解析与数值结合的方法及采用子结构法的改进

本文以常微分方程求解器为基础,采用康脱洛维奇法和线法,分别以矩形截面杆的扭转问题和含裂纹的Motz问题为例,对解析与数值结合的方法,进行了初步的研究.特别是在将子结构法引入后,数值结果得到明显的改进.     

用于军事态势估计的协作知识模型

分布式人工智能（ＤＡＩ）是ＡＩ领域的一个新分支。ＤＡＩ研究的主要目的在于分析和设计大型复杂的协作智能系统。本文以军事智能决策过程中的重要环节──态势估计任务为背景,提出了用于实现分布式协作求解的知识表示框架ＤＥＳＷ系统。文章简要分析了军事态势估计领域背景,然后从系统设计的三个方面依次介绍了ＤＥＳＷ的系统组织模型、主体概念模型和分布式协作推理模型。     

八毫米低副瓣卡氏天线的优化设计

为了解决副面遮挡导致小口径卡氏天线（Ｄ＝２９３ｍｍ）副瓣电平恶化这一难题,本文提出了一种优化赋形方法。采用优化口径场分布,对主、副面形状进行赋形设计。用该法设计了一种八毫米低副瓣卡氏天线（ｓｌｌ１≤－２５ｄＢ）,实验结果与理论计算十分吻合。     

Ada网络文件传输系统的实现

本文介绍了一个在NETBIOS支持下用Ada的任务机制实现的网络上任意两节点间的文件全双工传输系统。传输时,文件以数据报的分组形式发送,由Ada 的任务特性来管理收、发进程,实现后台全双工操作。本文还简要地介绍了实现中的一些技巧。     

聚氨酯/环氧树脂SIN中的增塑作用初探

本文通过测量聚醚氨酯(PU)/环氧树脂(EP)SIN系列的玻璃化转变温度(Tg);并对该数据进行分析及用DiBenedetto理论式对该Tg数据进行了处理,发现PU/EP SIN中,EP对PU链段存在着较强的增塑作用,这个增塑作用与PU与EP网间的互穿作用并存,它主要受PU/EP组成配比等因素的影响。     

毫米波高效率双极化馈源的研制

本文介绍已设计成功的一个8毫米波段、能工作于双极化状态的高效率馈源。馈源的各种性能指标比较优良,理论与实验十分吻合,文中提供了一组新的通用设计曲线,在设计各波段的变锥角高效率多模馈源时均可利用。     

Rigid elliptical cross-section ogive-nose projectiles penetration into concrete targets

The elliptical cross-section ogive-nose projectile (ECOP) has recently attracted attention because it is well suited to the flattened shape of earth-penetrating weapons. However, the penetration performance of ECOPs has not been completely understood. The objective of this study was to investigate the pene-tration performance of ECOPs into concrete targets using a theoretical method. A general geometric model of ECOPs was introduced, and closed-form penetration equations were derived according to the dynamic cavity-expansion theory. The model was validated by comparing the predicted penetration depths with test data, and the maximum deviation was 15.8％. The increment in the penetration depth of the ECOP was evaluated using the proposed model, and the effect of the major—minor axis ratio on the increment was examined. Additionally, the mechanism of the penetration-depth increment was inves-tigated with respect to the caliber radius head, axial stress, and resistance.     

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.     

浅谈变声期声乐教学的要求与方法

对于许多高等院校的音乐教育专业来说,培养目标的主要在于培养合格的中小学音乐教师。而这对于即将成为音乐教师的学生来说,如何掌握青少年变声期前后的声音特征,心理特征;并能运用科学的方法,适当的要求来进行教学,具有非常重要的意义。     

无人机飞行训练资源配置效率的AHP-Arena综合评价方法

为降低传统层次分析法(analytic hierarchy process,AHP)赋权过程主观片面性影响,提出了一种综合AHP与Arena仿真建模技术的无人机训练资源配置效率评价方法。基于飞行训练流程分析,确定了训练资源配置效率影响因素和效率评价指标,建立了层次型综合评价体系,概括了AHP-Arena综合评价步骤。利用Arena建模软件构建训练流程动态仿真系统并验证有效性,采用单变量数值仿真法、均方差决策法完成了影响因素客观赋权,通过线性加权综合法得出综合评价系数,实现资源配置效率评价与方案优选。实例应用说明了该方法的有效性,同时,该方法可推广至其他类似的训练过程中,亦可为其他多因素、多指标评价决策过程提供借鉴。