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.     

有约束的Hartley域自适应算法的应用研究

通过对有约束的Hartley域自适应算法、频域自适应算法及时域自适应算法用于自适应降噪系统的计算机仿真研究 ,认为在自适应通信降噪中采用基于Hartley变换的自适应算法较频域自适应算法及时域自适应算法性能更优、降噪效果更好 ,并在高速信号处理器TMS32 0C30上开发实现了该算法 .实验结果表明 ,将Hartley域自适应算法应用于通信降噪系统 ,方法实际可行     

全垫升式气垫船水压场数值模拟

提出了任意分布的气垫压力所产生的水压场的计算方法 ,对椭圆域上均匀分布的气垫压力产生的水压场进行了数值模拟 ,并将计算结果与实验进行了比较 .结果表明 ,用数值模拟的方法研究全垫升式气垫船水压场是可行的     

雷达对抗情报处理数据仓库辅助决策系统构建

本文提出了雷达对抗情报处理数据仓库系统的概念,设计了系统的技术体系结构,并结合现有雷达对抗情报处理子系统,具体规划了面向决策分析的雷达对抗情报处理数据仓库模型,研究了其实现方法。     

浅谈在营区规划中对营区文化的塑造

当前在军队工程建设中,对营区规划的主导思想已形成基本一致的认识,但多从物质技术层面去理解,就营区规划单位而言,尚没有广泛认识到营区文化也是规划中的重要内容以及在营区现代化建设中起着不可替代的作用。本文针对此情况重点论述了营区文化的主要内容和重要作用,并提倡通过对营区空间形态的创造来塑造有特色的营区文化,最终创造出一个充满凝聚力的,有利于长期发展的营区环境。     

超音速外流与塞式喷管形成的干扰流场数值模拟

从考虑了k ε湍流模型和双组分气体模型的三维薄层近似NS方程出发 ,采用高效ENO差分格式 ,数值模拟了超音速空气外流与塞式喷管燃气形成的内外流干扰流场。部分计算结果与国外文献相比一致。在此基础上论证了应用计算流体力学开展塞式喷管研究的可行性。     

浅谈发挥军旅格言的战斗文化功能

论述了如何充分发挥军旅格言的战斗文化功能，营造崇尚战斗、敢于战斗、争当战斗英雄的浓厚战斗文化氖围，努力把武警部队建设成为军心凝聚、士气高昂、英勇顽强的文明之师、威武之师，更好地履行党和人民“忠诚卫士”的神圣使命。     

Interdiction models for delaying adversarial attacks against critical information technology infrastructure

Information technology (IT) infrastructure relies on a globalized supply chain that is vulnerable to numerous risks from adversarial attacks. It is important to protect IT infrastructure from these dynamic, persistent risks by delaying adversarial exploits. In this paper, we propose max‐min interdiction models for critical infrastructure protection that prioritizes cost‐effective security mitigations to maximally delay adversarial attacks. We consider attacks originating from multiple adversaries, each of which aims to find a “critical path” through the attack surface to complete the corresponding attack as soon as possible. Decision‐makers can deploy mitigations to delay attack exploits, however, mitigation effectiveness is sometimes uncertain. We propose a stochastic model variant to address this uncertainty by incorporating random delay times. The proposed models can be reformulated as a nested max‐max problem using dualization. We propose a Lagrangian heuristic approach that decomposes the max‐max problem into a number of smaller subproblems, and updates upper and lower bounds to the original problem via subgradient optimization. We evaluate the perfect information solution value as an alternative method for updating the upper bound. Computational results demonstrate that the Lagrangian heuristic identifies near‐optimal solutions efficiently, which outperforms a general purpose mixed‐integer programming solver on medium and large instances.     

激波诱导异质气体界面失稳的数值模拟

基于二维N-S方程,利用有限差分数值离散方法,对激波诱导异质气体界面失稳的现象进行了数值模拟,与文献中实验结果和计算结果进行了定性比较,并进一步分析了整个流动的非定常动态变化特性和非线性特征.研究表明,本文数值模拟的非定常流场图谱与文献中的实验结果和数值结果吻合较好;数值结果捕捉到了六氟化硫界面的演变过程及流场中复杂的波系结构.