油井清、防蜡技术研究现状

主要介绍了目前常用的机械清防蜡、热力清防蜡、表面能防蜡 (内衬和涂料油管 )、化学剂清防蜡、超声波清防蜡、强磁清防蜡和微生物清防蜡技术等。生产实践中 ,应根据油井的含水、含蜡量选用合适的清防蜡技术 ,才能对清防蜡达到经济、满意的效果。

原子力显微镜研究蛋白质晶体生长机理及进展

原子力显微镜(AFM)这种能进行微尺度测量的精密仪器是目前研究晶体生长机理最为有效的方法之一,在晶体生长机理研究中起到了重要的作用,尤其是对于蛋白质晶体生长的研究显得更为突出。分别简明地阐述了利用AFM进行蛋白质晶体生长研究的工作原理,以及在这方面已经取得的研究成果,包括二维台阶生长、螺旋位错生长、法向生长、三维成核生长、台阶发展的不对称性、及杜仲抗真菌蛋白(EAFP)和天花粉蛋白(TCS)晶体生长的新进展。论述了利用空间微重力环境进行蛋白质晶体生长及空间蛋白质晶体生长的科研和应用,指出今后进行蛋白质晶体生长研究的趋势和前景。

用非结构网格研究旋转振荡圆柱绕流

研究了雷诺数Re=200,1000,线速度比α=0.5,2.0,4.0,强迫振荡频率fs=0.1～2.0情况下的旋转振荡圆柱绕流问题.通过基于非结构同位网格有限体积法对Navier-Stokes方程进行数值求解.对流项、扩散项和非恒定项的离散格式均具有二阶精度,利用SIMPLE算法处理压力-速度耦合.计算得到了作用力系数随不同控制参数的变化规律.通过对升力系数的频谱分析得到自然脱落频率和强迫振荡频率下的作用力振幅.通过对不同频率作用力幅值的分析,得到频率之间的竞争关系,进而定量地给出了不同尾迹涡脱落模式的分区图.

非转移弧层流等离子体射流铸铁表面熔凝强化

用大气压非转移弧层流等离子体射流,对W-Mo-Cu铸铁表面进行熔凝相变强化处理,观察和测试了试样经不同弧电流处理后的表面层组织、硬度、耐磨性.结果表明,层流等离子体射流对铸铁表面的局部快速加热熔化和冷却凝固,明显改变了表面层的微观组织,提高了硬度和抗磨损性能.

高温化学非平衡计算中源项处理方法

高超声速三维化学非平衡绕流流场的数值模拟中,在计算初期容易发生组元密度出现负值的非物理现象,另外源项的刚性是影响计算稳定性和收敛速度的主要原因.根据源项线性化理论,采用2种源项线性化方法处理化学反应源项.一种为根据流场内化学反应物理规律构造的线性化方法,该方法能抑制在计算过程中组元密度出现负值现象,提高了计算稳定性,加速了收敛速度.同时采用了时间预处理矩阵的线性化方法,较好地解决了非平衡化学反应与流场耦合的刚性问题.证明了所构造源项线性化方法相容性.数值实验表明该方法有效地避免了源项计算中密度出负的问题,加快了计算的收敛速度,从而提高了计算效率.

不同层显式格式及在微尺度热传导中的应用

　基于指数拟合和牛顿插值多项式构造了用于数值计算偏微分方程的不同层显式格式,应用不同层显式格式可获得不同精度的数值计算结果,并将该算法应用于微结构热传导方程和薄膜强瞬态热传导方程中.

非平整、多孔介质海底上波浪传播的复合方程

为了反映近岸区域实际存在的多孔介质海底效应,并且考虑到波浪在刚性海底上传播模型的最新研究进展,运用Green第二恒等式建立了波浪在非平整、多孔介质海底上传播的复合方程.假设水深和多孔介质海底层厚度均由两种分量组成:慢变分量,其水平变化的长度尺度大于表面波的波长;快变分量,其水平变化的长度尺度与表面波的波长等阶,但其振幅小于表面波的振幅.另外,多孔介质层下部边界的快变分量比水深的快变分量小1个量级.针对水体层和多孔介质层,选择Green第二恒等式方法给出了波浪传播和渗透的复合方程,它在交接面上满足压力和垂直渗透速度的连续性条件,可充分考虑波数变化的一般连续性,并包含了某些著名的扩展型缓坡方程.

Starting Nozzle Flow Simulation Using K-G Two-Equation Turbulence Model

The starting process of two-dimensional nozzle flows has been simulated with Euler, laminar and k - g two-equation turbulence Navier-Stokes equations. The flow solver is based on a combination of LUSGS subiteration implicit method and five spatial discretized schemes, which are Roe, HLLE, MHLLE upwind schemes and AUSM+, AUSMPW schemes. In the paper, special attention is for the flow differences of the nozzle starting process obtained from different governing equations and different schemes. Two nozzle flows, previously investigated experimentally and numerically by other researchers, are chosen as our examples. The calculated results indicate the carbuncle phenomenon and unphysical oscillations appear more or less near a wall or behind strong shock wave except using HLLE scheme, and these unphysical phenomena become more seriously with the increase of Mach number. Comparing the turbulence calculation, inviscid solution cannot simulate the wall flow separation and the laminar solution shows some different flow characteristics in the regions of flow separation and near wall.

Statistical Simulation of Thin-Film Bearings

The information preservation (IP) method and the direct simulation Monte Carlo (DSMC) method are used to simulate the gas flows between the write/read head and the platter of the disk drive (the slider bearing problem). The results of both methods are in good agreement with numerical solution of the Reynolds equation in the cases studied. However, the DSMC method owing to the problem of large sample size demand and the difficulty in regulating boundary conditions at the inlet and outlet was able to simulate only short bearings, while IP simulates the bearing of authentic length ~1000 m ? and can provide more detailed flow information.

Measurement of Electron Density Profile Behind Strong Shock Waves with a Langmuir Probe

At the shock velocity range of 7~9km/s, the variations of electron density behind strong normal shock waves are measured in a low-density shock tube by using the Langmuir electrostatic probe technique. The electron temperature, calculated based on Park’s three-temperature model, is used in interpreting the probe current data. The peak electron densities determined in the present experiment are shown to be in a good agreement with those predicted by Lin’s calculation. The experimentally obtained ratios of the characteristic ionization distance to the mean free path of freestream ahead of the shock wave are found to be in a good agreement with the existing experiments and Park’s calculation.

Substrate Strain and Proliferation & Differentiation of Bone Marrow Mesenchymal Stem Cells

New methods of surface modification of transparent silicone substrate were developed, and a new set of cell culture devices that provide homogeneous substrate strain was designed. Using the new device, effects of cyclic substrate strain on bone marrow mesenchymal stem cells(MSCs) were studied. It was found that cyclic strain influenced proliferation and differentiation of bone marrow MSCs in different ways.

不同重力条件下不相溶流体层间界面波演化规律的数值模拟研究

报道了关于不相溶流体层间界面波演化规律的数值模拟研究及结果，重点考察了重力条件对界面波演化特性的影响。考虑在深度方向无限扩展的互不相容的两个流体层，上层流体比下层的轻，但比下层的运动速度快；两层流体间的界面上存在正弦波形的初始扰动，并随流体流动而不断变化。本文采用Level Set方法来实现对运动的相界面的追踪，用有限差分法来离散控制方程组。为了提高数值算法的稳定性，采用三阶的Runge-Kutta法来离散时间导数，而采用五阶的WENO（Weighted Essentially Non-oscillatory）格式来离散一阶对流输运项，并用压力修正投影法（Pressure Correction Projection Method）来实现离散控制方程组的求解。为了提高对复杂非稳态过程的解的准确度，采用了嵌套的三层迭代循环。本文对一系列工况条件下的界面波演化过程进行了计算；除了研究重力的作用之外，还考察了流体密度、粘性、表面张力、初始界面波频率、振幅及波数对界面波演化特性的影响。其中，上下流体层的最大密度比和粘性比可达3000/1，而重力加速度在0~5g0（g0=9.8m/s^2）之间变化，上下流体层间的最大速度差为8m/s。研究结果表明，随着重力、流体密度比、流体粘性比及表面张力的增加，界面波的演化受到不同程度的抑制，而界面波的传播速度也与重力及流体的密度、粘性和表面张力等因素相关。

过冷池沸腾传热研究：I、地面常重力实验

针对我国返回式卫星搭载实验条件，我们研制了一套池沸腾实验装置初样（包括液池、壁温自动反馈控制系统等）和地面实验配套系统，以研究地面常重力和空间微重力条件下的过冷池沸腾传热规律，着重研究核态沸腾、临界热流密度和双模态过度沸腾等。本文采用恒流电源加热、恒压电源加热和壁温自动反馈控制等三种加热方式，实验研究了地面常重力环境中池沸腾现象及其传热规律。实验结果证明该装置能满足空间搭载实验的要求，实验结果具有良好的重复性。关于稳定双模态过渡沸腾，本文研究发现，在过冷条件下起其表现和文献报道的饱和条件时具有明显的差异，沸腾特征曲线具有一明显的极小值，其位置紧邻临界热负荷点。本文还对此进行了初步的理论探讨。

Numerical Simulation of R-M Instability

In order to capture shock waves and contact discontinuities in the field and easy to program with parallel computation a new algorithm is developed to solve the N-S equations for simulation of R-M instability problems. The method with group velocity control is used to suppress numerical oscillations, and an adaptive non-uniform mesh is used to get fine resolution. Numerical results for cylindrical shock-cylindrical interface interaction with a shock Mach number Ms=1.2 and Atwood number A=0.818, 0.961, 0.980 (the interior density of the interface/outer density p(1)/p(2) = 10, 50, 100, respectively), and for the planar shock-spherical interface interaction with Ms=1.2 and p(1)/p(2) = 14.28are presented. The effect of Atwood number and multi-mode initial perturbation on the R-M instability are studied. Multi-collisions of the reflected shock with the interface is a main reason of nonlinear development of the interface instability and formation of the spike-bubble structures In simulation with double mode perturbation vortex merging and second instability are found. After second instability the small vortex structures near the interface produced. It is important factor for turbulent mixing.