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Modification of the LS-STAG Immersed Boundary Method for Simulating Turbulent Flows

ISSN 1812-3368. Вестник МГТУ им. Н.Э. Баумана. Сер. Естественные науки. 2017. № 5

21

We denote the airfoil boundary as

.

K

Then the boundary conditions are the

following:

   

1 2 3

4

|

= ,

= 0,

| = .

ib

K

v

v

v

v v

n

It is possible to distinguish the linear turbulence scale

= ( )

turb turb

l

l

r

for all

turbulence models. In the framework of RANS approach this scale

turb

l

is equal to

scale

= ( ),

RANS RANS

l

l

r

which is determined by the turbulence model (Table 1).

Table 1

Turbulence scale

RANS

l

for some turbulence models [3]

Turbulence model

RANS

l

Comments

Spalart — Allmaras [4]

w

d

w

d

is the distance between the field point and

the nearest wall

 

k

[5]

3/2 1

k

is the dissipation rate of the turbulent kinetic

energy

k

 

k

[6],

 

k

SST [7]

 

1/2 *

1

( )

k

is the specific dissipation rate of the

k

,

 

*

0.09

In case of LES approach, the scale

turb

l

is equal to subgrid scale:

= .

LES

LES

l

C

(2)

Here

 

= ( )

r

is the characteristic filter size at the point of computational domain

with the radius vector

,

r

and

LES

C

is the empirical constant, which choice depends

on the turbulence model and numerical method used to solve the problem (1) in the

whole. Within the DES approach the linear turbulence scale

turb

l

is equal to hybrid

linear scale

=min{

,

}.

DES

RANS DES

l

l

C

(3)

Here

DES

C

is the empirical constant similar to

,

LES

C

and the maximum of the mesh

steps at the point of computational domain with the radius vector

r

is used as the

characteristic filter size

 

= ( ).

r

Thus, DES operates as RANS in the domain where

the mesh is too coarse and not suitable for resolving turbulent structures, i. e. at

> ,

DES

RANS

C l

and DES operates as subgrid model for LES in the domain where the

grid is sufficiently fine [3]. It should be noted that Smagorinsky model is used only

within LES approach.

In this paper Eddy Viscosity turbulence models (EVM) are considered. In EVM

models the eddy viscosity

t

(and the turbulent kinetic energy

k

in case of two-

equation models) is simulated and Reynolds or subgrid stresses are evaluated using

the Boussinesq eddy viscosity assumption [3]:

  

  

2

2

= 2

;

= 2

;

3

3

t

t

t

t

xx

yy

u

v

k

k

x

y

(4)