半无穷长圆管内的低雷诺数入口流

1969年Lew及Fung[1]计算了圆管内的低雷诸数入口流.1982年Dagan等人[2]得到了有限长圆柱形孔道内蠕动流的级数解.[1]中所得的数值解实质上代表有限长圆管内的低雷诺数入口流,因为一般解中的富氏积分已用富氏级数代替.本文直接计算富氏积分,更精确地求出了真正的半无穷长圆管内Stokes入口流的速度分布,压力分布以及流函数,与此对应的入口段长度为圆管半径的1.2倍,接近于Lew及Fung得到的结果1.3倍.此外,本文还研究了配置法的收敛性,证明了此法在入口流问题中具有很好的收敛性,因此可以在其他类似的问题中采用.     

蠕动流中圆球阻力系数的入口效应

本文研究了圆球在半无穷长圆管入口处的蠕动流。得到了速度分布,压力分布和流函数的无穷级数形式的分析解.采用配置法将无穷级数截断并确定出级数中各项系数.求出了均匀入口流绕静止圆球以及圆球以瞬时速度在管内静止流体中运动这两种情形下圆球的阻力系数以及圆球表面上的应力分布.结果表明,当圆球在入口处运动时会遭受到较无穷圆管内为大的阻力.本文还对配置法的收敛性进行了数值实验.试验证明,该法具有好的收敛性.     

半无限长圆管内Stokes流的入口流

本文研究了半无限长圆管内Stokes流的入口流问题.我们导出了一种新的级数解,它与文献[1,2]的解有一个明显的区别就是该解中不包含无穷积分,因此有利于计算.本文利用配点法进行了计算,得到了满意的结果.     

半无穷向量最优化问题的最优性条件

半无穷向量最优化问题的最优性条件李泽民（重庆建筑大学，６３００４５）１９９０年８月２７日收到．１９９３年３月１日收到修改、压缩稿．无穷维空间中的向量极值问题已引起了不少学者的兴趣［２－４］．本文研究半无穷向量极值问题的最优性条件，得出了一系列有意义的...     

半无穷区间二阶半正积分边值问题的多解性

通过构造一个特殊锥,结合平移变换的方法得到了一类半无穷区间半正积分边值问题至少存在三个正解的充分条件,并举例阐述了主要结果.     

关于无穷级半纯函数的填充圆

本文应用Ａｈｌｆｏｒｓ覆盖曲面理论，在一定条件下证明了无穷级半纯函数强性填充圆的存在性，从而部分地解决了李国平提出的一个猜想。     

二维半无穷管道上Darcy流体方程解的空间渐近性质

本文考虑多孔介质中Darcy流体方程在二维半无穷管道上的空间渐近性质.运用能量分析的办法和微分不等式技术,得到了一个关于“能量函数”的微分不等式,再解此微分不等式建立了解的Phragmén-Lindel?f型二择一结果.最后,在衰减的情形下我们得到了全能量的上界.另外,本文对解的增长率/衰减率做了探讨.     

温度相关双扩散模型在半无穷柱体上的结构稳定性

该文研究了定义在一个半无穷柱体上的温度相关双扩散模型的简化形式.利用先验估计和加权能量分析法,证明了当边界条件满足一定的约束条件时模型的解随空间变量指数式衰减.利用解的先验界和衰减性结果,得到了解对相互作用系数的结构稳定性.     

半无穷区间上具有共振的序列分数阶微分方程积分边值问题的可解性

本文研究半无穷区间上具有共振的分数阶微分方程积分边值问题.通过构造适当的Banach空间及算子,利用迭合度理论和Mawhin连续性定理获得上述边值问题解的存在性结论,推广了前人的结果.     

关于无穷级代数体函数Borel方向的定理

本文研究了无穷级代数体函数Borel方向的判定问题.利用代数体函数的一个基本不等式,获得了一个关于无穷级代数体函数Borel方向的判定定理,将李国平关于无穷级半纯函数的聚值线判定定理推广到了无穷级代数体函数.     

On the hydrodynamic interaction of two circular cylinders oscillating in a viscous fluid

The present paper deals with the plane flow fields induced by two parallel circular cylinders with radiia andb oscillating in a direction which is i) parallel or ii) perpendicular to the plane containing their axes. The effect of the cylinders' hydrodynamic interaction on steady streaming has been studied analytically at high frequency by the method of matched asymptotic expansions.It is found that ifa=b the steady streaming is directed symmetrically to the cylinders while whenab (in the case i)) the secondary steady flow is directed towards the larger cylinder and one of the outer steady vortices disappears.It is shown in case i) that the drag force acting on each cylinder is smaller than the same force experienced on a single cylinder with the same radius which is placed in an unbounded oscillating flow. When the cylinder radii are equal, the drag is greater on the forward cylinder than on the rear one.In contrast, in case ii), wherea=b, it is shown that the drag on each of the two cylinders is greater than the drag acting on a single cylinder with the same radius placed in an unbounded oscillating stream and also each of the cylinders experiences a repulsive force in a direction perpendicular to the oscillating flow.     

Computation of added mass and damping coefficients due to a heaving cylinder

We present the boundary value problem (BVP) for the heave motion due to a vertical circular cylinder in water of finite depth. The BVP is presented in terms of velocity potential function. The velocity potential is obtained by considering two regions, namely, interior region and exterior region. The solutions for these two regions are obtained by the method of separation of variables. The analytical expressions for the hydrodynamic coefficients are derived. Computational results are presented for various depth to radius and draft to radius ratios.     

Mechanics of transition in an axisymmetric laminar boundary layer on a circular cylinder

Measurements of the growth of artificially generated turbulent spots and intermittency distribution in the transition region on a circular cylinder in axial flow show that the instability Reynolds number of 11,000 has a marked effect on the properties. In particular, it is found that the spot production in the initial region when a single turbulent spot has not yet wrapped around the cylinder and the propagation is essentially two-dimensional, is significantly altered. But the transition in the downstream or latter region, where most of the turbulent spots propagate onedimensionally (like the turbulent plugs in a pipe), is not affected. When the radius Reynolds number is more than 11,000, the intermittency law in the initial region is essentially the same as in twodimensional flow on a flat plate and in the latter region it is the one-dimensional flow in a pipe, the demarcation between the two regions being quite sharp.     

Potential flow past a porous body with a core of different permeability

It is well known that a uniform flow past a non-permeable rigid body does not exert a total force upon the surface of the body, however this is not the case when the body is permeable. Power et. al. (1984, 1986) first solved the problem of uniform potential flow past a two-dimensional permeable circular cylinder, with constant permeability, and found that the exterior flow exerts a drag force upon the surface of the cylinder independent of its size and secondly the problem when the uniform potential flow past a porous sphere, with constant permeability, in this case the exterior flow exerts a drag force on the sphere which is linearly dependent on the radius of the sphere. Here we will present the solution of two problems, a uniform potential flow past a porous circular cylinder and past a porous sphere, for each case the porous body is composed of two materials with different permeabilities. In both cases the total force exerted by the exterior flow upon the body is dependent on the thickness of the porous materials, and in the limit when the two permeabilities are equal, the previous results, circular cylinder and sphere, with constant permeability, are recovered. Atlhough, the mathematics involved in the solution of the present problem is simple, due to the nice boundary geometry of the bodies, the final expression for the total force found in each case is quite interesting on the way it depends on the permeability relation, in particular, in the limiting cases of a porous body with solid or hollow core.     

Triple-deck analysis of formation of supersonic and local separation regions in transonic steady flow over a roughness element on the surface of a body of revolution

Transonic axisymmetric flow over a body of rotation with a small roughness element located on its surface is considered. The body is manly cylindrical. The roughness height is assumed to be much smaller than the radius of the cylinder and such that a triple-deck flow is induced in its neighborhood. The goal of the work is to study the effect of the cylinder radius and the roughness shape on the triple-deck flow when the cylinder radius is of the same order as the transverse size of the triple-deck interaction region. In this case, the effect of three-dimensionality of the flow is exhibited even in the first approximation. Special attention is given to the structure of supersonic regions and closing shock waves arising in the outer potential region, as well as to local separation regions if they develop in the lower viscous boundary sublayer. Specifically, it is shown that, as the radius of the cylinder increases at a fixed roughness height, the shock intensity grows considerably, whereas the position of the main shock varies little.     

Two-dimensional viscous flow between circular cylinders: application to damping devices for seismic isolation

A detailed analysis of the fluid dynamics of the two-dimensional viscous flow between circular cylinders is dealt with in this paper. Analytic solutions are found on the basis of asymptotic expansions with respect to a small parameter defined by the ratio between the difference of the radii and the radius of the internal cylinder. The analysis is related to the study of recently developed devices for seismic isolation of buildings based on modified pile foundation, separated from the soil, in which a viscous fluid is inserted in the void space between the pile and the lining of the surrounding soil. The availability of this analytical solution contributes to obtaining accurate predictions of the force on the pile.     

Scattering of Plane Elastic Waves on a Small Obstacle Inside a Layer

The problem on the diffraction of a plane elastic wave with horizontal polarization (SH wave) on a small obstacle placed in a layer is investigated. The layer is situated on a half-space with stress-free boundary. The obstacle is assumed to be a circular cylinder with radius small in comparison with the length of the incident wave. The polarization of the incident wave is parallel to the axis of the cylinder. It is proved that the small inhomogeneity radiates as a linear source such that the intensity of the radiation is proportional to the area of the cross-section of the obstacle and the jump of the squared transverse velocities in the layer and in the obstacle. Bibliography: 5 titles.     

Viscoelastic flow in a curved channel: A similarity solution for the Oldroyd-B fluid

A similarity solution is used to analyse the flow of the Oldroyd fluid B, which includes the Newtonian and Maxwell fluids, in a curved channel modelled by the narrow annular region between two circular concentric cylinders of large radius. The solution is exact, including inertial forces. It is found that the non-Netonian kinematics are very similar to the Newtonian ones, although some stress components can become very large. At high Reynolds number a boundary layer is developed at the inner cylinder. The structure of this boundary layer is asymptotically analysed for the Newtonian fluid. Non-Newtonian stress boundary layers are also developed at the inner cylinder at large Reynolds numbers.     

Interacting indentors on a poroelastic half-space

This paper examines the interaction between two rigid circular indentors on a poroelastic half-space. The resulting mixed boundary value problem, when formulated in the Laplace transform domain, yields an infinite set of Fredholm integral equations. These integral equations are then solved for some special cases. Numerical results for the case of a single indentor show a good agreement with those obtained by using Heinrich and Desoyer's assumption. For the case in which the radius of one indentor reduces to zero (interaction between a rigid indentor and an externally placed load), the resulting equations are solved by a semi-inverse method to give analytical solutions for the resultant force and moment required to maintain the indentor with no normal displacement. When the indentor is subjected to an axial load but allowed to undergo an additional settlement and tilt, numerical results are presented to demonstrate the manner in which Poisson's ratio and the drainage boundary conditions influence the consolidation of the half-space. Numerical results are also given to illustrate the interaction between two identical indentors when ratio of the radius to the spatial distance between them is small.