含新型间断探测器的混合WCNS格式在间断无粘可压流的应用

为了让高精度数值格式在含间断和小尺度涡等复杂结构的超声速无粘可压缩流动情况下,仍能鲁棒地捕捉激波并快速得到流场高保真的模拟结果,研究了以子模板导数组合为基础的光滑度量算法,构造了精度与鲁棒性兼顾的新型间断探测器,使间断识别对小尺度涡也具有高分辨率;研究了混合加权紧致非线性格式(weighted compact nonlinear scheme, WCNS)方法,对流场中的光滑与间断区域分别使用线性与非线性加权格式求解,从而克服单一非线性格式在光滑区分辨率难以达到设计精度的问题。数值实验表明,使用新型间断探测器的混合WCNS格式对一维、二维Euler方程模拟结果良好,并且相比于在全流场使用局部特征分解的原始WCNS方法有计算效率的提高。     

液氧甲烷膨胀循环变推力发动机系统方案对比研究

当前对液氧甲烷膨胀循环变推力火箭发动机的研制难点和关键技术认识不够清楚,尤其是在大变比推力调节方案方面。基于整个发动机系统,采用理论计算方法,探讨甲烷膨胀做功能力以及变推力调节方案可行性。分别给出了单涡轮系统方案和双涡轮系统方案,首次给出了不同工况下详细的系统状态参数分布,进行了对比分析,并探讨了甲烷做功能力随室压的变化规律。研究结果表明,甲烷做功能力随着室压的减小呈现先减小后增大的趋势,单涡轮和双涡轮系统方案均能够实现大范围推力调节;相比单涡轮方案,双涡轮方案能够更好地保证混合比,且甲烷气体做功能力利用效率更高,氧涡轮和燃料涡轮功率变化范围较窄,涡轮所处环境较为缓和,因此双涡轮系统方案具备一定优势。     

A novel non-separation opening scheme of front cover for rocket launch canister

In view of that existing opening technologies of front cover for rocket launch canister have disadvantages such as causing damage on the ground equipment, not being reused and easily broken. A novel reusable non-separation spring-driven opening scheme is proposed to achieve rapid and reliable opening of the front cover. The mathematical model of the opening process of the front cover is established by the rigid body dynamics theory. To establish a response surface model to optimize the opening scheme, three main influencing factors of the opening process are obtained through the designed experiments, including the pre-compression, the stiffness of the thrust spring, and the thrust spring force arm length. In addition, the prescribed kinematic law was taken as constraint, and the smaller thrust spring preliminary pressure and angular velocity was taken as optimization expectations. The results show that the opening scheme meets the design requirements on opening process well. It also shows that the optimized scheme can reduce the kinetic energy of the front cover, and the impact on the canister effectively, achieving a reliable and rapid opening of the front cover.     

五阶HWCNS在低速复杂流场中的应用

采用五阶精度显式混合加权紧致非线性格式求解雷诺平均NS方程;利用多块对接结构网格技术,对30P-30N多段翼型进行网格收敛性研究。在不考虑转捩的情况下,采用SA一方程湍流模型研究混合加权紧致非线性格式与二阶精度MUSCL格式对该翼型压力分布和典型站位速度型的影响,并与实验结果进行对比分析。采用混合加权紧致非线性格式和SA一方程湍流模型模拟梯形翼高升力构型低速复杂流场,通过对总体气动特性和压力分布的分析,探讨五阶精度显式混合加权紧致非线性格式在低速复杂外形流动中的应用能力。结果表明,对30P-30N三段翼型,采用全湍流模拟方法可以得到较好的压力分布;对梯形翼高升力构型,在附着流和边界层小分离情况下混合加权紧致非线性格式有较好的模拟能力。     

给定极小样本量的定量截尾序贯检验法及其应用

对现有截尾序贯检验法作了必要的改进,提出定量截尾序贯检验法。结合导弹命中精度验收试验的工程实际需求,在事先给定几种特小样本量的前提下,针对定量截尾序贯检验法的实际应用展开研究,给出了可应用于实际的检验方案。通过对检验实例的比较分析,说明了方案的优越性。     

基于秘密共享的军队指挥信息系统安全存储方案

在信息对抗条件下,军队指挥信息系统是敌对双方信息作战的焦点,因此数据安全是军队指挥信息系统高效、可靠工作的基础和保障.根据军队指挥信息系统的特点,给出一种基于秘密共享的数据安全存储方案,实现了数据库的可生存性、可用性及关键数据的机密性、完整性,能有效抵御以合法身份进行的恶意攻击,提高了军队指挥信息系统数据的安全性.并给出了该方案的安全性分析.     

Two-agent scheduling with linear resource-dependent processing times

This paper considers a two-agent scheduling problem with linear resource-dependent processing times, in which each agent has a set of jobs that compete with that of the other agent for the use of a common processing machine, and each agent aims to minimize the weighted number of its tardy jobs. To meet the due date requirements of the jobs of the two agents, additional amounts of a common resource, which may be in discrete or continuous quantities, can be allocated to the processing of the jobs to compress their processing durations. The actual processing time of a job is a linear function of the amount of the resource allocated to it. The objective is to determine the optimal job sequence and resource allocation strategy so as to minimize the weighted number of tardy jobs of one agent, while keeping the weighted number of tardy jobs of the other agent, and the total resource consumption cost within their respective predetermined limits. It is shown that the problem is -hard in the ordinary sense, and there does not exist a polynomial-time approximation algorithm with performance ratio unless ; however it admits a relaxed fully polynomial time approximation scheme. A proximal bundle algorithm based on Lagrangian relaxation is also presented to solve the problem approximately. To speed up convergence and produce sharp bounds, enhancement strategies including the design of a Tabu search algorithm and integration of a Lagrangian recovery heuristic into the algorithm are devised. Extensive numerical studies are conducted to assess the effectiveness and efficiency of the proposed algorithms.     

基于提升的双自适应小波变换算法研究

小波变换的传统提升算法的滤波器固定，不能随输入信号的变化而改变，针对该问题，结合现有的自适应算法，提出一种双自适应小波变换算法，并对该算法的更新和预测过程进行了自适应调整。实验证明，该算法比传统的提升算法和单纯的自适应更新或自适应预测算法具有更优越的性能。     

AUSMPW+格式在高超声速热化学非平衡流数值模拟中的应用

将AUSMPW+格式应用到高超声速热化学非平衡流场的数值模拟中。为提高精度,采用了三阶MUSCL插值方法。与LU SGS方法结合,提高了单步计算效率和收敛性。采用热化学非平衡十一组元气体模型求解了非定常轴对称Navier Stokes方程组,得到了收敛结果。数值模拟结果与文献结果进行了对比,并在弹道靶中进行了钢质圆球的实验验证。计算结果与文献、实验的对比说明,AUSMPW+格式可以在热化学非平衡流的数值模拟中精确地捕捉到强弓形激波,得到准确的空气动力系数。