了结构的固有频率，并进行了波浪力作用下的瞬态历程分析。     

电信计费模型的设计

依据电信计费系统存在的问题,本文详细描述了电信计费模型的设计方法和各个模块的设计内容。     

滑床板摩擦力对尖轨不足位移的影响

为解决道岔尖轨不足位移问题,根据尖轨的特殊结构外形、受力特性和扳动机理,建立尖轨不足位移计算仿真模型,分析不同滑床板表面摩擦系数取值下尖轨不足位移的变化。结果表明:摩擦力是导致尖轨产生不足位移的主要原因;尖轨不足位移随滑床板摩擦系数的增加而增大,基本成线性递增关系;最后牵引点距尖轨跟端间间距越大,摩擦系数对不足位移的影响也越大。减小摩擦力和优化牵引点间距能够较好地控制尖轨不足位移。提出设置滚轮式滑床板方案,将轨底与滑床板间的滑动摩擦转化为滚动摩擦,并优化滚轮式滑床板布置方式,进一步减小了尖轨不足位移。     

时延网络控制系统的保性能控制研究

针对网络控制系统中存在的不确定时延，在传感器采用时间驱动，执行器与控制器采用事件驱动、时延小于一个采样周期的条件下，将网络控制系统建模为一类具有不确定性的线性离散系统并且其标称模型可控。围绕该标称模型，利用Lyapunov方法，基于相应的LMI可行解，给出网络控制系统保性能控制律的设计方法。通过仿真证明了该方法的有效性。     

高强钢筋混凝土非线性力学模型研究

针对高强钢筋混凝土非线性分析，对非线性分析中裂缝的模拟、钢筋混凝土材料本构关系及其非线性问题求解方法的改进进行研究，提出了适用于高强混凝土的本构曲线，并将混合法用于非线性问题，为高强钢筋混凝土梁非线性分析提供了理论基础。     

支持协同设计的船舶设计过程模型研究

船舶设计过程模型是在网络环境下开展船舶并行和协同设计系统的基础.本文根据船舶设计的特点,提出了将船舶设计过程按照项目、设计任务和设计活动三个层次进行分解的方法,并给出了船舶设计过程模型形式化定义.该模型明确了设计任务间的并行、顺序和协同关系,可以直接按设计任务构成活动网络图进行规划、分析、管理等工作,使设计过程具有良好的可变更性和可控性.     

京秦线提速路涵过渡段动力仿真与试验对比

结合京秦线提速改造工程进行了列车 路基动力仿真计算。在不同速度条件下,通过对路涵过渡段加固前后状态下机车车辆运行安全舒适性指标、轨道及路基主要动力性能指标的分析计算,对京秦既有线路涵过渡段提速到200km/h的适应性及加固方案的可行性提出了相应评价意见与建议,并与随后的实车试验进行了对比。试验测试结果验证了仿真分析的可靠性。     

Dynamics of ships running aground

A comprehensive dynamic model is presented for analysis of the transient loads and responses of the hull girder of ships running aground on relatively plane sand, gravel, or rock sea bottoms. Depending on the seabed soil characteristics and the geometry of the ship bow, the bow will plow into the seabed to some extent. The soil forces are determined by a mathematical model based on a theory for frictional soils in rupture and dynamic equilibrium of the fluid phase in the saturated soil. The hydrodynamic pressure forces acting on the decelerated ship hull are determined by taking into account the effect of shallow water. Hydrodynamic memory effects on the transient hull motions are modeled by application of an impulse response technique. The ship hull is modeled as an elastic beam to determine the structural response in the form of flexural and longitudinal stress waves caused by the transient ground reaction and hydrodynamic forces. A number of numerical analysis results are presented for a VLCC running aground. The results include bow trajectory in the seabed, time variation of the grounding force, and the maximum values of the sectional shear forces and bending moments in the hull girder.     

Experimental ivnestigation on flow fields of viscous fluid around two-dimensional wings and comparison with computational results

To examine the flow field of a viscous fluid around the trailing edge of a wing with respect to the Kutta condition or the Joukowski hypothesis, an experimental investigation into the velocity fields around two-dimensional (2D) wings NACA0012 and NACA4412 was carried out using an X-type hot-wire anemometer in a wind tunnel and the method of colored milk injection in a circulating water channel. The results of these investigations revealed that the flow of a viscous fluid at the trailing edge of a 2D wing is tangential to the face on the pressure side, and that the flow is very slow or reversed on the suction side due to separation when the angle of attack is greater than 7.5°. By flow visualization, a Kármán vortex street was found in the wake of both wings (NACA0012 and NACA4412) when the angle of attack was 5°. These results show that the ordinary Kutta condition with respect to the direction of outflow at the trailing edge is not necessarily satisfied in a viscous fluid, but the Kutta condition with respect to the pressure at the trailing edge is satisfied as usual. Numerical results, which have been obtained as the solution of Reynolds-averaged Navier-Stokes equations, show good agreement with above-mentioned experimental results. Therefore, CFD (Computational Fluid Dynamics) simulation has proved to be very effective for studying steady viscous flow around the trailing edge of a 2D wing.     

流函数法在减径拔管上限分析中的应用

应用流函数法建立减径拔管的动可容速度场，用上限原理得出减径拔管的上限解，分析了摩擦状态，变形程度及相对壁厚等工艺参数对拉拔载荷的影响，从而得出最佳工艺参数。