经纬网络充气机翼构形特征与气动性能分析

将充气机翼应用于临近空间太阳能飞行器是具有创新性的设计概念。针对充气机翼构形特征和气动分析的相关问题,对构形特征进行分析和设计,并建立经纬网络充气机翼的模型;进一步运用数值方法,通过与标准翼型对比,分析二维充气机翼、三维经纬网络充气机翼的气动性能。数值分析结果表明,在设计的雷诺数条件下,充气机翼的气动性能相比于标准翼型有所降低。在此基础上,结合对流场结构和流动机理的研究,分析出导致充气机翼总阻力系数明显增加的主要原因是:充气机翼表面许多凹陷的局部区域所形成的涡结构,导致局部的摩阻有小幅的减小,但压差阻力大幅增加,最终使得总的气动性能有所降低。     

加油车加油系统瞬变流数值分析

针对加油车加油系统管路结构,利用特征线法和有限差分格式,对2种典型加油工况建立数学模型。用C#语言编制程序,对2种工况的泵出口压力和系统流量进行数值分析,得到压力和流量随时间变化的关系曲线。计算结果表明:单枪加油工况出现压力波动时间较早,且压力波动幅值较大。此方法更好地反映了加油系统的动态变化过程,为加油车虚拟训练系统的开发提供了理论依据。     

合成双射流冲击平板流场结构与模态分解分析

为揭示合成双射流冲击平板流场结构特征,通过大涡模拟方法对合成双射流冲击平板流动进行了仿真,采用有限时间Lyapunov指数方法对流场的拉格朗日涡结构进行了识别,并与欧拉框架下的速度矢量和涡量结果进行了对比分析。结果表明,在合成双射流两股射流交替作用下,射流核心区涡系结构较为复杂且涡量丰富,远离核心区存在一对稳定的涡结构,且拉格朗日涡结构与涡量对应较好,为合成双射流冲击冷却的布局设计提供了指导。另外,流场本征正交分解表明,第一阶模态关于激励器出口中心轴线大致对称,其能量占总体能量的35%,前6阶模态的能量占80%;根据前6阶模态所反映的流场特性,合成双射流冲击平板流场具有高度的对称性。     

高倍率脉冲放电锂电池的功率输出特性

由于电池内阻和极化现象的存在,锂电池在放电的瞬间会出现较大的电压跌落,高倍率脉冲放电锂电池更是如此。为了研究高倍率脉冲放电锂电池的功率输出特性,探讨温度、荷电状态和老化等因素对电池功率性能的影响规律,定义了锂电池的功率特性曲线,搭建了高倍率电池测试平台,并从温度、荷电状态和老化3个阻抗敏感因素开展实验研究。研究方法和结论对后期开展锂电池系统的峰值功率评估和功率曲线预测有一定的指导意义。     

Flow‐shop batch scheduling with identical processing‐time jobs

In many practical situations of production scheduling, it is either necessary or recommended to group a large number of jobs into a relatively small number of batches. A decision needs to be made regarding both the batching (i.e., determining the number and the size of the batches) and the sequencing (of batches and of jobs within batches). A setup cost is incurred whenever a batch begins processing on a given machine. This paper focuses on batch scheduling of identical processing‐time jobs, and machine‐ and sequence‐independent setup times on an m‐machine flow‐shop. The objective is to find an allocation to batches and their schedule in order to minimize flow‐time. We introduce a surprising and nonintuitive solution for the problem. © 2004 Wiley Periodicals, Inc. Naval Research Logistics, 2004     

Bounding the optimal burn‐in time for a system with two types of failure

Burn‐in is a widely used method to improve the quality of products or systems after they have been produced. In this paper, we consider the problem of determining bounds to the optimal burn‐in time and optimal replacement policy maximizing the steady state availability of a repairable system. It is assumed that two types of system failures may occur: One is Type I failure (minor failure), which can be removed by a minimal repair, and the other is Type II failure (catastrophic failure), which can be removed only by a complete repair. Assuming that the underlying lifetime distribution of the system has a bathtub‐shaped failure rate function, upper and lower bounds for the optimal burn‐in time are provided. Furthermore, some other applications of optimal burn‐in are also considered. © 2004 Wiley Periodicals, Inc. Naval Research Logistics, 2004     

Two‐machine flow shop no‐wait scheduling with a nonavailability interval

We study a two‐machine flow shop scheduling problem with no‐wait in process, in which one of the machines is not available during a specified time interval. We consider three scenarios of handing the operation affected by the nonavailability interval. Its processing may (i) start from scratch after the interval, or (ii) be resumed from the point of interruption, or (iii) be partially restarted after the interval. The objective is to minimize the makespan. We present an approximation algorithm that for all these scenarios delivers a worst‐case ratio of 3/2. For the second scenario, we offer a 4/3‐approximation algorithm. © 2004 Wiley Periodicals, Inc. Naval Research Logistics, 2004     

基于内角流动的板式表面张力贮箱内推进剂流动过程研究

分析了在微重力环境下,板式表面张力贮箱内推进剂的流动和定位过程.利用VOF方法对贮箱内推进剂的重定位过程进行了仿真计算,验证了贮箱及PMD的推进剂管理性能.用数学方法分析了液体在导流板的内角流动,用解析计算的方法求出流动过程中液面的长度,并和仿真计算结果进行了对比.因为实际的贮箱模型比较复杂,仿真计算结果和理论计算结果存在一定的误差,但其流动趋势保持一致.本文的工作能够为内角流动的研究提供有益的参考.     

线粘弹性材料中三维裂纹问题的加料有限元法

将加料有限元法扩展应用于线粘弹性材料三维断裂问题.为了反映裂纹尖端的奇异性,在裂尖附近的奇异区采用若干八节点六面体加料单元和过渡单元,非奇异区采用常规八节点六面体单元.三种单元分区混合使用形成求解域网格划分.基于Boltzmann叠加原理,推导了粘弹性材料的增量型本构关系,进而获得了增量加料有限元列式,并通过附加自由度计算粘弹性介质中裂纹应变能量释放率.数值算例验证了方法的正确性和有效性.     

基于STK的动能反卫作战信息流程构建

介绍了动能反卫星武器的信息系统构成及功能,对动能反卫作战过程进行了描述,提出了动能反卫作战中的信息需求,构建了动能反卫作战行动的信息流程。详细介绍了动能反卫星作战流程,并对作战信息需求进行分析。最后,利用卫星工具包(STK)实现一次对地基动能反卫星作战过程的仿真。