爆炸喷涂爆炸波参数数值计算

对爆炸喷涂燃烧室爆轰波的形成及爆轰产物热力学及动力学参数进行了数值计算．结果表明，爆炸喷涂气相爆轰系统爆轰特性主要取决于气相系统的选择和初始混合气体配比．C2H2 O2气相爆轰系统更适合于喷涂高熔点的陶瓷、金属陶瓷及纳米复合陶瓷粉体，其最优化工艺参数应该选择在零氧平衡附近．而H2 O2气相爆轰系统则适用于喷涂低熔点的金属及其合金，金属粉体的熔点越高，最优化参数越接近于零氧平衡点．     

低频弯张换能器指向性数值计算及实验测试

应用亥姆霍兹积分方程与有限元方法，建立了换能器在水中的振动方程，导出了换能器辐射声场指向性公式．实验结果表明，在谐振频率1．16kHz处，换能器水平面上的辐射指向性呈现各向均匀分布的特点，这与理论计算结果一致．     

二阶三点数值微分公式的外推算法

利用Taylor公式，给出了二阶三点数值微分公式在各点的截断误差的渐近展开式，并利用Richardson外推算法，提高二阶三点数值微分公式的收敛阶数，得到高精度的二阶数值微分公式．     

泵站枢纽三维湍流数值模拟研究

采用雷诺平均纳维斯托克斯方程(RANS)和标准κ-ε湍流模型,运用SIMPLEC算法,对无锡市仙蠡桥泵站枢纽6种运行组合工况进行了三维数值模拟,预测了回流区及旋涡发生的位置和形态,计算得出了泵站枢纽流速分布规律以及泵站出水河道与京杭大运河交汇处的最大横向流速,计算结果与水工模型试验结果吻合.该研究不仅为仙蠡桥泵站枢纽优化设计、合理布局提供了理论指导,而且研究方法可应用于其他泵站枢纽水流流态数值模拟.     

复杂外形火箭导弹三维绕流与喷流干扰流场的数值模拟

该文基于雷诺平均三维Navier-Stokees方程及k—ε模型，采用高精度的有限体积TVD格式以及多重网格Runge-Kutta时间推进算法对在超声速有攻角条件下带尾翼／弹翼的弹箭绕流与喷流干扰流场进行了数值模拟。获得了绕流和喷流相互干扰的波系结构，以及弹翼与尾翼、弹翼／尾翼与弹体相互作用的复杂流场，分析其流动现象，揭示了流动规律，为火箭导弹合理的气动布局提供依据。     

Computational fluid dynamics for dense gas-solid fluidized beds

Many computational fluid dynamics (CFD) models for describing the hydrodynamics of dense gas-solid flows in fluidized beds have been put forward in the past few decades. These models treat the solid phase as continuum or discrete particles, which leads to Eulerian-Eulerian or Eulerian-Lagrangian formulations, respectively. Different governing equations and closure relations essentially result from an insufficient understanding of the complex gas?particle and particle?particle interactions for gas?solid flows. The current status of these models is discussed briefly in this paper. All the approaches in the literature modify only the solid phase momentum balance equation introducing various forms of the solid phase stress tensor and the solid phase pressure drop in the Eulerian-Eulerian models. Taking them into consideration, a new model for predicting the fluid behavior of dense gas?solid flows in fluidized beds has been developed, which contains new terms in both the particle and gas phase momentum balance equations and requires only the use of an experimental drag force correlation. Several results are shown to verify the model’s reliability, which include the homogeneous fluidization of Geldart type A particles, the bubbling and jetting fluidization of Geldart type B particles in rectangular beds, and fluid dynamics in a complicated geometry for a bubbling?bed of a fast internally circulating fluidized?bed biomass gasifier.     

数控程序纠错系统

为防止数控系统程序指令出错，给出了一种平台独立的面向对象的数控程序纠错系统，利用这一系统能够帮助编程人员快速准确地编程，从而避免可能发生的加工事故。实践应用表明，该系统方便有效。     

变形双重介质分形油藏渗流流动分析

研究了变形双重介质分形油藏渗流问题的压力不稳定响应 ,考虑了储层的双重介质特征和分形特征以及应力敏感地层中介质的变形问题 ,建立了新的应力敏感地层双重分形介质数学模型 ,包括只有裂缝发生形变和裂缝与岩石同时发生形变时定产量生产的两类数学模型。渗透率依赖于孔隙压力变化的流动方程是强非线性的 ,故采用数值方法求解了这些数学模型。探讨了分形参数、变形参数和双重介质参数变化时压力的变化规律 ,给出了典型的压力曲线图板。这些结果可用于试井分析。     

Compact difference approximation with consistent boundary condition

For simulating multi-scale complex flow fields it should be noted that all the physical quantities we are interested in must be simulated well. With limitation of the computer resources it is preferred to use high order accurate difference schemes. Because of their high accuracy and small stencil of grid points computational fluid dynamics (CFD) workers pay more attention to compact schemes recently. For simulating the complex flow fields the treatment of boundary conditions at the far field boundary points and near far field boundary points is very important. According to authors' experience and published results some aspects of boundary condition treatment for far field boundary are presented, and the emphasis is on treatment of boundary conditions for the upwind compact schemes. The consistent treatment of boundary conditions at the near boundary points is also discussed. At the end of the paper are given some numerical examples. The computed results with presented method are satisfactory.     

空气水两相段塞流的跟踪模拟及试验研究

分析了前人提出的段塞跟踪模拟方法的优缺点 ,根据液塞头部的加速压降和入口液塞长度分布特征对段塞跟踪模型进行了改进。采用面向对象技术 ,实现了水平和倾斜管道段塞流的跟踪模拟 ,并与多相流试验环道的空气水试验数据进行了对比。模拟结果表明 ,当不考虑加速压降时 ,用跟踪模型预测的压降低于实测值 ;当考虑加速压降时 ,用跟踪模型预测的压降高于实测值。在管道上固定位置测出的压力信号符合正态分布 ,管道上某一固定点处液塞头部和尾部的速度分布也符合正态分布。当不考虑气泡尾波作用时 ,液塞长度沿管线增长较慢 ,分布形状无变化 ;但是考虑气泡尾波作用时 ,在入口附近液塞长度平均值增长较快 ,统计分布沿管轴向呈对数正态分布。