竞争失效产品恒应力加速寿命试验优化新方法

对加速寿命试验设计优化的相关知识进行研究分析,确定以竞争失效产品恒应力加速寿命试验为应用背景。在对加速寿命试验统计分析深入研究的基础上,通过分析方案要素、约束条件等建立优化目标函数,提出基于模拟退火算法的优化方法和具体实现思路。最后通过实例验证方法的可行性和实用性。     

扁平潜器前进与倒航稳定性评估

基于现有条件和针对扁平潜器的特点,由拖曳水池模型试验确定了攻角、漂角水动力,用经验方法近似估算了旋转水动力.用所得到的线性水动力系数,按照线性稳定性理论方法评估了扁平潜器正航和倒航下水平面、垂直面内的运动稳定性.将正航下水平面、垂直面内的运动稳定性计算结果与资料中类似的扁平潜器进行了比对分析,结果表明两者具有相同的稳定性特征,即垂直面内具有运动稳定性,而水平面内不具有航向稳定性.最后采用主推进器PD控制方法,用非线性运动模型数值仿真计算了主推进器控制作用下扁平潜器的运动.仿真计算结果表明,除了水平面倒航运动外,垂直面正航与倒航、水平面正航运动都可以通过主推进器的控制实现扁平潜器的运动控制.仿真计算结果还表明,在相同的PD控制参数下,航速愈低倒航对深度响应时间愈长.     

实验条件对纳米多孔二氧化硅薄膜性能的影响

以正硅酸乙酯(TEOS)为先驱体,采用酸/碱两步溶胶—凝胶法,结合旋转涂胶和超临界干燥等工艺在硅片上制备了SiO2薄膜。XRD和AFM表明该SiO2薄膜为无定形态,具有多孔网络结构,表面均匀、平整,其SiO2粒子和孔隙的直径为30～40nm。利用椭偏仪测量了薄膜的厚度和折射率,薄膜的厚度为300～1100nm,折射率为1.13～1.23,孔隙率为50%～70%,介电常数为1.9～2.4。SiO2薄膜的厚度随溶剂异丙醇(IPA)用量的减少、催化剂NH4OH用量的增加、SiO2溶胶粘度的增大和旋转涂胶速度的降低而增大;介电常数随NH4OH用量和SiO2溶胶粘度的增加而降低,IPA用量和旋转速度对SiO2薄膜的介电常数影响较小。     

中日历史与利益的博弈

日本想淡忘历史责任却又不断挑起历史问题,在利益方面对中国步步紧逼,以求对内对外博取最大的利益。中国必须以历史为支点,利用利益杠杆来调节中日关系。     

从《孙子兵法》管理思想看密切官兵关系的重要性

《孙子兵法》作为兵学圣典,对当前部队的日常管理具有重要的指导作用。从《孙子兵法》对自古以来官兵紧张关系的具体描述,剖析当前官兵关系紧张的成因,探讨科学解决官兵紧张关系的方法。     

中国共产党的三个历史阶段与马克思主义中国化的两次飞跃

中国共产党建党以来的90年,大致可分为三个阶段：1921—1949年,1949—1978年,1978年至今。党带领人民先后完成了三件大事：建立了社会主义新中国,进行了社会主义改造,开辟了中国特色社会主义的道路。第一个阶段,实现了马克思主义中国第第一次飞跃,形成了毛泽东思想;第二个阶段,既是马克思主义中国化第一次飞跃的延伸,又为第二次飞跃做了准备;第三个阶段,实现了马克思主义中国第二次飞跃,形成了中国特色社会主义理论体系。     

基于混沌特征的高分辨雷达目标识别

根据高分辨导弹制导雷达的基本工作原则和舰船目标的散射特性,利用现有雷达回波的仿真技术,在合理的战术想定下,计算了三类典型舰船的雷达回波.在此基础上,研究了利用雷达回波功率谱的方法来识别目标类型的有效性,并基于混沌理论提出了一种比功率谱方法更加有效的新的识别方法,从而为进一步利用混沌理论来开发雷达目标识别技术奠定了初步的理论基础.     

新型钢-混凝土组合板的力学性能研究

以加劲肋形式、组合板厚度和栓钉布置为参数,进行了9块新型组合板的力学性能试验.试验结果表明,组合板的正截面承载力可按基于修正平截面假定的极限状态计算;组合板的跨中挠度,可在按现行规范计算的基础上,加上考虑界面滑移影响的附加变形值予以修正.     

Aircraft routing under the risk of detection

The deterministic problem for finding an aircraft's optimal risk trajectory in a threat environment has been formulated. The threat is associated with the risk of aircraft detection by radars or similar sensors. The model considers an aircraft's trajectory in three‐dimensional (3‐D) space and represents the aircraft by a symmetrical ellipsoid with the axis of symmetry directing the trajectory. Analytical and discrete optimization approaches for routing an aircraft with variable radar cross‐section (RCS) subject to a constraint on the trajectory length have been developed. Through techniques of Calculus of Variations, the analytical approach reduces the original risk optimization problem to a vectorial nonlinear differential equation. In the case of a single detecting installation, a solution to this equation is expressed by a quadrature. A network optimization approach reduces the original problem to the Constrained Shortest Path Problem (CSPP) for a 3‐D network. The CSPP has been solved for various ellipsoid shapes and different length constraints in cases with several radars. The impact of ellipsoid shape on the geometry of an optimal trajectory as well as the impact of variable RCS on the performance of a network optimization algorithm have been analyzed and illustrated by several numerical examples. © 2006 Wiley Periodicals, Inc. Naval Research Logistics, 2006     

Effect of projectile parameters on opening behavior of PELE penetrating RC target

When a penetrator with enhanced lateral effect (PELE) impacts on a reinforced concrete (RC) target, the target is damaged with a large opening. An understanding of how PELE projectile parameters affect the opening dimension, is essential for effective design of the PELE projectile. In this study, under the condition that the impact velocity and target parameters (strength and thickness) were fixed values, the important influence factors of the PELE (jacket wall thickness B, jacket material strength Y1, filling material strength Y2 and angle of monolithic jacketθ) were determined by a dimensional analysis. Tests and simulations of the PELE penetrating the RC target were conducted to analyze the influence of these factors on opening diameter ((D), an equivalent diameter under relative kinetic energy). Based on the test and simulation results, it is found that the influence of these factors B, Y1 andθon the deformation mode of the jacket shows a similar trend:as values of the three factors decrease, the jacket deforms from small bending deformation to large one, and then to curling deformation. This causes the opening diameter to first increase with the decrease of these three factors, and then decreases. It is well known that the bending resistance of the jacket is related to these factors B, Y1 andθ. Therefore, a plastic limit bending moment (M0) of the jacket was quoted to characterize the influence of these factors on the bending deformation of the jacket and the opening diameter of the target. The influence factor Y2 causes (D) to first increase with the increase of Y2, and then decreases. A formula was developed to predict the opening diameter, whose influence parameters were considered in a dimensionless way. It has been shown that the dimensionless opening diameter (D)/d1 is dependent on two dimensionless parameters Q = (d31fc/M0) and G = (fc/Y2), where d1 and fc are the outer diameter of the projectile and the compressive strength of the target, respectively.