Asymptotic model of the development of separations inside a boundary layer under the action of a traveling pressure wave

2014 ◽  
Vol 49 (2) ◽  
pp. 198-207
Author(s):  
V. V. Bogolepov ◽  
V. Ya. Neiland
1997 ◽  
Vol 337 ◽  
pp. 103-128 ◽  
Author(s):  
OLEG S. RYZHOV ◽  
EUGENE D. TERENT'EV

The problem for a thin near-wall region is reduced, within the triple-deck approach, to unsteady three-dimensional nonlinear boundary-layer equations subject to an interaction law. A linear version of the boundary-value problem describes eigenmodes of different nature (including crossflow vortices) coupled together. The frequency ω of the eigenmodes is connected with the components k and m of the wavenumber vector through a dispersion relation. This relation exhibits two singular properties. One of them is of basic importance since it makes the imaginary part Im(ω) of the frequency increase without bound as k and m tend to infnity along some curves in the real (k, m)-plane. The singularity turns out to be strong, rendering the Cauchy problem ill posed for linear equations.Accounting for the second-order approximation in asymptotic expansions for the upper and main decks brings about significant alterations in the interaction law. A new mathematical model leans upon a set of composite equations without rescaling the original independent variables and desired functions. As a result, the right-hand side of a modified dispersion relation involves an additional term multiplied by a small parameter ε=R−1/8, R being the reference Reynolds number. The aforementioned strong singularity is missing from solutions of the modified dispersion relation. Thus, the range of validity of a linear approximation becomes far more extended in ω, k and m, but the incorporation of the higher-order term into the interaction law means in essence that the Reynolds number is retained in the formulation of a key problem for the lower deck.


2014 ◽  
Vol 2014.67 (0) ◽  
pp. _504-1_-_504-2_
Author(s):  
Toshiyuki AOKI ◽  
Nobuaki KONDOH ◽  
Hiromu YAMASAKI ◽  
Takuya OGAWA ◽  
Masaki OGISHIMA

1998 ◽  
Vol 359 ◽  
pp. 1-22 ◽  
Author(s):  
FEDERICO DOMENICHINI ◽  
GIANNI PEDRIZZETTI

The axisymmetric boundary-layer separation of an incompressible impulsively started flow in a wavy-walled tube is analysed at moderate to high values of the Reynolds number. The investigation is carried out by numerical integration of either the Navier–Stokes equations or Prandtl's asymptotic formulation of the boundary-layer problem. The presence of an adverse pressure gradient induces reverse flow at the tube wall independently of the Reynolds number; its occurrence can be predicted by a timescale analysis. Following that, the viscous calculations show different dynamics depending on the Reynolds number. As the Reynolds number increases, the boundary layer has in a well-defined internal structure where longitudinal lengthscales become comparable with the viscous one. Thus the boundary-layer scaling fails locally, with a minimum of pressure inside the boundary layer itself. The formation of the primary recirculation is well captured by the asymptotic model which, however, is not able to describe the roll-up of the vortex structure inside the recirculating region. This inadequacy appears well before the flow evolves to the characteristic terminal singularity usually assumed as foreshadowing the vortex shedding phenomenon. The outcomes are compared with the existing results of analogous problems giving an overall agreement but improving, in some cases, the physical picture.


2015 ◽  
Vol 2015.68 (0) ◽  
pp. 141-142
Author(s):  
Yujiro NAKAO ◽  
Takuya OGAWA ◽  
Masaki OGISHIMA ◽  
Nobuaki KONDOH ◽  
Masayuki ANYOJI ◽  
...  
Keyword(s):  

The steady flow of a viscous fluid moving under a constant pressure gradient in a curved tube with a uniform triangular cross section is investigated. Numerical solutions of the equations of motion have been found for the range 100-12 000 of the Dean number D = Ga 3 √(2a/ L )/ μv , where G is the constant pressure gradient, a is a dimension of the triangle, L the radius of the circle in which the tube is coiled, μ the viscosity and v the coefficient of kinematic viscosity of the fluid. The results for low D have been checked by an independent numerical method in which the stream function is expanded in a series of powers of D following the method of Dean (1928). All the results have been checked for accuracy by varying the grid size used in the numerical computations. The trend of the results as D increases is examined for evidence of the development of a boundary-layer structure as D → ∞. Some indication is found of the formation of a boundary layer of thickness proportional to D –1/3 near the side walls of the tube with an associated inviscid core region in the centre of the tube. In particular, comparison is made with details of an asymptotic model as D → ∞ proposed by Smith (1976). A measure of agreement with the general characteristics of this model is obtained, although there are some discrepancies in the precise details. It is possible that the range of D considered in the present work is not great enough to form any definite conclusions regarding the precise nature of the flow as D → ∞. A feature of the present results which develops for D > 3000 is that the maximum axial velocity in the tube ceases to occur on the axis of symmetry of the cross section. This feature appears to be generally consistent with numerical results obtained by Cheng & Akiyama (1970) and Hocking (unpublished) for a tube of rectangular cross section. The sequence of corner vortices of the type identified by Moffatt (1964) is found to occur in the numerical solutions. A detailed study of the vortices has already been published (Collins & Dennis 1976).


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