自润滑材料工作机理验证与材料再生

在研究含油量低(HDV6)、中(HDV12)、高(HDV20)3种材料的滑动摩擦特性基础上,通过实验验证了自润滑材料工作机理;并发现自润滑材料失去自润滑特性后,通过对其重新浸油,可以使材料的自润滑性能再生.     

PID调节下H桥式逆变器离散建模及分岔现象

为研究PID调节下H桥式逆变器的非线性行为,选取逆变器输入电压为分岔参数,利用频闪映射法推导出PID调节下H桥式逆变器的离散数学模型.使用Matlab编程得到系统输出电流随输入电压变化的动态分岔图,通过数值仿真验证了离散数学模型的正确性.仿真结果表明频闪映射法适用于建立H桥式逆变器的离散数学模型;PID调节下H桥式逆变器存在分岔行为.研究结果可为建立PID调节下H桥式逆变器的离散数学模型提供参考.     

斜体素体视技术在腐蚀图像合成中的应用研究

图像合成是计算机图像处理领域的一个关键课题．该文提出了一种基于科体素体视技术的图像合成算法．该算法对于研究船体腐蚀图像的合成具有十分重要的意义．     

晶体管自差收发机优化设计的数学模型

依据自差收发机灵敏度的计算公式,在满足技术要求所规定的辐射功率和电源噪声传输系数条件下,把自差收发机的灵敏度作为目标函数,对自差收发机的电路参数作为设计变量,对自差收发机进行了优化设计,得出自差机优化设计的数学模型。     

周期扰动下二次系统的混沌与次谐分枝

研究一类二次Hamilton系统在周期扰动下的动力学性质,应用Melnikov方法给出了该系统产生混优与次谐分枝的参数范围。     

引入定向越野训练,提高学员综合素质

将定向越野训练引入军事地形学教学,激发学员的竞争意识与学习兴趣,改变单一的教学方式,将用图训练与体能训练相结合,提高训练的难度与强度,加强了课程的综合性,这一过程无论从理论或实践上,都为全面提高学员的军人综合素质、课程教学质量,深化教学改革打下了基础。     

闭环校射仿真与试验

提出了一种可行的闭环校射火控模型,分析了导致脱靶量产生的诸多因素,并建立了简单可用的数学模型,据此来对脱靶量进行仿真。接着重点描述了如何实现闭环火控,通过仿真和实验,说明了该火控模型的可行性和正确性。     

舰载无源被动定位与卡尔曼滤波

根据舰载无源被动定位的特点,论述了用舰载雷达侦察设备通过测向对敌舰载雷达进行定位时,采用卡尔曼滤波提高被动定位精度及跟踪精度的原理和方法,为导弹进行隐蔽攻击奠定了基础。     

一套实时通信网络系统的设计与实现

阐述了一套可实现实时通信计算机局域网的设计与开发方法,并概述了其技术要点     

Effects of total pressures and equivalence ratios on kerosene/air rotating detonation engines using a paralleling CE/SE method

In this paper, the kerosene/air rotating detonation engines(RDE) are numerically investigated, and the emphasis is laid on the effects of total pressures and equivalence ratios on the operation characteristics of RDE including the initiation, instabilities, and propulsive performance. A hybrid MPI + OpenMP parallel computing model is applied and it is proved to be able to obtain a more effective parallel performance on high performance computing(HPC) systems. A series of cases with the total pressure of 1 MPa, 1.5 MPa, 2 MPa, and the equivalence ratio of 0.9, 1, 1.4 are simulated. On one hand, the total pressure shows a significant impact on the instabilities of rotating detonation waves. The instability phenomenon is observed in cases with low total pressure (1 MPa) and weakened with the increase of the total pressure. The total pressure has a small impact on the detonation wave velocity and the specific impulse. On the other hand, the equivalence ratio shows a negligible influence on the instabilities, while it affects the ignition process and accounts for the detonation velocity deficit. It is more difficult to initiate rotating detonation waves directly in the lean fuel operation condition. Little difference was observed in the thrust with different equivalence ratios of 0.9, 1, and 1.4. The highest specific impulse was obtained in the lean fuel cases, which is around 2700 s. The findings could provide insights into the understanding of the operation characteristics of kerosene/air RDE.