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Discrete Particles in a Jet Periodic Double Shear Flow - PanelDiscrete
Particles in a Jet Periodic Double Shear Flow - Panel

Pre-Analysis & Start-Up

Note

This site is currently under construction. Please come back after it is fully built. Thank you!

In the Pre-Analysis & Start-Up step, we'll review the following:

  • Theory for Fluid Phase
  • Theory for Particle Phase
  • Choosing the Cases

Pre-Analysis:

A particle laden flow is a multiphase flow where one phase is the fluid and the other is dispersed particles. Governing equations for both phases are implemented in Fluent. To run a meaningful simulation, a review of the theory is necessary.

Fluid Phase:

 

...

In

...

the

...

simulations

...

considered

...

for

...

this

...

tutorial,

...

the

...

fluid

...

flow

...

is

...

a

...

2D

...

perturbed

...

periodic

...

double

...

shear

...

layer

...

as

...

described

...

in

...

the

...

first

...

section.

...

The

...

geometry

...

is

...

Lx

...

=

...

59.15m,

...

Ly

...

=

...

59.15m,

...

and

...

the

...

mesh

...

size

...

is

...

chosen

...

as

...

Latex
{\large$$\Delta x = L_x / n_

...

x$$}

...

in

...

order

...

to

...

resolve

...

the

...

smallest

...

vorticies.

...

As

...

a

...

rule

...

of

...

thumb. One

...

typically

...

needs

...

about

...

20

...

grid

...

points

...

across

...

the

...

shear

...

layers,

...

where

...

the

...

vorticies

...

are

...

going

...

to develop.

...

The

...

boundary

...

conditions

...

are

...

periodic

...

in

...

the

...

x

...

and

...

y

...

 directions.

...

The

...

fluid

...

phase

...

satisfies the

...

Navier-Stokes

...

Equations:

...


-Momentum

...

Equations

Latex
{latex} \large 
\begin{eqnarray*}  
\rho_f (\frac{d \textbfmathbf{u}_f}}{dt}+\textbfmathbf{u}_f} \cdot \nabla \textbfmathbf{u}_f})=- \nabla p + \mu \nabla ^2 \textbfmathbf{u}_f} + \textbfmathbf{f}  
\end{eqnarray*} {latex 
}

-Continuity

...

Equation

Latex
{latex} \large 
\begin{align*}  
\frac{\partial \rho_f}{\partial t} + \nabla \cdot (\rho_f \textbfmathbf{vu}_f)=0 \\ \Rightarrow \nabla \cdot \textbf{v} = 0 \\ \
\end{align*} {latex
} 


where {latex}$\textbf{u_f}${latex} is the fluid velocity, {latex}$p${latex} the pressure, {latex}$\rho_f${latex} the fluid density and {latex}$\textbf{f}${latex} is a momentum exchange term due to the presence of particles. When the particle volume fraction and the particle mass loading {latex}$M

where

Latex
{\large$$\mathbf{u}$$}
is the fluid velocity,
Latex
{\large$$p$$}
the pressure,
Latex
{\large$$\rho_f$$}
the fluid density and
Latex
{\large$$\mathbf{f}$$}
is a momentum exchange term due to the presence of particles. When the particle volume fraction
Latex
{\large$$\phi$$}
and the particle mass loading
Latex
{\large$$M=\phi \rho_p/\rho_

...

f$$}

...

are

...

very

...

small,

...

it

...

is

...

legitimate

...

to

...

neglect

...

the

...

effects

...

of

...

the

...

particles

...

on

...

the

...

fluid:

...

Latex
{

...

\

...

large$$\

...

mathbf{f}

...

$$}

...

can

...

be

...

set

...

to

...

zero.

...

This

...

type

...

of

...

coupling

...

is

...

called

...

one-way.

...

In

...

these

...

simulations

...

the

...

fluid

...

phase

...

is

...

air,

...

while

...

the

...

dispersed

...

phase

...

is

...

constituted

...

of

...

about

...

400

...

glass

...

beads

...

of

...

diameter

...

a

...

few

...

dozens

...

of

...

micron.

...

This

...

satisfies both

...

conditions

...

Latex
{\large$$\phi \ll 

...

1$$}

...

and

...

Latex
{\large$$M \ll 

...

1$$}

...

One

...

way-coupling is legitimate here. See ANSYS documentation (16.2) for further details about the momentum exchange term.

Particle Phase:

The suspended particles are considered as rigid spheres of same diameter d, and density

Latex
{\large$$\rho_p$$}
. Newton’s second law written for the particle i stipulates:

Latex
{\large $$m_p \frac{d \mathbf{u}_p^i}{dt}=\mathbf{f}_{ex}^i$$}

where

Latex
{\large$$\mathbf{u}_p^i$$}
is

...

One way-coupling is legitimate here. See ANSYS documentation (16.2) for further details about the momentum exchange term.

 

Expected Results

...

the velocity of particle i,

Latex
{\large $$\mathbf{f}_{ex}^i$$}
the forces exerted on it, and
Latex
{\large $$m_p$$}
its mass.
In order to know accurately the hydrodynamic forces exerted on a particle one needs to resolve the flow to a scale significantly smaller than the particle diameter. This is computationally prohibitive. Instead, the hydrodynamic forces can be approximated roughly to be proportional to the drift velocity ref3:

Latex
{\large $$\frac{d \mathbf{u}_p^i}{dt}=\frac{\mathbf{u}_f-\mathbf{u}_p^i}{\tau_p}$$}

where

Latex
{\large $$\tau_p=\rho_p D^2/(18\mu)$$}
is known as the particle response time,
Latex
{\large $$\rho_p$$}
the particle density and D the particle diameter. This equation needs to be solved for all particles present in the domain. This is done in Fluent via the module: Discrete Phase Model(DPM).

 

Choosing the Cases:

The particle response time measures the speed at which the particle velocity adapts to the local flow speed. Non-inertial particles, or tracers, have a zero particle response time: they follow the fluid streamlines. Inertial particles with

Latex
{\large$$\tau_p \neq 0$$}
might adapt quickly or slowly to the fluid speed variations depending on the relative variation of the flow and the particle response time.

This rate of adaptation is measured by a non-dimensional number called Stokes number representing the ratio of the particle response time to the flow characteristic time scale.

Latex
{\large$$St = \frac{\tau_p}{\tau_f}$$}

In these simulations, the characteristic flow time is the inverse of the growth rate of the vortices in the shear layers. This is also predicted by the Orr-Sommerfeld equation. For the particular geometry and configuration we used in this tutorial, the growth rate is

Latex
{\large$$\gamma = 0.1751 s^{-1} = \frac{1}{\tau_f}$$}
. When St = 0 the particles are tracers. They follow the streamlines and, in particular, they will not be able to leave a vortex once caught inside.

When

Latex
{\large$$St \gg 1$$}
, particles have a ballistic motion and are not affected by the local flow conditions. They are able to shoot through the vorticies without a strong trajectory deviation. Intermediate cases
Latex
{\large$$St \approx 1$$}
have a maximum coupling between the two phases: particles are attracted to the vorticies, but once they reach the highly swirling vortex cores they are ejected due to their non zero inertia.

In this tutorial, we will consider a nearly tracer case St = 0.2, an intermediate case St = 1 and a nearly ballistic case St = 5.

Go to Step 2: Geometry

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