具有可控细节层次的阴影空间新算法

首先阐述了阴影空间算法 ,然后对基于层次结构化包围盒和光线投射技术的阴影空间新算法进行了详细地研究。采用本算法可使生成的阴影效果具有可控细节层次。     

旋转弹丸空气动力特性数值解法

为提高在弹道计算和弹丸设计中弹丸空气动力系数精度,采用隐式LU算法求解N S方程并考虑代数湍流模型,在旋转物面边界条件下计算弹丸的阻力、升力、俯仰力矩、滚转阻尼力矩、马格努斯力和力矩。通过对美国T388等弹丸的气动力系数计算并与弹道靶试验数据进行比较,以及对某榴弹的气动力计算结果在弹道计算中进行应用分析,表明用数值模拟得到的旋转弹丸空气动力系数好于以前用工程方法给出的结果。     

限时图形系统的限时计算和渲染技术

在介绍了限时图形系统概念模型的基础上 ,指出限时渲染也是限时图形系统的一个基本特征 ,并从软、硬件两个方面对当今国内外采用的一些典型的提高实时图形渲染性能的技术和方法进行了明确的分类和阐述 ,提出了根据模型特点选用适当渲染技术的思想     

Direct ink writing of 3D-Honeycombed CL-20 structures with low critical size

3D-Honeycombed CL-20 structures with low critical size of detonation have been fabricated successfully for intelligent weapon systems using a micro-flow direct ink writing (DIW) technology. The CL-20-based explosive ink for DIW technology was prepared by a two-component adhesive system with waterborne polyurethane (WPU) and ethyl cellulose (EC). Not only the preparation of the explosive ink but also the principle of DIW process have been investigated systematically. The explosive ink displayed strong shear-thinning behavior that permitted layer-by-layer deposition from a fine nozzle onto a substrate to produce complex shapes. The EC content was varied to alter the pore structure distribution and rheological behavior of ink samples after curing. The deposited explosive composite materials are of a honeycombed structure with high porosity, and the pore size distribution increases with the increase of EC content. No phase change was observed during the preparation process. Both WPU and EC show good compatibility with CL-20 particles. Apparently high activation energy was realized in the CL-20-based composite ink compared with that of the refined CL-20 due to the presence of non-energetic but stable WPU. The detonation performance of the composite materials can be precisely controlled by an adjustment in the content of binders. The 3D honeycombed CL-20 structures, which are fabricated by DIW technology, have a very small critical detonation size of less than 69 μm, as demonstrated by wedge shaped charge test. The ink can be used to create 3D structures with complex geometries not possible with traditional manufacturing techniques, which presents a bright future for the development of intelligent weapon systems.     

Economic impact of the ministry of defence’s budget: methodological design and results for the Spanish economy

This article analyses the economic impact of the expenditure budget of the Spanish Ministry of Defence (MoD) and its Autonomous Agencies (AA), distinguishing direct, indirect and induced effects. The input–output methodology is used to find intersectoral effects on the rest of the economy. The article quantifies the economic impact in terms of production, gross value added (GVA), employed population, tax revenue, and also in terms of its contribution to the gross domestic product (GDP) of Spain in 2010. The results show that the activity of the MoD and AA generates 1.2% of the country’s GDP and 1.7% of total employment in that year.     

高超声速飞行器前体外形设计与气动特性分析

利用数值计算开展了高超声速飞行器前体气动特性的考察,重点研究了三维效应对于前体流场及预压缩性能的影响,提出了抑制三维侧缘溢流影响、改善三维前体气动性能的前体侧缘设计思想,考察了侧缘外形的容积效率,提出了有效容积效率的概念和评估方法,对于不同侧缘形式的前体构型进行了气动特性的考察,给出了不同前体构型气动特征的变化规律。     

吻切锥乘波构型优化设计与分析

吻切锥乘波构型是未来高超声速有动力巡航飞行器气动外形重要的设计参考。采用参数化设计方法实现了吻切锥乘波构型的设计,并利用工程估算的方法对构型的气动性能进行了分析;在多参数正交试验分析的基础上,开展了以升阻比,容积和容积率为目标的设计优化。CFD计算显示,优化的外形具有良好的升阻比和容积率性能,且底部流动均匀,是实现高超声速飞行器前体/超燃发动机进气道一体化的重要参考。     

基于小波神经网络的货运量预测

选取我国1979—2011年国民生产总值、能源生产总值、进出口贸易额、社会消费品零售总额和固定资产投资总额5项指标作为货运总量的主要影响因素,以货运总量为输出,建立了基于Morlet小波函数的小波神经网络预测模型。该模型能够揭示货运量与相关变量之间的非线性映射关系,经实例分析得到了较满意的结果,并通过与实际货运量和BP神经网络预测结果的对比,证明了小波神经网络在货运量预测方面应用的可行性。     

高精度有限体积法与间断有限元法的比较

通过数值算例,比较了高精度有限体积法和间断有限元法在求解不同问题时的表现。研究发现:在精度相同的条件下,间断有限元法的计算误差要明显小于有限体积法;间断有限元法的重构过程与高精度有限体积法相比较为简单,但高阶情形下解多项式的自由度较多并且需要计算体积分,因此整个求解时间较长。降低时间积分时解多项式的自由度数目是实现高精度算法在实际问题中应用的重要手段。     

考虑压缩性影响的超空泡流动数值计算

为了研究水下航行体航速接近水中声速时水的可压缩性对超空泡外形的影响,采用理想可压缩流体定常流动以及Riabouchinsky空化封闭模型,基于势流理论和有限体积方法,对绕圆盘空化器的超空泡流动进行了数值计算.计算时考虑到水的压缩性,水的状态方程采用Tait幂次率.提出了一种新的超空泡外形迭代方法并分析了流体压缩性对超空...