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Numerical Heat Transfer, Part A: Applications
An International Journal of Computation and Methodology
Volume 73, 2018 - Issue 1
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Original Articles

Probing the Rayleigh–Benard convection phase change mechanism of low-melting-point metal via lattice Boltzmann method

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Pages 34-54 | Received 25 Oct 2017, Accepted 12 Dec 2017, Published online: 16 Jan 2018
 

ABSTRACT

A double distribution function lattice Boltzmann method (LBM) with multirelaxation time is implemented to simulate the Rayleigh–Benard convection melting of a typical low-melting-point metal in a rectangular cavity. Typical cases frequently encountered in practice with constant heat flux/constant temperature boundary conditions are parametrically investigated, with corresponding dimensionless results outlined; the influence of inclination angle of the cavity is also clarified. The computational speed of the current LBM would reach about 40 times faster than that of conventional finite volume method as performed by commercial software Fluent. The obtained results would be valuable for guiding practical thermal design.

Nomenclature

c=

lattice speed (m/s)

cp=

specific heat capacity (J/kg · K)

cs=

sound speed in lattice space (m/s)

=

propagation velocity of the ith discrete particle (m/s)

=

body force (N/m3)

Fo=

Fourier number

f=

density distribution function

fl=

liquid fraction

=

gravitational acceleration (m/s2)

g=

enthalpy distribution function

H=

total enthalpy (J/kg)

Hc=

cavity height (m)

ΔH=

fusion latent heat (J/kg)

I=

unit matrix

k=

thermal conductivity (W/m · K)

Lc=

characteristic length (m)

M=

orthogonal transformation matrix

Ma=

Mach number

m=

distribution function in moment space

Nu=

Nusselt number

=

unit normal vector on liquid–solid interface

P=

dimensionless pressure

Pr=

Prandtl number

p=

pressure (N/m2)

=

heat flux (W/m2)

Ra=

Rayleigh number

S=

diagonal matrix

Ste=

Stefan number

ST=

dimensionless subcooling

T=

temperature (K)

t=

time (s)

=

dimensionless velocity vector

U0=

characteristic velocity for natural convection (m/s)

=

(u, v), velocity vector (m/s)

=

dimensionless movement velocity of solid–liquid interface

=

movement velocity of solid–liquid interface (m/s)

W=

cavity width (m)

wi=

weighted coefficient of the ith discrete particle

X, Y=

dimensionless rectangular coordinates

x, y=

rectangular coordinates (m)

Greek letters=
α=

thermal diffusivity (m2/s)

β=

volume thermal expansivity (1/K)

γ=

aspect ratio of the cavity

ε=

small disturbance value

Θ=

dimensionless temperature

θ=

inclination angle (°)

υ=

kinetic viscosity (m2/s)

ρ=

mass density (kg/m3)

φ=

melting fraction

τ=

dimensionless relaxation time

Subscripts=
b=

bottom wall

C=

cold wall

eq=

equilibrium distribution

H=

hot wall, constant heat flux boundary condition

i=

= 0, 1, 2 … 8, discrete particle index

l=

liquid phase

la=

lattice space

m=

melting point

j=

index of lattice node on cavity bottom

T=

constant temperature boundary condition

r=

reference value

s=

solid phase

Nomenclature

c=

lattice speed (m/s)

cp=

specific heat capacity (J/kg · K)

cs=

sound speed in lattice space (m/s)

=

propagation velocity of the ith discrete particle (m/s)

=

body force (N/m3)

Fo=

Fourier number

f=

density distribution function

fl=

liquid fraction

=

gravitational acceleration (m/s2)

g=

enthalpy distribution function

H=

total enthalpy (J/kg)

Hc=

cavity height (m)

ΔH=

fusion latent heat (J/kg)

I=

unit matrix

k=

thermal conductivity (W/m · K)

Lc=

characteristic length (m)

M=

orthogonal transformation matrix

Ma=

Mach number

m=

distribution function in moment space

Nu=

Nusselt number

=

unit normal vector on liquid–solid interface

P=

dimensionless pressure

Pr=

Prandtl number

p=

pressure (N/m2)

=

heat flux (W/m2)

Ra=

Rayleigh number

S=

diagonal matrix

Ste=

Stefan number

ST=

dimensionless subcooling

T=

temperature (K)

t=

time (s)

=

dimensionless velocity vector

U0=

characteristic velocity for natural convection (m/s)

=

(u, v), velocity vector (m/s)

=

dimensionless movement velocity of solid–liquid interface

=

movement velocity of solid–liquid interface (m/s)

W=

cavity width (m)

wi=

weighted coefficient of the ith discrete particle

X, Y=

dimensionless rectangular coordinates

x, y=

rectangular coordinates (m)

Greek letters=
α=

thermal diffusivity (m2/s)

β=

volume thermal expansivity (1/K)

γ=

aspect ratio of the cavity

ε=

small disturbance value

Θ=

dimensionless temperature

θ=

inclination angle (°)

υ=

kinetic viscosity (m2/s)

ρ=

mass density (kg/m3)

φ=

melting fraction

τ=

dimensionless relaxation time

Subscripts=
b=

bottom wall

C=

cold wall

eq=

equilibrium distribution

H=

hot wall, constant heat flux boundary condition

i=

= 0, 1, 2 … 8, discrete particle index

l=

liquid phase

la=

lattice space

m=

melting point

j=

index of lattice node on cavity bottom

T=

constant temperature boundary condition

r=

reference value

s=

solid phase

Additional information

Funding

This work is partially supported by Dean’s Research Funding of the Chinese Academy of Sciences and the Frontier Project of the Chinese Academy of Sciences, the Ministry of Higher Education Equipment Development Fund.

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