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Linear stability analysis of fluid flows, Notas de estudo de Matemática

Basic concept of linear stability of small disturbances

Tipologia: Notas de estudo

2022

Compartilhado em 19/06/2023

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An Internet Book on Fluid Dynamics
Linear Stability Analyses
The stability of steady laminar flows of an incompressible, Newtonian uid 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 +uj
∂ui
∂xj
=1
ρ
∂p
∂xi
+ν2ui
∂xj∂xj
(Bkc2)
Each of the flow variables, q(where qrepresents uior 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¯qso that terms that are quadratic (or higher
order) in ˜qquantities 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,sothaqmay be written in the form
qq(xi)+˜q(xi,t)=¯q(xi)+Re ˜q(xi)ei(kxωt)(Bkc3)
where iisthesquarerootof1, Re{}denotes the “real part of” and ˜qis the amplitude of the
perturbation. The wavenumber, k, and the radian frequency, ω, may both be complex so that
k=kR+ikIand ω=ωR+I(Bkc4)
where the subscripts Rand Idenote the real and imaginery parts. This allows two types of solution that
are of particular interest namely
oscillatory perturbations that have an amplitude that is growing in space but not in time so that
ωI=0andω=ωRis the perturbation frequency. Then kRis the wavenumber of the wave-like
perturbation and kIis the growth or attenuation rate. For convenience we refer to this as the spatial
growth case.
oscillatory perturbations that have an amplitude that is growing in time but not in space so that
kI=0and2π/k =2π/kRis the wavelength of the perturbation. Then ωRis the spatial wavenumber
of the wave-like perturbation and ωIis the spatial growth or attenuation rate. For convenience we
refer to this as the temporal growth case.
Here we will focus primarily on the first case and examine the rate of growth, ωI, of perturbations of
frequency, ωR,andwavenumber,kR.
When expansions of the form (Bkc3) are substituted into the governing equation (Bkc2), the terms which
are independent of tare isolated and solved to obtain the mean motion. The terms that are linear in the
perturbations ˜qare 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
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An Internet Book on Fluid Dynamics

Linear Stability Analyses

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

  • uj

∂ui ∂xj

ρ

∂p ∂xi

  • ν

∂^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

  • oscillatory perturbations that have an amplitude that is growing in space but not in time so that ωI = 0 and ω = ωR is the perturbation frequency. Then kR is the wavenumber of the wave-like perturbation and kI is the growth or attenuation rate. For convenience we refer to this as the spatial growth case.
  • oscillatory perturbations that have an amplitude that is growing in time but not in space so that kI = 0 and 2π/k = 2π/kR is the wavelength of the perturbation. Then ωR is the spatial wavenumber of the wave-like perturbation and ωI is the spatial growth or attenuation rate. For convenience we refer to this as the temporal growth case.

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

∂u ∂x

  • v

∂U

∂y

ρ

∂p ∂x

  • ν

∂^2 u ∂x^2

∂^2 u ∂y^2

(Bkc5)

∂v ∂t

+ U

∂v ∂x

ρ

∂p ∂y

  • ν

∂^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

  • ν

−k^2

df dy

d^3 f dy^3

(Bkc9)

(k^2 U − kω)f = −

ρ

dg dy

  • ν

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

  • kf

d^2 U dy^2

= iν

d^4 f df^4

− 2 k^2

d^2 f dy^2

  • k^4 f

(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

  • kf

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