微小尺度下氢气预混燃烧的实验研究

对内径为1.66mm的不锈钢管燃烧室的氢气预混燃烧实验进行了描述，采用 红外测温仪测量了燃烧室壁面的温度场分布，获得了不同燃烧热功率下的运行界限．在突扩 段内高温回流区的作用下，在带有5mm长突扩段的燃烧室内可以实现完全预混燃 烧，最高运行界限可达1.415．由于较高的进气速度和较大的燃烧室壁面散热，在不带突扩 段的不锈钢管内无法实现完全预混燃烧．结果表明突扩段对微小尺度燃烧具有稳定火焰、拓 宽燃烧运行界限的作用．通过对火焰形状和结构的观察，结合突扩段燃烧流场的分析，合理 解释了燃烧室壁面温度场随过量空气系数的变化规律．     

Some qualitative properties of incompressible hyperelastic spherical membranes under dynamic loads

Some nonlinear dynamic properties of axisymmetric deformation are ex- amined for a spherical membrane composed of a transversely isotropic incompressible Rivlin-Saunders material. The membrane is subjected to periodic step loads at its inner and outer surfaces. A second-order nonlinear ordinary differential equation approximately describing radially symmetric motion of the membrane is obtained by setting the thick- ness of the spherical structure close to one. The qualitative properties of the solutions are discussed in detail. In particular, the conditions that control the nonlinear periodic oscillation of the spherical membrane are proposed. In certain cases, it is proved that the oscillating form of the spherical membrane would present a homoclinic orbit of type ＂∞＂, and the amplitude growth of the periodic oscillation is discontinuous. Numerical results are provided.     

步进摩擦分析测试平台的研制

研制了步进摩擦分析测试平台,可用于检测人体在静止及运动路面上的步进摩擦特性.该平台主要由六自由度摇摆台、三维测力台和数据采集系统三部分构成,六自由度摇摆台可提供六个自由度的任意组合运动,用来模拟舰船、海浪和地震等工况;三维测力台可测量出人体在行走时的三维力和力矩;数据采集系统将六自由度运动平台和三维测力台的输出数据采集并保存到计算机中,用来分析人体运动时的步进摩擦特性.采用研制平台进行了一组试验,结果表明:人在上、下坡行走时的垂直地面反作用力与在水平路面行走时的垂直地面反作用力具有不同的分布规律,并且垂直地面反作用力均随坡度角的增大而减小.     

阶梯圆形和环形薄板的大幅度基本振动

利用修正迭代法求出了具有多个阶梯厚度圆形和环形薄板轴对称大幅度自由振动的一种新的解析解，导出了振幅和非线性振动基频的解析关系式，给出了较完善的数值计算结果，所得结果可供工程设计时参考。     

明渠中跌坎后突扩分离流数值研究

利用大涡模拟技术，对明渠中跌坎后的二维突扩分离流结构进行了数值模拟，探讨了这类典型分离流各特征区的流动性质，分析了再附区壁面上不同测点处脉动压力的统计特征，并与试验结果进行了比较．在数值模拟中，采用了弱压缩流的控制方程和非均匀网格系统．     

无条件稳定的更新精细积分方法

提出将Pade逼近与精细积分方法中的指数矩阵运算技巧结合起来,建立了精细积分法的更新形式及计算过程,对该更新精细积分方法的稳定性进行了论证与探讨.结果表明,该更新精细积分方法是无条件稳定的,整个积分方法的精度取决于所取Pade逼近的阶数与高斯积分点的数量.数值例题也显示了该方法的高效率及其可行性.     

A stabilized finite element predictor–corrector scheme for the incompressible Navier–Stokes equations using a nodal‐based implementation

A finite element model to solve the incompressible Navier–Stokes equations based on the stabilization with orthogonal subscales, a predictor–corrector scheme to segregate the pressure and a nodal based implementation is presented in this paper. The stabilization consists of adding a least‐squares form of the component orthogonal to the finite element space of the convective and pressure gradient terms, which allows to deal with convection‐dominated flows and to use equal velocity–pressure interpolation. The pressure segregation is inspired in fractional step schemes, although the converged solution corresponds to that of a monolithic time integration. Finally, the nodal‐based implementation is based on an a priori calculation of the integrals appearing in the formulation and then the construction of the matrix and right‐hand side vector of the final algebraic system to be solved. After appropriate approximations, this matrix and this vector can be constructed directly for each nodal point, without the need to loop over the elements and thus making the calculations much faster. Some issues related to this implementation for fractional step and our predictor–corrector scheme, which is the main contribution of this paper, are discussed. Copyright © 2004 John Wiley & Sons, Ltd.     

星载合成孔径雷达数据压缩

星载遥微波成像雷达的观测区域广阔，图像分辨清度高。所以，星载遥感微波成像雷达具有数据率高、数据量大的特点。这就对遥感数据的传输和存储提出了较高的要求。本文提出采取数据压缩方法，在不降低测绘带宽和测绘精度条件下，降低遥感雷达数据率和数据量，从而降低对数据链和星上数据存储设备的要求。本文还对遥感雷达原始数据压缩和遥感雷达图像数据压缩优缺点进行了比较，提出了采用遥感原始数据压缩的建议。最后，对遥感雷达原     

两步退火对SIMOX结构形成的影响

本文通过卢瑟夫沟道背散射(RBS/Channeling)及透射电子显微镜(TEM)研究了SIMOX结构的低、高温两步退火形成。实验结果表明:通过两步退火可以获得顶部硅层中无氧沉淀缺陷的、硅与二氧化硅界面较为突变的SIMOX结构。本文也讨论了在两步退火期间,SIMOX结构形成的物理过程。