(修，2撤3)关键几何参数对超声速膨胀器流场和性能影响的数值研究

为了揭示关键几何参数对超声速膨胀器流动特性影响的规律,对3种隔板安装角和5种出进口面积比超声速膨胀器设计工况下的流场进行了数值研究。结果表明：随隔板安装角增加,斜激波向出口迁移,斜激波强度略有降低,超声速膨胀器膨胀比减小,效率提高;随出进口面积比增加,流道内高速区显著扩大并逐渐靠近压力面,斜激波增强,出口流动损失增加,超声速膨胀器膨胀比增大,效率降低。为获得综合性能较优超声速膨胀器结构,需在较小出进口面积比和较大隔板安装角之间做折衷选择。     

基于组合赋权雷达图实现电网电能质量综合评估

将改进的组合赋权雷达图方法用于电网电能质量综合评估。对主观、客观赋权法组合,基于组合权重与原权重之间的偏差尽可能小的优化思想,求取雷达图中各项指标的组合权值。利用各指标对应的扇形区域的对角线作为指标轴绘制雷达图,不仅最大限度体现各指标的独立权重,也反映了各指标之间的相互影响。利用雷达图的面积和周长两个变量完成对电能质量的综合评估。最后通过应用实例,验证了论文方法的合理性和在电能质量综合评估中的有效性。     

内编队地球重力场测量性能数值分析

内编队系统通过实现内卫星纯引力轨道环境和内卫星精密定轨,完成高精度地球重力场测量,实现了不依赖于加速度计的重力卫星实施新途径。针对内编队重力场测量性能难以解析分析的情况,基于MATLAB并行程序设计进行了重力场测量数值模拟,获得了内编队重力场测量的有效阶数及其精度。在内编队轨道高度为300km、内卫星干扰力为1.0×10-10m/s2、外卫星定轨精度为3cm、内外卫星相对状态测量精度为1mm的条件下,计算得到内编队测量重力场的有效阶数为72,相应的大地水准面累积误差为44cm,重力异常累积误差为4.5mGal,由此可知内编队测量重力场的有效阶数主要分布在低阶部分。     

基于联合相似测度的SAR图像边缘点特征配准方法

针对SAR图像配准过程中几何变换影响特征匹配稳健性和适应性的问题,提出了一种在特征匹配过程中直接解算几何变换模型的边缘点特征配准方法。利用SAR图像边缘点的梯度和方向特征,基于像素迁移思想,定义了图像匹配的联合相似度——联合特征均方和(SSJF),并建立了SAR图像边缘点集相似性匹配准则;基于方向模板提出了改进的ROEWA算子;利用改进的遗传算法(GA)来进行相似度的全局优化搜索,获取配准模型参数;利用多幅SAR图像的配准试验,对本文方法的性能进行了验证。     

战时装备调配保障决策模型构建研究

分析了战时装备调配保障决策的特点,运用模糊聚类分析法对装备调配保障对象进行了分组和优先级排序,以此为基础,运用目标规划法构建了战时装备调配保障决策模型,最后,通过实例验证了模型的可行性和有效性．     

Experimental and numerical investigation of zirconium jet performance with different liner shapes design

This paper studies the shaped charge jet performance in terms of different liner shapes including conical,bell,hemispherical and bi-conical liners.The critical angles and the relevant flow velocities for the zir-conium liner material were calculated analytically and numerically using Autodyn hydro-code.The relationship between the critical collapse angle and the flow velocity was determined for the conditions of jet formation and coherency.Penetration tests according to the standard testing procedures of API-RP34 (Section-Ⅱ) were performed to validate the numerical predictions of the jet performance of the studied liners.It was found that the four shaped charge liners all produced coherent jets with different performances.The penetration depth of the shaped charges with the bell and the bi-conical liner shapes increased by 10.3％ and 22％,respectively,while the crater diameter of shaped charge with hemispherical liner increased by 85％ representing the formation of an explosively-formed-projectile (EFP),when they are compared with the corresponding jet characteristics of a conical liner shaped charge.     

A general approach to the shape of failure rate and MRL functions

Failure rate and mean residual life are two important characteristics for studying reliability of products. In literature, some work studied the shape of failure rate function based on the knowledge of the associated probability density function; some other work investigated the shape of mean residual life function based on the shape of the associated failure rate function separately for continuous case and discrete case. In this article, a general approach is developed which can be applied to the aforementioned studies. © 2004 Wiley Periodicals, Inc. Naval Research Logistics, 2004     

一种新型内曲线式径向柱塞泵的设计

讨论了各种液压泵的使用特点,提出了一种新型内曲线式径向柱塞泵的设计思路.通过合理设计泵内定子内曲线表面,在理论上实现了无流量脉动;为了提高柱塞泵的使用寿命,采取了降低定子导轨压力角的措施;通过Matlab实现了定子表面曲线和压力角的仿真计算;理论分析的结果对于设计和制造低噪声的柱塞式液压泵有一定的指导意义.     

陆军诸兵种合同作战兰切斯特方程的弹药消耗预测研究

描述了诸兵种合同作战的兰切斯特方程及其矩阵解,提出了一种通过兵力损耗换算弹药损耗的新思路,分析和确定了用该方法预测弹药消耗的相关参数,最后运用Matlab进行仿真计算,预测出了武器装备战损情况和弹药消耗情况。     

利用样条插值法计算摩擦离合器瞬时转速曲线

研究了履带车辆主离合器瞬时转速测试方法,在数据处理过程中两次运用样条插值算法,较好地解决主、被部分实测转速精度低及转速数据长度不一致的问题,得到较为理想的瞬时转速曲线。