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STOKES FLOW

(Redirected from Creeping flow)
'Stokes flow' (named after George Gabriel Stokes) is a type of fluid flow where inertial forces are small compared with viscous forces. The Reynolds number is low, i.e. extit{Re} ll 1. This is a typical situation in flows where the fluid velocities are very slow, the viscosities are very large, or the length-scales of the flow are very small, such as in MEMS devices or in the flow of viscous polymers.

Contents
Stokes equations
Properties
Methods of solution
Certain problems, such as the evolution of the shape of a bubble in a Stokes flow, are conducive to numerical solution by the Boundary Element method. This technique can be applied in both 2- and 3-dimensional flows.
See also
References

Stokes equations


For this type of flow, the inertial forces are assumed to be negligible and the Navier-Stokes equations simplify to give the Stokes equations:
:oldsymbol{
abla} cdot mathbb{P} + oldsymbol{f} = 0
where mathbb{P} is the comoving stress tensor, and oldsymbol{f} an applied body force. There is also an equation for conservation of mass. In the common case of an incompressible Newtonian fluid, the Stokes equations are:
:oldsymbol{
abla}p = mu
abla^2 oldsymbol{u} + oldsymbol{f}
:oldsymbol{
abla}cdotoldsymbol{u}=0
Properties

The Stokes Equations represent a considerable simplification of the full Navier-Stokes Equations, especially in the incompressible Newtonian case. In this case, the equations are:
; Instantaneity
:A Stokes flow has no dependence on time other than through time-dependent boundary conditions. This means that, given the boundary conditions of a Stokes flow, the flow can be found without knowledge of the flow at any other time.
; Time-reversibility
:An immediate consequence of instantaneity, time-reversibility means then a time-reversed Stokes flow solves the same equations as the original Stokes flow. This property can sometimes be used (in conjunction with linearity and symmetry in the boundary conditions) to derive results about a flow without solving it fully.
While these properties are true for incompressible Newtonian Stokes flows, the non-linear and sometimes time-dependent nature of Non-Newtonian fluids means that they do not hold in the more general case.
Methods of solution

By streamfunction


It can be shown that in 2-D, the streamfunction for an incompressible Newtonian Stokes flow satisfies the Biharmonic Equation
abla^4 psi = 0.
In the 3-D axisymmetric case, the streamfunction Psi solves the equation E^2 Psi = 0, where E = {partial^2 over partial r^2} + {sin{ heta} over r^2} {partial over partial heta} { 1 over sin{ heta}} {partial over partial heta}.

By Papkovich-Neuber solution


The Papkovich-Neuber Solution represents the velocity and pressure fields of an incompressible Newtonian Stokes flow in terms of two harmonic potentials.

By Boundary element method

Certain problems, such as the evolution of the shape of a bubble in a Stokes flow, are conducive to numerical solution by the Boundary Element method. This technique can be applied in both 2- and 3-dimensional flows.
By Green's function


The linearity of the Stokes equations in the case of an incompressible Newtonian fluid means that a Green's function for the equations can be found. The solution for the pressure p and velocity oldsymbol{u} due to a point force oldsymbol{F}delta(oldsymbol{x}) acting at the origin with |oldsymbol{u}|,p o 0 as |oldsymbol{x}| oinfty is given by
:oldsymbol{u}(oldsymbol{x}) = oldsymbol{F} cdot mathbb{J}(oldsymbol{x})
:p(oldsymbol{x}) = rac{oldsymbol{F}cdotoldsymbol{x}}{4 pi |oldsymbol{x}|^3}
where
:mathbb{J}(oldsymbol{x}) = {1 over 8 pi mu} left( rac{mathbb{I}}{|oldsymbol{x}|} + rac{oldsymbol{x}oldsymbol{x}}{|oldsymbol{x}|^3}
ight).
is a second-rank tensor known as the Oseen Tensor (after Carl Wilhelm Oseen).
The solution for a distributed force density oldsymbol{f}(oldsymbol{x}) (again with decay at infinity) can then be constructed by superposition:
:oldsymbol{u}(oldsymbol{x}) = int oldsymbol{f}(oldsymbol{y}) cdot mathbb{J}(oldsymbol{x} - oldsymbol{y}) , mathrm{d}^3!y
:p(oldsymbol{x}) = int rac{oldsymbol{f}(oldsymbol{y})cdot(oldsymbol{x}-oldsymbol{y})}{4 pi |oldsymbol{x}-oldsymbol{y}|^3} , mathrm{d}^3!y

See also



Darcy's law

Lubrication theory

Slender-body theory

References



★ Happel, J. & Brenner, H. (1981) ''Low Reynolds Number Hydrodynamics'', Springer. ISBN 9001371159.

★ Kim, S. & Karrila, S. J. (2005) ''Microhydrodynamics: Principles and Selected Applications'', Dover. ISBN 0486442195.

★ Ockendon, H. & Ockendon J. R. (1995) ''Viscous Flow'', Cambridge University Press. ISBN 0521458811.

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