ASP中session变量的丢失问题分析

Session对象是ASP中的一个内置对象，可以存储特定用户会话所需信息。用户只能访问属于自己的session变量，无法访问其他用户的session变量。现就session变量的丢失和处理进行了分析和探讨。     

J2EE平台会话管理机制分析与改进

在分析J2EE平台会话管理机制的基础上,指出了J2EE会话管理机制在会话状态管理方面的不足,提出了解决方案,论述了实现该方案时要解决的五个关键问题。     

非页面日志信息在改进会话识别中的应用研究

会话识别是web日志挖掘数据预处理的关键步骤,其质量对日志挖掘结果有重要影响。文章介绍了现有的会话识别方法,提出了利用数据清洗中废弃的图片等日志数据和web图结构,改进会话识别中的页面分组规则和路径补全算法,并通过实验证实方法对改善会话识别质量是有效的。     

ASP在机械制造企业的应用及发展现状

通过介绍了ASP在国内外的发展现状和发展趋势，以及机械制造企业对ASP服务模式的需求、ASP在机械制造企业的应用和发展现状，提出了将机械制造企业和ASP服务模式相结合的特点及优势。     

飞机通信寻址与报告系统消息安全研究及仿真

ACARS消息安全( AMS)以一种独立于底层通信机制的应用方式，通过安全机制及支持该机制的加密算法，提供数据机密性、消息认证和完整性的安全服务。介绍了AMS消息结构和处理过程，建议采用一种综合对称和非对称加密系统优势的航空通信方案，分析了安全会话过程，仿真试验证明， AMS在面对安全威胁时能保证ACARS消息的安全传输。     

面向高安全数据分发服务的身份认证协议设计

为解决数据分发服务安全规范中身份认证与密钥协商协议存在共享密钥建立缺乏公平性、缺乏验证密钥一致性机制及会话过程缺乏完整性等安全问题,以协议为基础,设计一种新的高安全数据分发服务身份认证与密钥协商协议。新协议引入了ACK机制,并利用D－H密钥交换和非对称密码体制特点解决了原协议存在的安全问题,具备实用性和更高的安全性。     

基于波长共享机制的机载WDM网络波长分配算法

针对航电网络节点间信息量的不同,依据子网划分理论,提出了一种光电混合式航电波分复用(WDM)网络结构,并在此基础上提出了一种基于邻接会话和行(列)会话共享波长的机载WDM子网路由波长分配算法。定义了邻接会话和行(列)会话,分析了会话间共享波长的原理,推导了波长需求数目。仿真结果证明,正常情况下该算法波长需求数目与Token算法一样,最好情况下相比Token本算法可减少éN/6ù的波长耗费(N为网络节点数),达到了有效利用波长的目的,且简单易实现,是一种值得参考的机载WDM网络RWA设计方法。     

远程网络教学组卷测试子系统的设计与实现

随着网络信息技术和计算机技术的飞速发展,远程教育作为一种新型教学方式日益完善,并且逐步发挥出巨大的作用。本文着重以《大学语文》远程网络系统组卷测试的设计和实现为例,介绍ADO和ASP技术在网络中的应用,以及系统组卷测试所特有的题型实现机制和方略。     

论会话含意的理解过程

根据会话语言特点，从关联理论角度，分析会话含意的理解过程，发现它实际上是听话者通过认知语境，将接收话语建立的新的假设进行关联、激活、选择、推理并获取会话含意的过程。对言语的理解离不开语境、语境制约着言语的选择和运用，二者密不可分。     

基于虚拟机的一种移动代理安全策略

主要研究在普适计算环境下移动代理的安全机制,提出了一种主从模式下代理密钥协商的协议,此协议实施的关键是使用指令系统可变的虚拟机.这种虚拟机可被动态生成,并且每次都使用不同的指令系统,以此来保证恶意宿主不能在短时间内获取会话密钥的信息.通过模拟攻击测试验证了此移动代理安全策略的有效性.     

ν-gap度量及其在飞行控制律评估中的应用

 传统控制律评估方法主要用于单输入单输出（SISO）系统，且对模型参数摄动考虑不够全面,针对这些不足，研究了ν-gap度量方法。在介绍系统广义稳定裕度相关概念的基础上，给出了ν-gap度量的定义、特点和性质以及近似摄动模型的计算，提出ν-gap度量评估控制律的步骤。实例结果表明，该方法不仅克服了上述传统评估方法的缺陷，而且还有根据所求的各摄动影响情况忽略影响小的元素，以减少计算量及可以找到最坏情况下的参数摄动组合等优点。     

Integrated Entry Guidance for Reusable Launch Vehicle

A method for the implementation of integrated three-degree-of-freedom constrained entry guidance for reusable launch vehicle is presented. Given any feasible entry conditions, terminal area energy management interface conditions, and the reference trajectory generated onboard then, the method can generate a longitudinal guidance profile rapidly, featuring linear quadratic regular method and a proportional-integral-derivative tracking law with time-varying gains, which satisfies all the entry corridor constraints and meets the requirements with high precision. Afterwards, by utilizing special features of crossrange parameter, establishing bank-reversal corridor, and determining bank-reversals according to dynamically adjusted method, the algorithm enables the lateral entry guidance system to fly a wide range of missions and provides reliable and good performance in the presence of significant aerodynamic modeling uncertainty. Fast trajectory guidance profiles and simulations with a reusable launch vehicle model for various missions and aerodynamic uncertain-ties are presented to demonstrate the capacity and reliability of this method.     

基于飞机油箱模型形状特征油量测量切片步长选择方法研究

 在分析飞机数字式油量测量过程中目前广泛使用的切片法油量测量原理的基础上,针对现有的定步长切片法无法得到准确、可靠的燃油质量特性数据库的缺陷,结合对飞机油箱模型形状特征的分析,提出了基于飞机油箱模型形状特征的油量测量切片步长选择方法。此方法包括切片步长整体和局部选择两个过程,整体选择以实现相邻两切片平面所夹油箱模型体积近似相等为目的来确定切片步长,以体现油箱模型截面整体变化规律;局部选择以设计切片平面与截面突变平面重合或尽可能接近的方式,突出油箱截面的局部变化特征。实验结果表明：该切片步长选择方法较定步长方法能够建立更为合理、可靠的燃油质量特性数据库,从而提高了油量测量精度。     

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.      

二维翼段颤振的μ控制

 采用超声电机作为作动器来实现含控制面的翼段颤振鲁棒抑制。针对作者设计的二维翼段颤振主动抑制系统，通过理论与实验相结合的方法，建立了考虑沉浮方向阻尼和作动器模型参数不确定性的控制系统模型，设计了μ控制器，并对控制器做了降阶处理。数值仿真和风洞试验表明，μ控制器可有效地抑制颤振的发生，将颤振临界速度提高23.4%。相对于H_∞控制器，μ控制器的控制效果和鲁棒性更好。     

航空发动机管路测量数据分割方法

 为了提高航空发动机管路测量数据的反求建模效率,提出了一种区域增长分割算法。该方法主要是利用管路表面在曲面索引系数映射、主曲率映射、高斯映射上的特性,并基于均值漂移算法和遗传算法提出了区域分割算法中种子区域的选择策略。然后利用区域增长分割方法实现了对管路测量数据的分割。经过仿真和实测数据验证,所提管路分割算法具有较好的分割质量和效率。     

Abnormal Shape Mould Winding

为解决网格化芯模的缠绕问题,本文提出了复合材料面片缠绕机理;接着详细分析了面片缠绕过程中的芯模凹曲面上纤维滑线和架空现象,应用微分几何曲面理论和空间几何理论,提出判据及其解决方案;最后,针对飞机发动机进气道的缠绕成型,编制缠绕控制程序并进行相应的实验,验证了面片缠绕方法的可行性。     

Interfacial Properties Modification of Carbon Fiber/ Polyarylacetylene Composites

This work was dedicated to performing surface oxidation and coating treatments on carbon fibers (CF) and investigating the changes of fiber surface properties after these treatments, including surface composition, relative volume of functional groups, and sur- face topography with X-ray photoelectron spectroscopy (XPS) and atom force microscopy (AFM) technology. The results show that, after oxidation treatments, interfacial properties between CF and non-polar polyarylacetylene (PAA) resin are remarkably modified by removing weak surface layers and increasing fiber surface roughness. Coating treatment by high char phenolic resin solution after oxida- tion makes interface of CF/PAA composites to be upgraded and the interfacial properties further bettered.     

Thermal Stresses and Cracks During the Growth of Large-sized Sapphire with SAPMAC Method

本文利用有限元法对冷心放肩微量提拉法(SAPMAC)生长大尺寸蓝宝石单晶过程中的热应力进行了模拟计算,应用临界缺陷理论解释了裂纹的萌生与扩展机理。研究表明,晶体内的热应力主要与晶体生长速率,环境温度和结晶取向有关;较大热应力多出现在结晶界面,放肩、收尾以及直径急剧变化等位置;最大热应力总是出现在籽晶与新生晶体的界面附近。裂纹将在临界缺陷位置产生,并在应力作用下沿a或m面扩展。计算结果与实验结果基本吻合,通过晶体生长系统和生长工艺的改进,对晶体的开裂问题得到了有效的抑制。     

Optimization Design System for Composite Structures Based on Grid Technology

To solve the topology optimization of complicated multi-objective continuous/discrete design variables in aircmit structure design, a Parallel Pareto Genetic Algorithm （PPGA） is presented based on grid platform in this paper. In the algorithm, the commercial finite element analysis （FEA） software is integrated as the calculating tool for analyzing the objective functions and the filter of Pareto solution set based on weight information is introduced to deal with the relationships among all objectives. Grid technology is utilized in PPGA to realize the distributed computations and the user interface is developed to realize the job submission and job management locally/remotely. Taking the aero-elastic tailoring of a composite wing for optimization as an example, a set of Pareto solutions are obtained for the decision-maker. The numerical results show that the aileron reversal problem can be solved by adding the limited skin weight in this system. The algorithm can be used to solve complicated topology optimization for composite structures in engineering and the computation efficiency can be improved greatly by using the grid platform that aggregates numerous idle resources.