弹塑性梁动态断裂的线弹簧模型

The elastic-plastic line-spring model is proposed to analyse the dynamicfracture of a cracked beam of ductile material in present paper. It can be expected from thenumerical results that this method for the analysis of dynamic fracture under elastic-plasticconditions will be valuable due to its computational simplicity.     

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。     

一种新的基于特征值分解的双站无源定位算法

在自卫式噪声干扰的条件下,地面制导雷达将无法得到目标的斜距信息,无法实现对目标的定位,此时只有采用雷达组网方式,利用2个或多个雷达站的测角信息来对空间目标进行定位。提出一种基于特征值分解的新的定位跟踪算法,该算法具有计算简单、清晰,运算量小的优点,仿真也表明该算法有较好的精度。     

视频监控系统中的动目标检测新方法

在分析了现有算法在复杂背景下所存在的不足的基础上,提出了一种适用于视频监控系统的基于视频序列像素时空相关性检测的动目标检测方法.该方法首先用每一帧中像素的空间相关性检测出目标,再用序列图像中目标的时间相关性检验目标的真实性,从而最终确定是否有运动目标.试验表明,该方法能很好地检测出运动目标,并具有较强的抗干扰能力.     

Numerical studies on four-engine rocket exhaust plume impinging on flame deflectors with afterburning

This paper studies the four-engine liquid rocket flow field during the launching phase. Using three-dimensional compressible Navier-Stokes equations and two-equation realizable k-epsilon turbulence model, an impact model is established and flow fields of plume impinging on the two different shapes of flame deflectors, including wedge-shaped flame deflector and cone-shaped flame deflector, are calcu-lated. The finite-rate chemical kinetics is used to track chemical reactions. The simulation results show that afterburning mainly occurs in the mixed layer. And the region of peak pressure occurs directly under the rocket nozzle, which is the result of the direct impact of exhaust plume. Compared with the wedge-shaped flame deflector, the cone-shaped flame deflector has great performance on guiding exhaust gas. The wedge-shaped and cone-shaped flame deflectors guide the supersonic exhaust plume away from the impingement point with two directions and circumferential direction, respectively. The maximum pressure and temperature on the wedge-shaped flame deflector surface are 37.2% and 9.9% higher than those for the cone-shaped flame deflector. The results provide engineering guidance and theoretical significance for design in flame deflector of the launch platforms.     

The deformation and failure mechanism of cylindrical shell and square plate with pre-formed holes under blast loading

The deformation and failure mechanism of cylindrical shells and square plate with pre-formed holes under blast loading were investigated numerically by employing the Ansys 17.0 and Ls-Dyna 971. To calibrate the numerical model, the experiments of square plates with pre-formed circle holes were modeled and the numerical results have a good agreement with the experiment data. The calibrated numerical model was used to study the deformation and failure mechanism of cylindrical shells with pre-formed circle holes subjected to blast loading. The structure response and stress field changing process has been divided into four specific stages and the deformation mechanism has been discussed systematically. The local and global deformation curves, degree of damage, change of stress status and failure modes of cylindrical shell and square plate with pre-formed circular holes are obtained, compared and analyzed, it can be concluded as: (1) The transition of tensile stress fields is due to the geometrical characteristic of pre-formed holes and cylindrical shell with arch configuration; (2) The existence of pre-formed holes not only lead to the increasing of stress concentration around the holes, but also release the stress concentration during whole response process; (3) There are three and two kinds of failure modes for square plate and cylindrical shell with pre-formed holes, respectively. and the standoff distance has a key influence on the forming location of the crack initiating point and the locus of crack propagation; (4) The square plate with pre-formed holes has a better performance than cylindrical shell on blast-resistant capability at a smaller standoff distance, while the influence of pre-formed holes on the reduction of blast-resistant capability of square plate is bigger than that of cylindrical shell.     

针对KMC局部最优问题的飞蛾捕焰优化方法

针对传统飞蛾捕焰(MFO)算法求解复杂函数时后期收敛速度慢与求解精度较低等问题,提出了一种基于快速收敛的飞蛾捕焰(RMFO)算法.采用最大最小距离积的方法来初始化飞蛾群,能够提高算法全局收敛速度并且优化解的质量,同时构造出MFO算法的适应度函数作为寻优函数.将RMFO算法和有K均值聚类算法(KMC)进行交叉迭代,构建基于RMFO优化的KMC算法,求解聚类中心时能够改善聚类性能,可以解决现有KMC算法选取初始聚类中心不确定陷入结果局部最优的问题.实验结果表明,通过用UCI国际通用测试数据库的Iris、Wine和Glass 3种数据集,对RMFO算法和优化KMC算法进行性能测试,提出的RMFO算法更加精准,收敛速度快,不易陷入局部最优解,同时,优化KMC算法的聚类性能更好.     

基于调制/解调的动态响应测试方法

在磁悬浮列车中,悬浮控制系统要求间隙传感器的动态特性,但无法用机械方法测试较高频率时的动态特性。根据传感器工作机制,用模拟涡流场来代替被测导体的涡流效应,提出基于调制/解调原理的动态特性测试方法,并分别对正弦信号和方波信号的测试方法进行了探讨。最后给出了两种特征信号的传感器动态特性测试结果。实验表明,这种方法能够满足测试要求,相对于机械方法有很大的优越性。     

Optimal inventory control policy for periodic‐review inventory systems with inventory‐level‐dependent demand

We consider a setting in which inventory plays both promotional and service roles; that is, higher inventories not only improve service levels but also stimulate demand by serving as a promotional tool (e.g., as the result of advertising effect by the enhanced product visibility). Specifically, we study the periodic‐review inventory systems in which the demand in each period is uncertain but increases with the inventory level. We investigate the multiperiod model with normal and expediting orders in each period, that is, any shortage will be met through emergency replenishment. Such a model takes the lost sales model as a special case. For the cases without and with fixed order costs, the optimal inventory replenishment policy is shown to be of the base‐stock type and of the (s,S) type, respectively. © 2012 Wiley Periodicals, Inc. Naval Research Logistics, 2012     

多核环境下负载均衡的并行离散事件全局调度机制

分析了多核环境下传统的离散事件时间弯曲并行系统的性能,针对其事件调度开销小和负载均衡能力强难以兼得的问题,提出了一种基于分布式队列的全局调度机制,设计了相应的数据结构和调度算法,大大减少了锁开销.通过大量实验对多核环境下几种典型离散事件系统并行策略的性能分析表明,本文提出的全局调度策略不仅事件调度开销小,而且回滚率大大降低,有效克服了传统策略回滚量较大或难以实现动态负载平衡的情况,并具备良好的可扩展性.