基于信息系统的作战指挥效能“嵌入式”评估策略

在分析基于信息系统的作战指挥效能评估特点的基础上,提出了"嵌入式"作战指挥效能评估策略;按照指挥实体、指挥活动、指挥效果3个层次,梳理了指挥主体效能、指挥信息系统效能、指挥活动效能和指挥对象任务效能4个方面的评估内容框架;根据评估活动与作战指挥活动"一体化"原理,设计了作战指挥效能评估在各个作战阶段的活动流程,并进一步提出了作战指挥效能评估工具"功能性嵌入"作战指挥信息系统的方法。     

Influence of propagation direction on operation performance of rotating detonation combustor with turbine guide vane

Due to the pressure gain combustion characteristics, the rotating detonation combustor (RDC) can enhance thermodynamic cycle efficiency. Therefore, the performance of gas-turbine engine can be further improved with this combustion technology. In the present study, the RDC operation performance with a turbine guide vane (TGV) is experimentally investigated. Hydrogen and air are used as propellants while hydrogen and air mass flow rate are about 16.1 g/s and 500 g/s and the equivalence ratio is about 1.0. A pre-detonator is used to ignite the mixture. High-frequency dynamic pressure transducers and silicon pressure sensors are employed to measure pressure oscillations and static pressure in the combustion chamber. The experimental results show that the steady propagation of rotating detonation wave (RDW) is observed in the combustion chamber and the mean propagation velocity is above 1650 m/s, reaching over 84% of theoretical Chapman-Jouguet detonation velocity. Clockwise and counterclockwise propagation directions of RDW are obtained. For clockwise propagation direction, the static pressure is about 15% higher in the combustor compared with counterclockwise propagation direction, but the RDW dominant frequency is lower. When the oblique shock wave propagates across the TGV, the pressure oscillations reduces significantly. In addition, as the detonation products flow through the TGV, the static pressure drops up to 32% and 43% for clockwise and counterclockwise propagation process respectively.     

Experimental investigation on enhanced damage to fuel tanks by reactive projectiles impact

Enhanced damage to the full-filled fuel tank,impacted by the cold pressed and sintered PTFE/AL/W reactive material projectile(RMP)with a density of 7.8 g/cm3,is investigated experimentally and theoretically.The fuel tank is a rectangular structure,welded by six pieces of 2024 aluminum plate with a thickness of 6 mm,and filled with RP-3 aviation kerosene.Experimental results show that the kerosene is ignited by the RMP impact at a velocity above 1062 m/s,and a novel interior ignition phenomenon which is closely related to the rupture effect of the fuel tank is observed.However,the traditional steel projectile with the same mass and dimension requires a velocity up to 1649 m/s to ignite the kerosene.Based on the experimental results,the radial pressure field is considered to be the main reason for the shear failure of weld.For mechanism considerations,the chemical energy released by the RMP enhances the hydrodynamic ram(HRAM)effect and provides additional ignition sources inside the fuel tank,thereby enhancing both rupture and ignition effects.Moreover,to further understand the enhanced ignition effect of RMP,the reactive debris temperature inside the kerosene is analyzed theoretically.The initiated reactive debris with high temperature provides effective interior ignition sources to ignite the kerosene,resulting in the enhanced ignition of the kerosene.     

试验鉴定中的装备适用性概念辨析

针对试验鉴定领域的装备适用性概念不统一和存在学术分歧的现象,以及相应指标体系偏于混乱和缺乏规范的问题,开展装备适用性概念辨析.通过检索文献并梳理其中与装备适用性相关的各种称谓,以及分析其对应概念的理解情况,对装备适用性概念进行了文献综述;通过辨识分析为什么要考察装备适用性、装备适用性因何而产生等问题,构建了装备适用性概念的描述框架,并阐述了该框架是开放的、边界清晰的.