大企口缝单孔空心板桥截面等效方法研究

采用不扣除企口缝部分的近似计算方法和扣除企口缝的精确计算方法对大企口缝单孔空心板截面等效方法进行研究,得出近似等效计算方法的误差远远大于5%,不能满足工程需要,故在等效计算中,企口缝不能忽略,需使用面积等效、惯性矩等效、形心轴位置不变等3个原则方可求得其精确解.研究结论可为工程设计人员处理同类问题提供参考.     

电视购物调查分析——以陕西电视台“乐家购物”为例

对"乐家购物"消费者的调查数据用交互式列联表作初步的描述分析,表明随着年龄的增长、教育程度的提高、月收入的增加,选择电视购物的次数都有增加的趋势;构建Logistic回归模型对影响电视购物的因素作深入分析研究,揭示影响消费者选择电视购物的主要因素是年龄和受教育程度,并为电视购物的发展提出建议。     

低能电子束曝光的散射研究

采用Mott弹性散射截面和Monte Carlo计算方法进行模拟,将Joy和Lou的Bethe修正公式作为解决能量损失问题的非弹性散射模型。描述电子束入射固体过程,确定散射角、方位角、自由程和散射点处能量等参数。利用能量不超过5keV的低能电子束,模拟在不同厚度的抗蚀剂中进行的刻蚀过程,得到了不同能量电子束在衬底表面光刻的最佳抗蚀剂厚度。     

低雷诺数气液交叉流装置研究（I）——孔流液柱流动特性数值模拟

针对低雷诺数的气液交叉流气体净化过程,提出有效避免二次雾沫夹带的液柱流体力学条件。数值模拟结果表明,液柱表面随着离开孔口的距离而变化,采用公式Lb／d=2．84We^0.694能有效预测液柱的断裂行为。     

中美文化差异对国际商务谈判的影响

经济全球化浪潮下的中关经贸合作达到前所未有的高度,但文化差异却时常成为中关商务谈判的障碍。本文通过文化差异对中关商务谈判的影响做出分析,指出文化在中美商务谈判活动中具有的重要作用并提出相应对策。     

端部约束悬臂输流管道的非线性动力学特性

针对悬臂端受线性弹簧支承和扭转弹簧约束的约束悬臂输流管道,采用分岔图、相平面图、Poincare截面和Lyapunov指数等非线性振动的数值仿真方法,研究其在自激-参数激励-外激励联合激励作用下的非线性动力学特性,分析系统出现周期和混沌运动响应的参数条件,揭示其通向混沌的途径,探寻各参数对输流管道振动特性的影响规律和各参数之间的相互制约关系.数值仿真结果表明,管道系统随质量比、端部约束刚度和管道粘弹性系数的不同,分别呈现周期、概周期、阵发性和混沌运动多种响应形式,系统通过倍周期分岔或阵发性进入混沌,通过倍周期倒分岔脱离混沌.     

基于VTK的虚拟心脏切面交互式可视化方法

为解决传统医学影像技术方向性单一的问题,满足临床医学从不同方位从整体或切面等多角度对器官组织进行观察分析的需求,提出了心脏核磁共振成像(MRI)数据的体可视化和任意角度切面的可视化方法.基于可视化工具包VTK,在VC6.0开发环境中,运用光线投射算法设计并实现了MRI羊心脏切片数据的三维体绘制,横断、冠状、矢状位置的标准切片、切面以及任意角度、任意位置切面的绘制技术.通过简单的鼠标操作就可以实时的对切面进行移动、旋转、缩放等交互操作.实验结果表明:该方法有助于医生从多个方位观察整体器官组织和切面形态.在疾病预防、医疗诊断、手术方案制定以及术后评价中具有较大的实用价值.     

钢筋混凝土柱-H型钢斜梁结构有限元分析

钢筋混凝土柱-H型钢斜梁结构由混凝土和钢两种性能差异较大的材料构成,其受力性能相对复杂.针对大部分设计人员采用PKPM进行该结构设计的现状,笔者将ANSYS考虑大变形、非线性的计算结果引入.分析表明,因PKPM未考虑非线性等因素,故导致相同条件下水平推力和水平位移的计算结果存在较大偏差.     

Numerical study on the restriction speed of train passing curved rail in cross wind

The results of numerical investigations of aerodynamic forces and moment coefficients of flow passing a simplified train geometry under different wind speeds are summarized. To compute numerically the different coefficients, the three-dimensional Reynolds-Averaged Navier-Stokes (RANS) equations, combined with the k-ε turbulence model, were solved using finite volume technique. The pres-sure-velocity fields were coupled using the SIMPLE algorithm. At each iteration the pressure correction was obtained by sol...     

Design concept of three-dimensional section controllable internal waverider hypersonic inlet

A new hypersonic inlet named three-dimensional section controllable internal waverider inlet is presented in this paper to achieve the goal of section shape geometric transition and complete capture of the upstream mass. On the basis of the association between hypersonic waverider airframe and streamtraced hypersonic inlet, the waverider concept is extended to yield results for the internal flows, namely internal waverider concept. It is proven theoretically that not osculating cones but osculating axisymmetric theory is appropriate for the design of section controllable internal waverider inlet. And two design methods out of the internal waverider concept are proposed subsequently to construct two inlets with specific section shape request, triangle to ellipse and rectangle to ellipse ones. The calculation results show that the inlets are capable of keeping their shock structures and the main flow characteristics exactly as their derived flowfield. Further, the inlets successfully capture all the upstream mass despite their complicated cross-section transitions. It is believed that the concept proposed explores a new way of designing three-dimensional hypersonic inlets with special demand of section shape transition. However, the detailed flow characteristic and the performance of the internal waverider inlets are still under investigation. Supported by the National Natural Science Foundation of China (Grant No. 90405009)