WINDOWS系统中的QoS保障机制研究

针对微软提出的常规服务质量(GeneralQualityofService,简称GQoS)的QoS解决方案,讨论了WINDOWS系统中的QoS保障机制。通过WINSOCK2的API函数设计程序,进行了Win98上的QoS性能测试。结果表明,在QoS启用的情况下,数据的传输时间和延迟抖动明显减小,说明WINDOWS系统中的QoS保障机制有效。     

一种新型甲醛气体清除材料的实验研究

采用溶胶-凝胶法将纳米TiO2负载在活性碳纤维上,制备出一种新型甲醛气体清除材料。在制备中依次掺杂Fe3+和十二烷基苯磺酸钠(SDBS)对纳米TiO2进行改性,研究了纳米TiO2光催化活性的变化,并测试了自制材料的甲醛清除效率。结果表明:Fe3+和SDBS的添加不会改变纳米TiO2的晶型结构,但有利于晶粒的成长和负载膜的光催化活性;添加体积分数分别为0.8%的Fe3+和3%的SDBS时,材料的甲醛清除效率最高。     

损伤铝合金表面超声焊接界面断口分析与结合机理

采用超声焊接铝合金箔材的工艺修复处理表面腐蚀受损的2A12CZ基体,并利用Quanta200型环境扫描电子显微镜分析了截面形貌及箔材与基体之间界面表面断口的微观形貌。结果表明：从截面来看,箔材与基体之间大部分发生了焊合,界面分界线大部分消失;从机械脱开的界面断口来看,其表面微观形貌表现为鳞片状及韧窝状的典型金属型断口形貌。这说明在给定条件下,焊接部位大部分呈冶金结合。最后对铝台金箔材与铝合金基体之间超声焊接机理进行了探讨。     

舰载试验指挥控制系统研究与实践

针对靶场海上试验发展的综合需求,对舰载试验指挥控制系统发展的必要性及现状进行了分析,重点从与靶场其它系统的接口关系、系统功能、体系结构及软件设计几方面完成了系统总体设计研究,最后阐述了系统实现过程的关键技术。实践表明,该系统的应用大大提高了海上试验指挥水平。     

The effect of al particle size on thermal decomposition,mechanical strength and sensitivity of Al/ZrH2/PTFE composite

To study the thermal decomposition of Al/ZrH2/PTFE with different Al particle size as well as mechanical strength and impact sensitivity under medium and low strain rates, molding-vacuum sintering was adopted to prepare four groups of power materials and cylindrical specimens with different Al particle size. The active decomposition temperature of ZrH2 was obtained by TG-DSC, and the quasi-static me-chanics/reaction characteristics as well as the impact sensitivity of the specimen were studied respec-tively by quasi-static compression and drop-hammer test. The results show that the yield strength of the material decreased with the increase of the Al particle size, while the compressive strength, failure strain and toughness increased first and then decreased, which reached the maximum values of 116.61 MPa, 191％, and 119.9 MJ/m respectively when the Al particle size is 12—14μm because of particle size grading. The specimens with the highest strength and toughness formed circumferential open cracks and reacted partly when pressed. Those with developmental cracks formed inside did not react. It is considered that fracture of specimens first triggered initial reaction between Al and PTFE to release an amount of heat. Then ZrH2 was activated and decomposed, and participated in subsequent reaction to generate ZrC. The impact sensitivity of the specimens decreased with the increase of Al particle size.     

Dynamic necking of a near α titanium alloy at high strain rates:Experiments and modelling

The tensile behaviour of near α Ti3Al2.5 V alloy, conceived for applications in aerospace and automotive engineering, is characterized from quasi-static to high strain rates. The material is found to present noticeable strain rate sensitivity. The dynamic true strain rate in the necking cross-section reaches values up to ten times higher than the nominal strain rate. It is also observed that beyond necking the dynamic true stress-strain curves present limited rate dependence. The experimental results at different strain rates are used to determine a suitable constitutive model for finite element simulations of the dynamic tensile tests. The model predicts the experimentally macroscopic force-time response, true stress-strain response and effective strain rate evolution with good agreement.     

Supercritical carbon dioxide as a new working medium for pneumatic launch: A theoretical study

Compared with the conventionally gaseous or liquid working media, the specific internal energy of supercritical carbon dioxide (SCD) is higher at the same temperature and pressure, and the critical temperature of carbon dioxide is close to room temperature, making SCD a potential new working medium for pneumatic launch. To analyze the feasibility of this conception, an analytical model of a pneumatic catapult is established on basis of the conservations of mass and energy. The model consists of a high-pressure chamber and a low-pressure chamber connected by multiple valves, and there is a movable piston in the low-pressure chamber that can push an aircraft to accelerate. The effects of the launch readiness state of SCD in the high-pressure chamber, the initial volume of the low-pressure chamber and the valve control on the movement of the aircraft are analyzed. It is found that there is a restrictive relation between the temperature and pressure of the launch readiness state of SCD, i.e., there is a maximum allowable launch readiness pressure when the launch readiness temperature is fixed. If this restrictive relation is not satisfied, the working medium in the low-pressure chamber will drop to its triple point within a few milliseconds, leading to a launch failure. Owing to this restrictive relation, there is an optimal launch readiness state of SCD with the highest working capacity for any allowable launch readiness temperature. The pressure of the low-pressure chamber will decrease significantly as the initial volume increases, leading to a decreased acceleration of the aircraft. The ac-celeration can be controlled below a critical value by a designed sequential blasting technique of multiple valves. The calculated results show that a 500 kg aircraft can be accelerated from 0 to 58 m/s in 0.9 s with 36 kg of carbon dioxide. This research provides a new technique for the controllable cold launch of an aircraft.     

基于统计的网络化指挥控制系统拓扑模型

灵活、安全、高效的拓扑是网络化指挥控制系统研究领域最基本的问题之一。针对复杂的网络化环境,拓扑统计模型对于构建可用、可信、可控的网络化指挥控制系统拓扑具有重要意义。对网络化指挥控制系统的功能性、安全性和服务质量方面的拓扑统计特性需求进行了总结,然后分别对当前的代表性拓扑模型进行分析,指出这些模型相对于网络化指挥控制系统拓扑统计特性需求存在的不足,最后给出研究中面临的问题和需要研究的内容,为该领域的下一步研究提供参考。     

基于动力学和扩散分段控制的Mg/H2O反应模型及数值分析

为了数值研究宽广温度范围内Mg/H2O的反应特性,分别建立了考虑部分MgO在液滴表面凝聚的Mg/H2O扩散燃烧模型和基于Arrhenius公式的Mg/H2O反应动力学模型.数值研究了Mg/H2O反应速率在扩散控制和化学动力学控制下随反应条件变化的规律.研究结果表明,Mg液滴扩散燃烧时间计算结果与文献值相符;提高温度和水...     

基于惩罚函数的C~4ISR系统效能指标聚合方法

针对C4ISR系统效能评估过程中指标聚合计算不合理的问题,提出了一种新的指标聚合计算方法,即惩罚函数法。分析了C4ISR系统效能评估方法的现状,以及常用的指标聚合方法;给出了C4ISR系统效能指标体系和指标度量方法;描述了惩罚函数的思想以及3种不同的函数形式;通过一个C4ISR系统效能评估算例,对3种惩罚函数的计算结果进行了对比分析,并给出了函数选择的建议。