Publication Cover
Numerical Heat Transfer, Part B: Fundamentals
An International Journal of Computation and Methodology
Volume 69, 2016 - Issue 5
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Original Articles

A coupled element-based finite-volume method for the solution of incompressible Navier-Stokes equations

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Pages 447-472 | Received 05 Aug 2015, Accepted 23 Oct 2015, Published online: 23 Mar 2016
 

ABSTRACT

This article presents a new element-based finite-volume discretization approach for the solution of incompressible flow problems on co-located grids. The proposed method, called the method of proper closure equations (MPCE), employs a proper set of physically relevant equations to constrain the velocity and pressure at integration points. These equations provide a proper coupling between the nodal values of pressure and velocity. The final algebraic equations are not segregated in this study and are solved in a fully coupled manner. To show the applicability and performance of the method, it is tested on several steady two-dimensional laminar-flow benchmark cases. The results indicate that the method simulates the fluid flow in complex geometries and on nonorthogonal computational grids accurately. Also, it is shown that the method is robust in the sense that it does not require severe underrelaxation even at relatively high Reynolds numbers. In each test case, the required underrelaxation parameter, the number of iterations, and the corresponding CPU time are reported.

Nomenclature

a=

wavy wall amplitude

=

influence coefficients for example in Eq. (38)

A=

area of control surface, matrix of coefficients

bU, bV, bP=

vectors of known values

Cf=

Skin-friction coefficient

=

influence coefficients, for example in Eq. (58)

F=

flow term

Gm=

influence coefficient in Eq. (44)

h=

nondimensional uniform grid spacing

H=

height

=

influence coefficients, for example in Eq. (47)

=

influence coefficients, for example in Eq. (51)

L=

length, width

N=

bi-linear shape functions and total number of nodes

p=

pressure

P=

dimensionless pressure

r=

radius

Re=

Reynolds number

Res=

residual

s, t=

local coordinates

u, v=

velocity components

U, V=

dimensionless velocity components

=

velocity vector

x, y=

Cartesian coordinates

X, Y=

dimensionless Cartesian coordinates

=

gradient

⟦ ⟧=

maximum value

θ=

inclination angle

μ=

dynamic viscosity

ρ=

density

ϕ=

a general scalar variable

ω=

relaxation parameter

Subscripts=
0=

reference value

avg=

average

d=

down

e=

end point of the wavy wall

i=

inner

i, j, m, n, p, q=

dummy indices

ip=

integration point

l=

left

lid=

lid-driven

max=

maximum

o=

outer

r=

right

rms=

root mean square

u=

up

s=

start point of the wavy wall

w=

wall

Superscripts=
con=

continuity

exa=

exact

mom=

momentum

n=

iteration level

num=

numerical

P=

pressure

U, V=

velocity components

U-conv=

X-momentum convection

U-conv-U,-V, …=

influence coefficients in X-momentum convection

U-diff=

X-momentum diffusion

U-diff-U,-V, …=

influence coefficients in X-momentum diffusion

u-, U-mom=

x and X momentum

U-press=

X-momentum pressure

U-press-U,-V, …=

influence coefficients in X-momentum pressure

v-, V-mom=

y and Y momentum

u-, U-mom=

x and X momentum

Nomenclature

a=

wavy wall amplitude

=

influence coefficients for example in Eq. (38)

A=

area of control surface, matrix of coefficients

bU, bV, bP=

vectors of known values

Cf=

Skin-friction coefficient

=

influence coefficients, for example in Eq. (58)

F=

flow term

Gm=

influence coefficient in Eq. (44)

h=

nondimensional uniform grid spacing

H=

height

=

influence coefficients, for example in Eq. (47)

=

influence coefficients, for example in Eq. (51)

L=

length, width

N=

bi-linear shape functions and total number of nodes

p=

pressure

P=

dimensionless pressure

r=

radius

Re=

Reynolds number

Res=

residual

s, t=

local coordinates

u, v=

velocity components

U, V=

dimensionless velocity components

=

velocity vector

x, y=

Cartesian coordinates

X, Y=

dimensionless Cartesian coordinates

=

gradient

⟦ ⟧=

maximum value

θ=

inclination angle

μ=

dynamic viscosity

ρ=

density

ϕ=

a general scalar variable

ω=

relaxation parameter

Subscripts=
0=

reference value

avg=

average

d=

down

e=

end point of the wavy wall

i=

inner

i, j, m, n, p, q=

dummy indices

ip=

integration point

l=

left

lid=

lid-driven

max=

maximum

o=

outer

r=

right

rms=

root mean square

u=

up

s=

start point of the wavy wall

w=

wall

Superscripts=
con=

continuity

exa=

exact

mom=

momentum

n=

iteration level

num=

numerical

P=

pressure

U, V=

velocity components

U-conv=

X-momentum convection

U-conv-U,-V, …=

influence coefficients in X-momentum convection

U-diff=

X-momentum diffusion

U-diff-U,-V, …=

influence coefficients in X-momentum diffusion

u-, U-mom=

x and X momentum

U-press=

X-momentum pressure

U-press-U,-V, …=

influence coefficients in X-momentum pressure

v-, V-mom=

y and Y momentum

u-, U-mom=

x and X momentum

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