超声速二元机翼随机混沌运动分析

以考虑随机扰动的超声速二元机翼为研究对象,采用Kapitaniak方法对超声速二元机翼的随机混沌特性进行研究。采用三阶活塞理论推导超声速二元机翼的非线性气动力和气动力矩,建立考虑随机扰动、具有俯仰立方非线性的机翼2自由度运动微分方程,并将其写成4维状态方程的形式;采用中心流形方法对系统进行降维,将系统状态方程从4维降为2维;再联合利用累积量截断法、非高斯截断法获得系统的二维联合概率密度函数及系统的概率时差图,采用Kapitaniak方法分析系统在不同扰动强度下的随机混沌特性;采用系统响应、庞加莱截面图及最大Lyapunov指数等对系统的随机混沌特性进行验证。本研究对超声速二元机翼在复杂环境下的稳定性、安全性及响应特性等研究具有重要的促进作用。     

军队会计流程存在的问题及优化策略

在新军事变革的背景下,军队会计流程存在不适应新管理体制需要、信息技术应用对会计流程再造力度不够、军队会计科目设置影响流程等问题。本文从界定军队会计流程的含义入手,提出了优化军队会计流程、建立智能化军队会计信息系统的四项策略,即重塑军队会计流程体系、重构军队会计信息系统、调整军队会计科目体系以及完善各流程会计处理方法。优化军队会计流程、建设智能化军队会计信息系统,不仅能够反映军事经济活动的历史信息,还能为不同类型的信息使用者提供预测、决策等支持,并有利于改善军队会计核算质量,准确反映各类资产负债的价值信息和单位的真实财务状况,对于提高军队会计信息质量具有一定的借鉴意义。     

Optimization of buckling load for laminated composite plates using adaptive Kriging-improved PSO: A novel hybrid intelligent method

An effective hybrid optimization method is proposed by integrating an adaptive Kriging (A-Kriging) into an improved partial swarm optimization algorithm (IPSO) to give a so-called A-Kriging-IPSO for maxi-mizing the buckling load of laminated composite plates (LCPs) under uniaxial and biaxial compressions. In this method, a novel iterative adaptive Kriging model, which is structured using two training sample sets as active and adaptive points, is utilized to directly predict the buckling load of the LCPs and to improve the efficiency of the optimization process. The active points are selected from the initial data set while the adaptive points are generated using the radial random-based convex samples. The cell-based smoothed discrete shear gap method (CS-DSG3) is employed to analyze the buckling behavior of the LCPs to provide the response of adaptive and input data sets. The buckling load of the LCPs is maximized by utilizing the IPSO algorithm. To demonstrate the efficiency and accuracy of the proposed methodology, the LCPs with different layers (2, 3, 4, and 10 layers), boundary conditions, aspect ratios and load patterns (biaxial and uniaxial loads) are investigated. The results obtained by proposed method are in good agreement with the literature results, but with less computational burden. By applying adaptive radial Kriging model, the accurate optimal results-based predictions of the buckling load are obtained for the studied LCPs.     

A novel launch dynamics measurement system for multiple launch rocket system and comparative analysis with numerical simulations

In this paper,a novel launch dynamics measurement system based on the photoelectric sensor pair is built.The actual muzzle time(i.e.a time duration that originates from the initial movement to the rocket's departure from the muzzle)and the muzzle velocity are measured.Compared with the classical methods,the actual muzzle time is obtained by eliminating the ignition delay.The comparative analysis method is proposed with numerical simulations established by the transfer matrix method for multibody systems.The experiment results indicate that the proposed measurement system can effectively measure the actual muzzle time and reduce the error of classical methods,which match well with the simulation results showing the launch dynamics model is reliable and helpful for further analysis and design of the MLRS.     

间接边界元法模拟含裂纹介质中弹性波的传播

介绍了间接边界元法的基本理论,利用二维弹性动力边界积分方程解决了地震波在含裂纹介质中的散射问题。编写了地震波在二维非均匀介质中传播的数值模拟程序,模拟了爆炸点源在含裂纹介质中的传播情况,分析了裂纹的分布及填充物对波传播的影响。结果表明,边界元法是研究含裂纹介质中弹性波传播的有效工具。     

改进AgCl浊度法测定舰船火灾烟气中氯

为快速、准确地测定出现场舰船火灾烟气中氯的含量,在体系中加入适量的十二烷基苯磺酸钠(DBS)、聚乙烯醇溶液(PVA)和吐温-80,对传统AgCl浊度法进行了改进。结果表明,系统的稳定性、灵敏度均大幅度提高,检测限则由3.5×10-1mg/l降低至3.1×10-2mg/l。改进后的方法线性范围宽、重现性好。     

一种关于~pc(0≤c<1)的快精算法

求pc(p>1,正整数)的值时,若c较小,通常会存在收敛速度较慢以及数值字长有限所致精度变差的问题。提出了一种关于pc(0≤c<1)的快精算法,该方法按照定点二进制数特点,通过适当扩大c值,利用牛顿迭代法求取近似值,在采用选值法确定初值时,将对应值域分为若干等间隔子区间,初值精度取决于间隔h的大小,而h的大小则根据迭代精度和预定迭代次数确定,由此可获得高精度初值,从而在理论上使pc的迭代计算达到快速、高精度的目的。     

基于调制/解调的动态响应测试方法

在磁悬浮列车中,悬浮控制系统要求间隙传感器的动态特性,但无法用机械方法测试较高频率时的动态特性。根据传感器工作机制,用模拟涡流场来代替被测导体的涡流效应,提出基于调制/解调原理的动态特性测试方法,并分别对正弦信号和方波信号的测试方法进行了探讨。最后给出了两种特征信号的传感器动态特性测试结果。实验表明,这种方法能够满足测试要求,相对于机械方法有很大的优越性。     

大椭圆轨道航天器编队飞行相对运动分析

大椭圆轨道航天器在较长轨道周期内运行于远地点上空,因而该轨道多应用于卫星通信、天体观测、空间磁场探测等。上述空间任务所需的多航天器协同运动理论亟待解决。利用运动学方法推导了大椭圆轨道编队的相对运动模型,简要证明了实现长期近距离编队的必要条件,分析了相对轨道根数对线性化模型精度及其动力学特性的影响。仿真结果表明,相对运动模型在轨道远地点处精度较高,适当选择相对轨道根数可设计出满足任务要求的编队轨道。     

一娄非线性抛物方程组解的爆破现象新证明

利用能量方法给出了一类非线性抛物方程组解的有限时刻爆破现象的新证明,此方法将初值的条件从正的初值减弱到某些非负的情形。