THE EXISTENCE AND UNIQUENESS OF A SIMILARITY SOLUTION ARISING FROM SEPARATION AT A FREE STREAM LINE

1972 ◽  
Vol 23 (1) ◽  
pp. 63-77 ◽  
Author(s):  
J. B. McLEOD
1976 ◽  
Vol 74 (1) ◽  
pp. 143-159 ◽  
Author(s):  
H. G. Hornung

Analytic solutions are obtained for non-equilibrium dissociating flow of an inviscid Lighthill-Freeman gas after a curved shock, by dividing the flow into a thin reacting layer near the shock and a frozen region further downstream. The method of matched asymptotic expansions is used, with the product of shock curvature and reaction length as the small parameter. In particular, the solution gives expressions for the reacting-layer thickness, the frozen dissociation level, effective shock values of the frozen flow and the maximum density on a stream-line as functions of free-stream, gas and shock parameters. Numerical examples are presented and the results are compared with experiments.


1958 ◽  
Vol 54 (3) ◽  
pp. 391-395 ◽  
Author(s):  
J. B. Helliwell

In an earlier paper (Helliwell and Mackie(3)) it was shown that steady two-dimensional flow patterns of a compressible inviscid fluid at high subsonic speed past a finite wedge could be determined quite simply when sonic velocity is attained at the shoulder of the wedge and thereafter the flow breaks away from the shoulder with a free streamline. In a subsequent paper (Helliwell (4)) a similar method of analysis has been applied to determine a flow pattern of the same general type past a finite wedge symmetrically placed in a channel, from which the case of the wedge in the free stream may be deduced as a special case. However, in a general investigation into transonic flow past wedges (Mackie and Pack (5)) it was argued that when the wedge angle or the free stream (subsonic) velocity is too small no supersonic region would develop on the wedge side, and the flow would break away from the wedge shoulder with some higher subsonic velocity, giving a free stream line. The present note examines the flow pattern which develops under these conditions for a wedge symmetrically placed in a channel with parallel walls.


Comparatively little progress in the solution of the problem of discontinuous fluid motion past a curved barrier was made until Levi-Civita formulated a method of transforming that part of the barrier which is in contact with the moving fluid into a semi-circle in an Argand diagram. This, indeed, was the starting point of much work of interest and importance. Useful accounts of the problem of motion past any barrier, together with extensions, are given by Cisotti and Brillouin. Leaving out of account such barriers as are made up of one or more planes, problems which can be solved by the older methods based on Schwartz-Christoffel transformations, the only applications of Levi-Civita’s method to curved barriers seem to be that made by Brillouin in the paper referred to, and those made by S. Brodetsky in 1922. The work of Brillouin. however, and that of other investigators are essentially backward processes, in which a likely expression is written down and the streaming motion implied, as well as the shape of the boundary, are investigated. A more direct attack is obtained by suitably choosing the coefficients in Levi-Civita’s general formula, and arriving at the solution for a given curved barrier by a series of steps in successive approximation. The solution of the problem for a circular barrier placed symmetrically in the streaming fluid has been obtained in this manner by S. Brodetsky. The object of this paper is to solve the problem of the circular barrier placed in any position in the streaming fluid, subject to the condition, however, that neither of the ends of the barrier are in the “dead” fluid— i. e ., the radius of curvature of the free stream line is zero at each end. This immediately restricts the barrier, if convex to the streaming fluid, to be of angular extent less than 110·2°.


1979 ◽  
Vol 46 (4) ◽  
pp. 789-794 ◽  
Author(s):  
L. N. Tao

The problem of freezing or melting of a polymorphous material in a semi-infinite region with arbitrarily prescribed initial and boundary conditions is studied. Exact solutions of the problem are established. The solutions of temperature of all phases are expressed in polynomials and functions in the error integral family and time t and the position of the interfacial boundaries in power series of t1/2. Existence and uniqueness of the series solutions are considered and proved. It is also shown that these series are absolutely and uniformly convergent. The paper concludes with some remarks on density changes at the interfacial boundary and various special cases, one of which is the similarity solution.


1970 ◽  
Vol 68 (2) ◽  
pp. 493-508
Author(s):  
J. Buckmaster

AbstractThe title problem is investigated with the view of clarifying the nature of the separation in an adverse pressure gradient when the suction υ0 is very strong. A linear model is investigated, but it is argued that this must contain many of the essential features of the exact (non-linear) problem. With a free-stream U = 1 − x the similarity solution u = (1 − x)f(y) is appropriate when (υ0x − y) ≫ 1, x = O(1), 1−x = O(1). There is an O(1) layer centred on y = υ0x in which more complex x-dependence first appears and then, when (y − υ0x) ≫ 1, the solution assumes its final asymptotic behaviour. The y = υ0x layer is non-uniform in x and exhibits a marked change in behaviour when (1 − x;) = O(l/υ0). The solution in this narrow rectangle is singular like (1 − x)−2 at the trailing edge. It is these singular terms that induce separation and reversed flow in an exponentially small neighbourhood of the trailing-edge.


1995 ◽  
Vol 294 ◽  
pp. 301-321 ◽  
Author(s):  
Nikolaos A. Pelekasis ◽  
Andreas Acrivos

The steady laminar flow of a well-mixed suspension of monodisperse solid spheres, convected steadily past a horizontal flat plate and sedimenting under the action of gravity, is examined. It is shown that, in the limit as Re → ∞ and ∈ → 0, where Re is the bulk Reynolds number and ∈ is the ratio of the particle radius a to the characteristic length scale L, the analysis for determining the particle concentration profile has several aspects in common with that of obtaining the temperature profile in forced-convection heat transfer from a wall to a fluid stream moving at high Reynolds and Prandtl numbers. Specifically, it is found that the particle concentration remains uniform throughout the O(Re−1/2) thick Blasius boundary layer except for two O(∈2/3) thin regions on either side of the plate, where the concentration profile becomes non-uniform owing to the presence of shear-induced particle diffusion which balances the particle flux due to convection and sedimentation. The system of equations within this concentration boundary layer admits a similarity solution near the leading edge of the plate, according to which the particle concentration along the top surface of the plate increases from its value in the free stream by an amount proportional to X5/6, with X measuring the distance along the plate, and decreases in a similar fashion along the underside. But, unlike the case of gravity settling on an inclined plate in the absence of a bulk flow at infinity considered earlier (Nir & Acrivos 1990), here the concentration profile remains continuous everywhere. For values of X beyond the region near the leading edge, the particle concentration profile is obtained through the numerical solution of the relevant equations. It is found that, as predicted from the similarity solution, there exists a value of X at which the particle concentration along the top side of the plate attains its maximum value ϕm and that, beyond this point, a stagnant sediment layer will form that grows steadily in time. This critical value of X is computed as a function of ϕs, the particle volume fraction in the free stream. In contrast, but again in conformity with the similarity solution, for values of X sufficiently far removed from the leading edge along the underside of the plate, a particle-free region is predicted to form adjacent to the plate. This model, with minor modifications, can be used to describe particle migration in other shear flows, as, for example, in the case of crossflow microfiltration.


1939 ◽  
Vol os-10 (1) ◽  
pp. 283-298 ◽  
Author(s):  
N. SIMMONS
Keyword(s):  

Sign in / Sign up

Export Citation Format

Share Document