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Basic concept of linear stability of small disturbances
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An Internet Book on Fluid Dynamics
The stability of steady laminar flows of an incompressible, Newtonian fluid of kinematic viscosity, ν, is assessed by a linear stability analysis that begins with the relevant equations of continuity and motion, (Bhf3) and (Bhf4): ∂ui ∂xi
= 0 (Bkc1)
∂ui ∂t
∂ui ∂xj
ρ
∂p ∂xi
∂^2 ui ∂xj∂xj
(Bkc2)
Each of the flow variables, q (where q represents ui or p) is then decomposed into a steady or time- independent component denoted by an overbar, ¯q, and a small, time-dependent perturbation, ˜q. The latter is envisaged as a small perturbation such that ˜q ¯q so that terms that are quadratic (or higher order) in ˜q quantities can be neglected leaving only terms that are either independent of or linear in ˜q quantities. Consequently various perturbations, ˜q, can be linearly superposed.
We will conduct what is known as a normal mode analysis by considering perturbations that are oscillatory in time, t, and in one spatial direction, say x, so that ˜q may be written in the form
q = q¯(xi) + ˜q(xi, t) = ¯q(xi) + Re
q˜∗(xi)ei(kx−ωt)
(Bkc3)
where i is the square root of −1, Re{ } denotes the “real part of” and ˜q∗^ is the amplitude of the perturbation. The wavenumber, k, and the radian frequency, ω, may both be complex so that
k = kR + ikI and ω = ωR + iωI (Bkc4)
where the subscripts R and I denote the real and imaginery parts. This allows two types of solution that are of particular interest namely
Here we will focus primarily on the first case and examine the rate of growth, ωI , of perturbations of frequency, ωR , and wavenumber, kR.
When expansions of the form (Bkc3) are substituted into the governing equation (Bkc2), the terms which are independent of t are isolated and solved to obtain the mean motion. The terms that are linear in the perturbations ˜q∗^ are the linear stability equations that are to be solved to determine the stability of the flow.
In practice, the implementation of this procedure is very difficult unless the basic mean flow is simple. Here we shall limit the implementation to simple planar, parallel flows in which the unperturbed flow consists
of a velocity, ¯u = U(y), in the x direction, ¯v = 0 and ¯p is uniform and constant. The equations of motion (Bkc2) for this parallel flow are:
∂u ∂t
∂u ∂x
∂y
ρ
∂p ∂x
∂^2 u ∂x^2
∂^2 u ∂y^2
(Bkc5)
∂v ∂t
∂v ∂x
ρ
∂p ∂y
∂^2 v ∂x^2
∂^2 v ∂y^2
(Bkc6)
The perturbations in the streamfunction, ψ˜, and pressure, ˜p, will be represented by
ψ˜ = Re
f(y)ei(kx−ωt)
and ˜p = Re
g(y)ei(kx−ωt)
(Bkc7)
so that
u˜ = Re
df dy
ei(kx−ωt)
and v˜ = Re
−ikf(y)ei(kx−ωt)
(Bkc8)
and substituting these expressions into the equations of motion, (Bkc5) and (Bkc6), yields
(ikU − iω)
df dy
− ik
dU dy
f = −
ikg ρ
−k^2
df dy
d^3 f dy^3
(Bkc9)
(k^2 U − kω)f = −
ρ
dg dy
ik^3 f − ik
d^2 f dy^2
(Bkc10)
Eliminating the function g from these two equations results in
(ω − kU)
d^2 f dy^2
− k^2 f
d^2 U dy^2
= iν
d^4 f df^4
− 2 k^2
d^2 f dy^2
(Bkc11)
This equation which must be solved for the perturbation f(y) is called the Orr-Sommerfeld equation. The version in which the viscous terms are neglected is
(ω − kU)
d^2 f dy^2
− k^2 f
d^2 U dy^2
= 0 (Bkc12)
and is called the Rayleigh equation. Notice that both versions are homogeneous in f and represent eigen- value problems for which we need to identify boundary conditions.
It remains to discuss the boundary conditions under which these equations must be solved. We will do so for boundary layer velocity profiles, for planar Couette flow and for planar pipe flow, cases which will be addressed in other sections. At any solid boundary parallel with the x direction at, say, y = 0, the zero normal velocity and no-slip conditions require that
(f)y=0 = 0 and
df dy
y=
= 0 (Bkc13)
Furthermore, in the case of the boundary layer problem we must require that
(f)y→∞ → 0 (Bkc14)
in order that the perturbation velocities decay to zero at large y. In the inviscid case governed by the Rayleigh equation (Bkc12), these three boundary conditions (equations (Bkc13) and (Bkc14)) complete the eigenvalue problem. The calculation for the spatial problem using a shooting method can proceed as follows. Given U(y) and a real frequency, ωR, we choose guessed vales for both kR and kI and begin the