Simulation of the plasticizing behavior of composite modified double-base (CMDB) propellant in grooved calendar based on adaptive grid technology

The frequent occurrence of safety accidents during the calendering process is caused by the flammable and explosive properties of composite modified double-base (CMDB) propellant. Optimization of process parameters with the aid of fluid simulation technology could effectively ensure the safety of the calendering process. To improve the accuracy of the simulation results, material parameters and model structure were corrected based on actual conditions, and adaptive grid technology was applied in the local mesh refinement. In addition, the rheological behavior, motion trajectories and heat transfer mechanisms of CMDB propellant slurry were studied with different gaps, rotational rates and temperatures of two rollers. The results indicated that the refined mesh could significantly improve the contour clarity of boundaries and simulate the characteristics of CMDB propellant slurry reflux movement caused by the convergent flow near the outlet. Compared with the gap, the increased rotational rate of roller could promote the reflux movement and intensify the shear flow of slurry inside the flow region by viscous shear dragging. Meanwhile, under the synergistic effect of contact heat transfer as well as convective heat exchange, heat accumulated near the outlet and diffused along the reflux movement, which led to the countercurrent heat dissipation behavior of CMDB propellant slurry. The plasticizing mechanism of slurry and the safety of calendering under different conditions were explored, which provided theoretical guidance and reference data for the optimization of calendering process conditions. Based on the simulation results, the safety of the CMDB propellant calendering process could be significantly improved with a few tests conducted during a short research and development cycle.     

非线性控制在磁悬浮系统中的应用

用滑模变结构控制原理设计磁悬浮系统非线性控制器，并在磁悬浮球装置上进行了试验，结果证实这种控制器具有完全的鲁棒性、良好的参数适应性，设计方法也有广泛的适用性。悬浮系统的刚度有显著的提高。     

基于FrFT的差分跳频通信LFM干扰抑制算法

针对差分跳频通信系统抗LFM干扰能力不足的问题,利用差分跳频信号和LFM干扰信号调频斜率参数的不同,通过估计采样信号中LFM干扰信号的调频斜率K和旋转阶次α参数,结合分段、参数估计和均值处理提高估计精度,进一步在采样信号的分数阶时频域二维参数平面(α,μ)中利用LFM干扰信号频带外的平面均值替代LFM信号成分,实现对差分跳频通信中LFM干扰信号的抑制。仿真结果表明,该算法可有效抑制差分跳频信号中LFM干扰信号,提高信噪比约11 d B。     

基于指挥信息系统的作战指挥特点

基于指挥信息系统的作战指挥是一种新的作战指挥方式,给指挥员作战指挥提出挑战,只有深刻认识基于信息系统作战指挥的特点,才能发挥出最大作战效能。文章从六个方面对基于指挥信息系统作战指挥的特点进行了阐述,详述了指挥信息系统的作战特点以及应用特点。以为指挥员了解指挥信息系统,基于指挥信息系统开展作战指挥提供理论支撑。     

红外脉冲强光辐射源中电爆丝爆炸机理研究

利用电爆丝的一种红外脉冲强光辐射新技术,从理论和实验上研究了电爆丝的爆炸机理。用电爆丝绝热加热模型数值模拟了电爆丝在冲击大电流作用下的电爆炸特性,电爆丝根数对电爆炸特性的影响。实验结果与理论模拟相一致。     

电磁发射高速旋转弹丸马格努斯效应

和传统火药发射弹丸相比,电磁发射弹丸具有初速高、射程远等优势,但尾部的电枢臂槽会使弹丸部流场不再轴对称,产生独特的气动力特性。基于三维非定常Navier-Stokers方程,采用滑移网格技术,分析电磁发射弹丸的气动力特性。研究表明,对于高速旋转的电磁发射弹丸,马格努斯效应来源于激波层内流场畸变和电枢臂的迎风面积变化的共同作用;电枢臂迎风面积的周期性变化是导致气动力和力矩周期性变化的原因,马格努斯力矩在滚转角45°和135°时分别达到最小值和最大值;电枢臂槽的存在既加剧了马格努斯效应(135°时增加50%以上),又使得压心周期性前移(绝对前移量达5%),并且随着转速的增加,马格努斯力矩增加和压心前移效果越来越显著,不利于弹丸的动稳定。     

关于培养创新人才的几点思考

随着知识经济的发展,以开发和激励学生创新能力,培养创新人才的创新教育已成为一股世界性潮流,其影响力越来越大。把创新教育作为教育教学改革的核心,通过教育教学改革加速创新人才的培养,已迫在眉睫。     

长管水击最大水击压强的解析

从管道水击微分方程的特征分析入手,提出了水击特征方程的黎曼不变量和网格分析解,建立了管道水击问题的近似解析解,给出了长管水击最大水击压强的计算表达式。通过实际算例对解析解和数值解结果进行了比较。对水击微分方程的重力项也进行了讨论。     

A worst‐case formulation for constrained ranking and selection with input uncertainty

In this research, we consider robust simulation optimization with stochastic constraints. In particular, we focus on the ranking and selection problem in which the computing time is sufficient to evaluate all the designs (solutions) under consideration. Given a fixed simulation budget, we aim at maximizing the probability of correct selection (PCS) for the best feasible design, where the objective and constraint measures are assessed by their worst‐case performances. To simplify the complexity of PCS, we develop an approximated probability measure and derive the asymptotic optimality condition (optimality condition as the simulation budget goes to infinity) of the resulting problem. A sequential selection procedure is then designed within the optimal computing budget allocation framework. The high efficiency of the proposed procedure is tested via a number of numerical examples. In addition, we provide some useful insights into the efficiency of a budget allocation procedure.     

CODE新光压模型对北斗混合导航星座精密轨道确定的影响

运用卫星定轨软件工具包NUDTTK,分析了欧洲定轨中心扩展的经验光压模型(EECOM)对北斗二代混合导航星座精密轨道确定的影响。研究表明:对地球静止轨道卫星而言,EECOM能够明显改善定轨精度,相比于传统的ECOM-9和ECOM-5模型,卫星激光测距检核精度分别提高17.4%和35.1%。对倾斜地球同步轨道卫星和中轨道卫星而言,采用ECOM-5模型的定轨精度要优于采用EECOM和ECOM-9模型的,新光压模型EECOM并不能有效改善倾斜地球同步轨道卫星和中轨道卫星的定轨精度。与IGS数据分析中心WHU、GFZ和CODE的轨道产品相互比对的结果显示:目前,国防科技大学北斗精密轨道产品中,地球静止轨道卫星的定轨精度为1~4 m,倾斜地球同步轨道卫星的定轨精度为25~30 cm,中轨道卫星的定轨精度为10~20 cm。