基于VS．NET 2005的GPS组件封装

首先分析GPS接受器输出信息的格式,然后介绍.NET2.0 SerialPort类的使用.在此基础上,基于VS.NET 2005平台开发一个GPS组件.给出了必要的过程和重要的代码.该组件在导航、无线监测系统中具有重要的作用.     

基于MES的生产管理系统应用

通过对某航空企业车间生产管理特点的分析,采用B/S模式以及ASP.NET C# SQL Server2000设计开发基于MES的生产管理系统.介绍该系统的设计原理、软硬件结构图,着重分析说明计划管理系统的开发过程、技术关键及具体实现方法和运行结果.该系统为某航空企业的车间实施计算机管理、提高生产效率提供了有效的工具.     

MATLAB与Visual C#.NET混合编程

在分析MATLAB与Visual C#．NET通用性和优缺点的基础上,介绍了MATLAB和Visual C#．NET混合编程的设计思想和编程特点。接着具体给出了基于visual C#．NET开发应用程序调用MATLAB算法的实现方法,并重点结合实例闸述了运用COM组件技术混合编程的具体步骤和注意事项。     

利用LEX及YACC实现嵌入式SQL分析器

Lex和Yacc是用来产生词法分析器和语法分析器的工具。本文讨论了LEX与YACC之间的关系 ,然后讨论了如何利用LEX和YACC实现嵌入式SQL分析器。在上面的研究基础之上 ,文章最后给出了利用LEX和YACC实现嵌入式SQL分析器的流程图。     

用C#构造可复用软件体系结构

以提高软件的复用性为目的,提出了一种用C#语言在.NET平台上,通过反射技术和XML配置文件,构造可复用软件体系结构的方案,并给出了具体的分析和实现代码。     

基于C/S架构的ERP中物流系统研制

介绍的是ERP系统中的物流子系统的开发过程，本系统前端采用Microsoft Visual Basic．net开发，后端利用SQL Server2000开发。系统采用了一种基于局域网的C／S为主体架构模式，以．NET与SQL SERVER2000中的．基于．NET数据库开发的DATASET思想，在具体实现中运用OLEDB控件与DATAGRID控件及T_SQL语句，用DataRelation对象来描述数据集中表问的关系。利用Toolbar控件与imagelist控件来实现主界面的设计。该系统是以一个合资企业为模型设计开发的物流信息管理系统。     

基于ASP.NET的计量器具管理系统设计

介绍了利用ASP.NET技术进行计量器具管理系统的设计,通过此系统可以完成注册登录、角色管理、信息录入与编辑、批量导入与修改、多条件查询、到期提醒、信息统计、报表打印、数据的备份与恢复等功能;后台数据库选用SQL Server 2008进行设计。     

剖析SQL Server数据库的备份与恢复

在基于Microsoft SQL Server(以下简称SQL Server)数据库的备份和恢复的方法下,从简单、实用的角度出发,提出了通过Powerbuilder(以下简称PB)应用工具实现SQL server数据库的备份和恢复,同时给出了该方法的主要代码。     

SQL查询性能的优化研究

数据库是应用程序的核心,为提高基于SQL Server数据库应用程序的执行效率,本文分析了SQL Server数据库的查询优化处理技术,分别讨论了建立索引,避免SQL排序,优化多表查询等技术,从而优化SQL查询的性能.     

．NET中网络数据传输的安全对策

通过网络数据传输实例,分析了在.NET中实现数据保密性和完整性的方法,并介绍了如何用C#语言实现.NET环境下的数据加密与解密以及如何利用HASH运算和数字签名保证数据的完整性。     

The effect of inlet conditions on the flow and heat transfer in multiple rotating cavity with axial throughflow

This paper discusses experimental results from two different build configurations of a heated multiple rotating cavity test rig.Measurements of heat transfer from the discs and tangential velocities are presented.The test rig is a 70% full scale version of a high pressure compressor stack of an axial gas turbine engine.Of particular interest are the internal cylindrical cavities formed by adjacent discs and the interaction of these with a central axial throughflow of cooling air.Tests were carried out for a range of non-dimensional parameters representative of high pressure compressor internal air system flows(Re up to 5×106 and Rez up to 2×105).Two different builds have been tested.The most significant difference between these two build configurations is the size of the annular gap between the(non-rotating) drive shaft and the bores of the discs.The heat transfer data were obtained from thermocouple measurements of surface temperature and a conduction solution method.The velocity measurements were made using a two component,LDA system.The heat transfer results from the discs show differences between the two builds.This is attributed to the wider annular gap allowing more of the throughflow to penetrate into the cavity.There are also significant differences between the radial distributions of tangential velocity in the two builds of the test rig.For the narrow annular gap,there is an increase of non-dimensional tangential velocity V/Ωr with radial location to solid body rotation V/Ωr=1.For the wider annular gap,the non-dimensional velocities show a decrease with radial location to solid body rotation.      

Research on Auto-detection for Remainder Particles of Aerospace Relay Based on Wavelet Analysis

Aerospace relay is one kind of electronic components which is used widely in national defense system and aerospace system. The existence of remainder particles induces the reliability declining, which has become a severe problem in the development of aerospace relay. Traditional particle impact noise detection (PIND) method for remainder detection is ineffective for small particles, due to its low precision and involvement of subjective factors. An auto-detection method for PIND output signals is proposed in this paper, which is based on direct wavelet de-noising (DWD), cross-correlation analysis (CCA) and homo-filtering (HF), the method enhances the affectiv-ity of PIND test about the small particles. In the end, some practical PIND output signals are analysed, and the validity of this new method is proved.     

Preparation of Highly Dispersed Antimony-doped Tin Oxide Nano-powder via Ion-exchange Hydrolysis of SnCl4 and SbCl3 and Azeotropic Drying

Antimony-doped tin hydroxide colloid precipitates have been synthesized by hydrolysis of SnCl4 and SbCl3 using: (1) an ion-exchange hydrolysis to remove chlorine ions, and (2) isoamyl acetate as an azeotropic solvent to obviate water. The obtained dried powder is of high dispersivity without any need for further grinding. The size and dispersivity of the final particles are investigated with the aid of TG-DTA, BET, XRD and TEM. After having calcined, the antimony-doped tin oxide nanopowder possesses a tetragonal rutile structure with high dispersivity, uniform particles and low hard agglomeration.     

Effects of Mo on the Microstructure and Hydrogen Sorption Properties of Ti-Mo Getters

The effects of Mo on the microstructure evolution, porosity and hydrogen sorption properties of Ti-Mo getters are investigated in this work. The results show that the addition of Mo prolongs the densification process of Ti-Mo getters and results in a significant amount of sintered pores. With the Mo content increasing, the porosity of getters firstly increases reaching the maximum value as it at- tains about 7.5wt.%, and then drops. At the room temperature, the hydrogen sorption property of getters increases progressively with the Mo content increasing, but the tendency is not very clear before its content lies below 2.5wt.%. When the Mo content achieves about 7.5wt.%, the hydrogen sorption property proves to be the best. The discussion is made about the above mentioned phenomena inclusive of hydrogen sorption properties of getters under different activation conditions (from 500-750 ℃).     

超声速燃烧数值模拟中的湍流与化学反应相互作用模型

高精度数值模拟有助于理解超声速湍流燃烧中湍流与化学反应的相互作用,可为发动机燃烧室等工程应用设计提供可靠的预测模型。除直接数值模拟外,目前在湍流燃烧应用中使用的大涡模拟和雷诺平均Navier-Stokes模拟均需要借助模型模化发生在湍流小尺度上的流动与化学反应过程对湍流大尺度运动的影响。现有的湍流与化学反应相互作用模型大致可分为:火焰面类模型和概率密度函数类模型,2类模型在不同的应用中各自具有优势和局限性。此外,现有模型大都基于低马赫数燃烧,而超声速燃烧中通常会伴随快速混合、局部熄火和再着火以及激波等复杂过程,这为发展其中的湍流与化学反应相互作用模型提出了更多的挑战。     

适于低轨卫星IP网络的单核共享树组播算法(英文)

为了解决低轨卫星IP网络中现有典型源组播算法的信道资源浪费问题,本文提出了一套单核共享树组播算法,即核心群合并共享树(CCST)和加权核心群合并共享树(w-CCST)算法。CCST 算法包括动态近似中心(DAC)选核方法和核心群合并组播路径构建方法。DAC方法专为周期、规律运动的低轨卫星网络提出,不需要复杂的星上计算。在核心群合并方法中,以核节点作为初始核心群,通过核心群和剩余组成员的最短路径方法逐步扩展直至整棵组播树构建完成,从而使得组播树的树代价最小,大大提高了网络的带宽利用率和组播传输效率。w-CCST 算法中所提出的加权因子可以调整树代价和端到端传播时延之间的折衷程度,因此,可以通过调整加权因子来适度增大树代价、降低端到端传播时延以支持某些端到端时延要求苛刻的实时组播业务。最后,与低轨卫星 IP 网络中典型算法进行了性能比较,仿真结果说明,CCST 算法的平均树代价比其它算法显著降低,w-CCST 算法的平均端到端传播时延小于 CCST 算法。     

Jet Vectoring Control Using a Novel Synthetic Jet Actuator

A primary air jet vectoring control system with a novel synthetic jet actuator (SJA) is presented and simulated numerically. The results show that, in comparison with an existing traditional synthetic jet actuator, which is able to perform the duty of either “push” or “pull”, one novel synthetic jet actuator can fulfill both “push” and “pull” functions to vector the primary jet by shifting a slide block inside it. Therefore, because the new actuator possesses greater efficiency, it has potentiality to replace the existing one in various appli- cations, such as thrust vectoring and the reduction of thermal signature. Moreover, as the novel actuator can fulfill those functions that the existing one can not, it may well be expected to popularize it into more flow control systems.     

Nonlinear Adaptive Slewing Motion Control of Spacecraft Truss Driven by Synchronous V-gimbaled CMG Precession

The slewing motion control of a truss arm driven by a V-gimbaled control-moment-gyro (CMG) is a nonlinear control problem. The V-gimbaled CMG consists of a pair of gyros that must precess synchronously. The moment of inertia of the system, the angular momentum of the gyros and the external disturbances are not exactly known. With the help of feedback linearization and recursive Lyapunov design method, an adaptive nonlinear controller is designed to deal with the unknown items. Performance of the proposed controller is verified by simulation.     

An SOR Implicit Time-accurate Scheme in Calculating Unsteady Flows

A new time-accurate marching scheme for unsteady flow calculations is proposed in the present work. This method is the combination of classical Successive Over-Relaxation (SOR) iteration method and Jacobian matrix diagonally dominant splitting method of LUSGS. One advantage of this algorithm is the second-order accuracy because of no factorization error. Another advantage is the low computational cost because the Jacobian matrices and fluxes are only calculated once in each physical time step. And, the SOR algorithm has better convergence property than Gauss-Seidel. To investigate its accuracy and convergency, several unsteady flow computa- tional tests are carried out by using the proposed SOR algorithm. Roe’s FDS scheme is used to discritize the inviscid flux terms. Un- steady computational results of SOR are compared with the experiment results and those of Gauss-Seidel. Results reveal that the numerical results agree well with the experimental data and the second-order accuracy can be obtained as the Gauss-Seidel for unsteady flow computations. The impact of SOR factor is investigated for unsteady computations by using different SOR factors in this algorithm to simulate each computational test. Different numbers of inner iterations are needed to converge to the same criterion for different SOR factors and optimal choice of SOR factor can improve the computational efficiency greatly.