NUMERICAL SIMULATION OF FLOW PATTERNS IN PLANAR JETS

INTRODUCTIONTurbulent jet flow is the most widely usedflow type in engineering applications especiallyfor combustion engines which provide most ener-gy sources for industrial production and trans-portation,and a large proportion of energy trans-portation and conversion processes is dominatedby transient evolution of large- scale structures,or so called coherent structures,in turbulentjets.As the flow control and optimization pro-cesses are closely related to the understanding ofdetailed in…     

箭状矩阵的广义特征值反问题

讨论实对称箭状矩阵（除对角元及最后一行、最后一列元素外，其余位置元素全为零）的广义特征值反问题，它可以用来描述星形弹簧质量系统的振动问题，即给出系统的振动频率如何来确定质点的质量或弹簧的刚度。通过对箭状矩阵特征多项式性质的研究，运用部分分式理论，证明了给定正定箭状矩阵B，实数{λi}i=1^n,{μi}i=1^n-1，满足λ1＜μ1＜…＜μn-1＜λn，存在箭状矩阵A，使广义特征值问题Ax-λBx有解{λi}i=1^n，而广义特征值问题A(n-1)x=λB(n-1)x有解{μi}i=1^n-1，其中A（n-1),B(n-1)分别表示A，B的n-1级主子矩阵。     

激波对血液成分影响的实验研究

用自行研制的无膜激波管，研究在一定强度激波的作用下，激波对血液成分的影响。分析了激波与血液作用时的波系结构，得到了作用在血液上的透射激波速度和透射波波后压力的表达式。共对24组新鲜血液进行了对照实验，实验后的医学化验表明：激波对血液有相当强的作用，其中尤为明显的是作用后的血液中游离血红蛋白明显增多、血小板数减少。结果还表明这些变化跟激波作用的次数有一定的关系。文中对造成血液破坏的机制也作了初步的分析。     

实双对称矩阵的特征值问题及其反问题的降阶法

本文将实双对称矩阵的特征值问题化为阶数减半的实对称矩阵的特征值问题。并利用这个结果来求解斜对称Jacobi矩阵的特征值反问题,即构造一个斜对称Jacobi矩阵A,使之具有预先指定的特征值{λ_i}_(i=1)~n或预先指定的特征对(λ_1,x_1)和(λ_2,x_2)。     

磁悬挂天平系统的磁场分析与计算(60mm×60mm 磁悬挂天平技术研究之一)

磁悬挂天平系统的磁场设计好坏是磁悬挂天平系统结构设计成败的关键。而磁悬挂天平系统的磁场结构比较复杂,用简单的磁路设计方法已经不能满足更高的设计要求。本文介绍了一种求解电磁场的方法——二维电磁场有限元法,建立了相应的磁悬挂天平系统的数学模型,并应用此法,对磁悬挂天平的均匀磁场和梯度磁场分布进行了分析计算;提出了一种用于求解磁场开域问题的方法。文章中还介绍了根据磁场的计算结果来确定线圈间间距和铁芯厚度的方法。在此基础上,提出了一个60mm×60mm 的磁悬挂天平系统的设计方案,并给出了此设计方案的理论计算与实验结果的对比表。     

一种用于目标特征提取的改进RELAX算法

传统RELAX算法是基于sinc核函数进行处理的，该算法在正弦信号参数估计上具有良好的鲁棒性和有效性。在远场成像条件下，逆合成孔径雷达（ISAR）目标回波可近似为复正弦模型，因而可以采用RELAX算法进行目标特征提取。当对ISAR实测数据进行处理时，复杂目标中强散射中心的高旁瓣电平和噪声的共同影响，造成特征提取中对散射中心的个数估计不准确，影响了特征提取精度。针对这一问题对RELAX算法进行了改进，提出采用加窗处理技术，对RELAX处理的核函数进行修正。数值仿真和对ISAR实测数据的处理结果表明，改进的RELAX算法改善了旁瓣性能，提高了散射中心提取精度。     

Thermocapillary motion of droplets at large Marangoni numbers

In this paper, the thermocapillary motion problem of drops is investigated using the axisymmetric model. The front-tracking method is employed to capture the drop interface. We find that the migration velocity of the drop is greatly influenced by the temperature field in the drop when Ma is fairly large (>100), which leads to an increase–decrease migration velocity at the beginning of our simulations.     

Effect of Electromagnetic Stirring on the Quality of K417 Superalloy Ingots

The effect of electromagnetic stirring on the inner quality of K417 superalloy ingots is studied with EPMA and optical microscope.The results show that while an electromagnetic stirring with 50Hz frequency and 80A current is imposed,the equiax crystals of K417 superalloy ingots can be effectively refined and increased,and the central shrinkage porosity and the dendritic segregation of K417 superalloy ingots are greatly reduced,so the inner quality of K417 superalloy ingots is obviously improved.     

Numerical and experimental investigation into hypersonic boundary layer transition induced by roughness elements

In this work, the Direct Numerical Simulation(DNS) and Oil-Film Interferometry(OFI)technique are used to investigate the hypersonic boundary layer transition induced by single and double roughness elements at Mach number 5. For single roughness, the DNS results showed that both horseshoe vortices and hairpin vortices caused by shear layer instability can affect the boundary layer instability. The generation of the near-wall unstable structure is the key point of boundary layer transition behind the roughness element. At the downstream of the roughness element, the interaction between horseshoe vortices and hairpin vortices will spread in the spanwise direction.For double roughness elements, the effect of the spacing between roughness elements on the transition is studied. It is found that the case of higher spacing between roughness elements is more effective for inducing transition than the lower one. The interaction between two adjacent roughness elements can suppress the evolution of horseshoe vortices in the downstream and trigger the instability of shear layer. Thus, the transition will be suppressed accordingly.     

基于神经网络的仿真转台控制系统

在转台存在偏载、摩擦等不确定负载干扰的情况下,用神经网络与PID(Proportional-Integral-Differential)控制相结合的方法,设计了适应负载变化的转台控制系统.分析了基于BP(Back Propagation)神经网络的自适应PID控制器的基本原理,建立了转台位置控制系统的数学模型,并对控制系统进行仿真分析和实验验证,通过与传统PID控制的对比实验与仿真表明:所设计系统由于有自学习能力,能动态调整PID参数,使系统表现出良好的抗干扰能力和跟踪性能,证明了所设计系统的有效性.该算法结构简单,PID初始参数调整方便,易于在转台实时控制系统中应用.