网络数据驱动模型

本文在传统的客户机与服务器之间的软件体系基础上,提出了网络数据驱动模型这一新的结构。     

用InstallShield制作中文界面安装盘的高级技巧

本文介绍了用ＩｎｓｔａｌｌＳｈｉｅｌｄ制作安装盒的原理和方法,给出了其制作安装盘的一般步骤,并详细论述了用它制作安装盘的一些高级技巧。     

粮食物流系统中移动POS终端的设计

电子商务的发展对建立集信息流、商流、资金流和物流于一体的新型物流配送中心提出了更高的要求。本文根据嵌入式系统设计的具体特点,分析了系统结构和移动终端的硬件组成,给出了实现该系统的软、硬件终端,以及WAP网关的解决方案。     

两种水轮发电机组开机控制技术的比较及优化

本文建立了水轮发电机组仿真模型,并以某电站的水流特性、机组惯性等实际参数作为仿真模型参数,着重研究水轮发电机组的两种开机控制规律,分析了原有以空载开度为限制的机组开机控制技术,提出以恒转速变化率为控制目标的机组开机控制技术,并将两种开机控制技术进行了仿真比较。通过仿真波形分析比较表明,两种开机控制技术各自具有的优越动态性能。在工程实践中,将这两种开机控制技术都应用到水轮机调速器开机程序中,可以根据水电站现场对开机动态性能的不同要求在停机态切换两种开机控制流程。     

The aeroelastic effects on the scatter phenomenon of wind-tunnel data

The unsteady Reynolds-averaged Navier-Stokes equations coupled with the k SST turbulence model are solved to obtain the steady and unsteady aerodynamic forces for airfoils and wings.The effects of vibration types and amplitudes on aerodynamic forces of airfoils and wings are studied.The deformation characteristics of a swept wing induced by steady aerodynamic load are presented.It is found that for a vibrating elastic wing at small and medium incidences,its mean aerodynamic loads are almost the same as those obtained from the static one.On the contrary,at high incidences especially around the stall incidence,the vibration may change the mean values.In addition,the larger amplitude is,the larger discrepancy will be.For a swept wing,the steady aerodynamic loads usually lead to the "pitching down" effect on the wing tip which delays the stall compared with a rigid one;But this phenomenon dose not occur on a aeroelastic wing which can induce the separation ahead and trigger the stall.The above conclusions are in good agreement with the scatter characteristics of wind-tunnel data.The reason why the data obtained from wind tunnel and CFD are different is also analyzed.Meanwhile,it can be an explanation for scatter phenomenon of wind-tunnel data,especially for high incidence cases,which remains a puzzle so far.     

Multidisciplinary design optimization of adaptive wing leading edge

Adaptive wing can significantly enhance aircraft aerodynamic performance, which refers to aerodynamic and structural opti-mization designs. This paper introduces a two-step approach to solve the interrelated problems of the adaptive leading edge. In the first step, the procedure of airfoil optimization is carried out with an initial configuration of NACA 0006. On the basis of the combination of design of experiment (DOE), response surface method (RSM) and genetic algorithm (GA), an adaptive air-foil can be obtained whose lift-to-drag ratio is larger than the baseline airfoil’s at the given angle of attack and subsonic speed.The next step is to design a compliant structure to achieve the target airfoil shape, which is the optimization result of the previous step. In order to minimize the deviation of the deformed shape from the target shape, the load path representation topology method is presented. This method is developed by way of GA, with size and shape optimization incorporated in it simul-taneously. Finally, a comparison study with the Solid Isotropic Material with Penalization (SIMP) method in Altair OptiStruct is conducted, and the results demonstrate the validity and effectiveness of the proposed approach.     

一种基于P系统的图像阈值分割方法

将P系统引入到图像阈值分割中,提出了一种基于P系统的图像阈值分割方法。采用一个两层膜的组织型P系统作为其计算框架,每个膜作为独立的并行计算单元,速度一位置模型作为进化规则,同时采用同向／反向转运规则交换和共享膜之间的对象。实验结果表明,这个基于P系统框架的阈值分割方法具有可用性和有效性,能为图像寻找最优的分割阈值。     

FPGA的动力电池检测系统研究

为提高动力电池使用效率,提出了一种基于FPGA的动力电池检测系统的设计方案.采用AD转换芯片实现对电池电压、电流的采集,数字温度传感器对温度进行采集,再通过软件实现对数据的处理和实时显示.系统运行稳定,数据处理能力强,集成度高,易于扩展.     

农村公共支出、基本建设投入与城乡收入差距

根据我国1978-2006年有关数据,建立向量自回归模型,对我国农村公共支出、基本建设投入与城乡收入差距的长期均衡关系进行了检验,在协整关系存在的前提下,进一步检验了三者的格兰杰因果关系,并利用脉冲响应函数对三者的动态关系进行了分析.实证结果显示,我国农村公共支出和基本建设投入有助于减少城乡收入差距,而且农业基本建设投入的作用较大.     

UG在无盘站机房上的教学与使用问题分析及解决方案

对UG软件功能进行了简单介绍,对UG在无盘站上教学与使用过程中遇到的问题进行了分析并提出解决方案。针对使用中遇到的运行问题,详细介绍了通过VB编程的方法解决UG在无盘站上运行问题。