子空间分解与淘汰优化方法

提出一种新的多学科设计优化方法,即子空间分解与淘汰优化方法.该方法通过子空间的分解和淘汰,提高剩余子空间的近似模型精度,基于子空间近似模型优化获取最优解.首先,基于设计空间近似模型获取最优解,如果近似模型达到满意精度,则终止优化;否则将设计空间分解为多个子空间.然后,各子空间基于近似模型优化,如果子空间没有可能获得优于...     

建筑外保温系统消防安全问题及对策研究

近年来,我国与建筑外保温系统有关的火灾事故频发,引起了社会对建筑外保温系统及外保温材料防火问题的高度关注。在对常见建筑外保温材料的性能特点及外保温系统的做法进行归纳总结的基础上,分析了相关火灾危险性;针对存在的消防安全问题,从完善法规体系、促进新技术应用、加强政府监管、整治现有火灾隐患以及应急救援准备等方面提出了加强建筑外保温系统消防工作的对策。     

某高炮数字指挥仪的改造

为了使某高炮数字指挥仪能够适应现代战争的需要,遵照中央军委关于"要用高新技术改造现役装备"的指示,在不降低原高炮数字指挥仪战术技术性能的基础上,加装了红外热像仪、激光测距机、激光距离转换计算机、雷达诸元转换计算机.使该装备不仅能够与部队现配置的雷达连接使用,还增加了目标探测手段,增强了夜间作战能力,提高了装备的性能,成为新一代的光电防空火控系统,适应现代战争的要求.     

Recent advances in catalytic combustion of AP-based composite solid propellants

Composite solid propellants (CSPs) have widely been used as main energy source for propelling the rockets in both space and military applications. Internal ballistic parameters of rockets like characteristic exhaust velocity, specific impulse, thrust, burning rate etc., are measured to assess and control the performance of rocket motors. The burn rate of solid propellants has been considered as most vital parameter for design of solid rocket motors to meet specific mission requirements. The burning rate of solid propellants can be tailored by using different constituents, extent of oxidizer loading and its particle size and more commonly by incorporating suitable combustion catalysts. Various metal oxides (MOs), complexes, metal powders and metal alloys have shown positive catalytic behaviour during the com-bustion of CSPs. These are usually solid-state catalysts that play multiple roles in combustion of CSPs such as reduction in activation energy, enhancement of rate of reaction, modification of sequences in reaction-phase, influence on condensed-phase combustion and participation in combustion process in gas-phase reactions. The application of nanoscale catalysts in CSPs has increased considerably in recent past due to their superior catalytic properties as compared to their bulk-sized counterparts. A large surface-to-volume ratio and quantum size effect of nanocatalysts are considered to be plausible reasons for improving the combustion characteristics of propellants. Several efforts have been made to produce nanoscale combustion catalysts for advanced propellant formulations to improve their energetics. The work done so far is largely scattered. In this review, an effort has been made to introduce various combustion catalysts having at least a metallic entity. Recent developments of nanoscale combustion catalysts with their specific merits are discussed. The combustion chemistry of a typical CSP is briefly discussed for providing a better understanding on role of combustion catalysts in burning rate enhancement. Available information on different types of combustion nanocatalysts is also presented with critical comments.     

钝体高超声速气动加热与结构热传递耦合的数值计算

气动加热与结构热传递耦合问题在航天和工程应用领域非常重要。分别采用松耦合与紧耦合方法,数值模拟了高超声速二维圆管绕流的流场与结构传热耦合的非定常过程。在紧耦合方法中,流场部分采用基于Navier Stokes方程的有限体积法,将AUSM+格式与时间方向的显式多步Runge Kutta法结合;结构传热部分采用基于二维热传导方程的Galerkin有限元法。流场与结构区通过交界面的热流和温度边界条件实现耦合。计算结果分别与实验、文献做了对比,结构内部温度变化关系以及壁面的热流分布均较好地吻合。两种耦合方式的计算结果对比表明,对于流场特征时间远小于结构传热特征时间的问题,松耦合方法计算效率高,精度与紧耦合方法接近。     

稳定正规环分解定理

提出了稳定正规环的概念；推广了正规环的分解定理；给出了正则局部环整性的一个简单证明；指出了研究正则环的一条新途径。     

非结构动网格分区并行计算方法

针对包含运动边界的非定常流动问题,基于弹簧近似法设计了一套非结构动网格分区并行计算流程,引入了METIS软件进行非结构网格二次剖分,研究了对接边界通信类型及其处理方法,基于消息传递并行编程模式实现了非结构动网格求解器的并行化。测试结果表明:该求解器具有较高的并行效率,网格变形模块对非结构动网格并行计算性能具有重要影响。     

基于协同相关度的作战任务分解优化

针对协同作战中任务分解的优化问题,构建了任务协同相关度的量化模型。对作战任务中几个基本概念进行定义,从时间、逻辑、功能3个维度对任务间的协同关系进行了形式化描述,在此基础上,建立了任务协同关系的综合度量模型。最后,通过设置任务协同度阈值的方法,对协同紧密的任务进行聚合,实现任务分解的优化。通过仿真实验验证了模型的可行性和有效性。     

Optimally scheduling interfering and non‐interfering cranes

This article treats the problem of scheduling multiple cranes processing jobs along a line, where cranes are divided into different groups and only cranes in the same group can interfere with each other. Such crane scheduling problems occur, for example, at indented berths or in container yards where double rail‐mounted gantry cranes stack containers such that cranes of the same size can interfere with each other but small cranes can pass underneath larger ones. We propose a novel algorithm based on Benders decomposition to solve this problem to optimality. In a computational study, it is shown that this algorithm solves small and medium‐sized instances and even many large instances within a few seconds or minutes. Moreover, it improves several best known solutions from the literature with regard to the simpler problem version with only one crane group. We also look into whether investment in more complicated crane configurations with multiple crane groups is actually worthwhile.