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.     

Partial penetration of annular grooved projectiles impacting ductile metal targets

Changing and optimizing the projectile nose shape is an important way to achieve specific ballistic performance. One special ballistic performance is the embedding effect, which can achieve a delayed high-explosive reaction on the target surface. This embedding effect includes a rebound phase that is significantly different from the traditional penetration process. To better study embedment behavior, this study proposed a novel nose shape called an annular grooved projectile and defined its interaction process with the ductile metal plate as partial penetration. Specifically, we conducted a series of low-velocity-ballistic tests in which these steel projectiles were used to strike 16-mm-thick target plates made with 2024-O aluminum alloy. We observed the dynamic evolution characteristics of this aluminum alloy near the impact craters and analyzed these characteristics by corresponding cross-sectional views and numerical simulations. The results indicated that the penetration resistance had a brief decrease that was influenced by its groove structure, but then it increased significantly-that is, the fluctuation of penetration resistance was affected by the irregular nose shape. Moreover, we visualized the distribution of the material in the groove and its inflow process through the rheology lines in microscopic tests and the highlighted mesh lines in simulations. The combination of these phenomena revealed the embed-ment mechanism of the annular grooved projectile and optimized the design of the groove shape to achieve a more firm embedment performance. The embedment was achieved primarily by the target material filled in the groove structure. Therefore, preventing the shear failure that occurred on the filling material was key to achieving this embedding effect.     

Transshipment through crossdocks with inventory and time windows

A major challenge in making supply meet demand is to coordinate transshipments across the supply chain to reduce costs and increase service levels in the face of demand fluctuations, short lead times, warehouse limitations, and transportation and inventory costs. In particular, transshipment through crossdocks, where just‐in‐time objectives prevail, requires precise scheduling between suppliers, crossdocks, and customers. In this work, we study the transshipment problem with supplier and customer time windows where flow is constrained by transportation schedules and warehouse capacities. Transportation is provided by fixed or flexible schedules and lot‐sizing is dealt with through multiple shipments. We develop polynomial‐time algorithms or, otherwise, provide the complexity of the problems studied. © 2005 Wiley Periodicals, Inc. Naval Research Logistics, 2005     

次氯酸钙乳液消毒剂模拟剂的研究

研究了一种次氯酸钙乳液消毒剂的模拟剂,以及一些影响稳定性因素．该模拟剂是以氢氧化钙为分散相,水为分散介质,表面活性剂和无机盐为稳定剂组成．实验结果表明,该模拟剂具有与次氨酸钙消毒乳液相同的物理性能,并且无污染,可用于教育、作训之中．     

"三个代表"与马克思主义哲学教育

在马克思主义哲学教学中实现"三个代表"重要思想的"三进入",必须引导学员全面把握"三个代表"蕴涵的哲学智慧和科学实践观,深刻领会"三个代表"对唯物史观的运用和发展,培养其创新意识创新能力,通过"第二课堂"自觉实践"三个代表".     

预燃室内气氢气氧射流燃烧过程数值分析

建立了液体火箭发动机预燃室内气氢气氧射流燃烧过程的数学模型,包括燃烧过程控制守恒方程、湍流流动方程和湍流燃烧模型,以及求解控制方程所需的辅助关系式;给出了模拟射流燃烧过程的数值方法。对于给定的预燃室结构型式和尺寸,研究了喷嘴构型和氧的喷射方式对化学反应流场和燃烧性能的影响规律。结果表明,喷嘴构型和氧的喷射方式对流动过程和燃烧性能都有影响,且喷嘴结构的影响较为明显。     

湍流射流火焰中煤粉颗粒尺寸和结构的变化

采用湍流煤粉射流火焰模拟实际工业煤粉燃烧中的迅速热解,取样分析实验研究煤粉热解过程中颗粒尺寸和内部结构的变化。结果表明：在热解过程中煤粉颗粒体积发生了明显的膨胀,膨胀程度强烈地依赖于颗粒的初始尺寸和加热速率;热解时挥发份的迅速释放及煤的热塑性导致了颗粒内部的空心结构,这种结构有效地提高炭粒的燃烧速率。     

基于锥形量热法的油池火相似性及点火特性模拟实验

针对油料池火灾相似性及点火特性研究需要,构建了一种基于耗氧原理的油池火锥形量热法模拟实验系统,引入火灾尺度相似性概念,研究了实验室尺度油池火与真实尺度油池火的相似性关系,探讨了实验室尺度油池火预测真实尺度油池火的可行性,基于实验室尺度锥形量热法研究了油池火点火特性,得到了辐射强度、辐射距离对油料点燃时间的影响规律以及点燃时间与锥照射强度之间的拟合公式。     

单层平板吸波体界面反射模型的带宽理论研究

为了优化和指导吸波体设计,介绍了单层平板吸波体界面反射模型,推导了模型所揭示的吸波体内部能量流动关系。在此基础上,导出吸波体反射吸收带宽计算公式,由界面反射模型得出影响吸收带宽的因素,包括吸波层厚度、1/4波长厚度在峰值频率处的变化率、指定的反射波能量、前界面反射波能量及后界面反射波能量等。利用推导的能量关系及带宽公式,对3个同轴样品进行分析计算,结果表明计算值与实验值吻合较好,带宽公式推导正确。     

车辆半主动悬挂的频域控制算法

依据阻尼对车辆悬挂各指标传递特性的影响在频域上存在一定一致性的特点,提出了一种频域半主动控制算法.该算法只需在车身上安装一个加速度传感器,通过简单的规则判定悬挂振动频率所属频带范围,并实施相应的阻尼控制,即可显著改善车辆的乘坐舒适性和操纵稳定性.与天棚控制相比,频域控制算法振动抑制效果好,所需传感器少,因而具有更好的性价比和可靠性,适用于工程应用.