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Fig. 12.1 Physical problem
at time t* = 0
Based on the previous hypothesis, the governing equations used in the non-
rectangular liquid domain can be written in their dimensionless form as following:
r V ¼ 0
ð 12 : 3 Þ
q ð T Þ q ref
q ref
k
gH 3
t 2
ð V V ¼ r 2 V r P+
ð 12 : 4 Þ
Pr r 2 h
( V h ¼ 1
ð 12 : 5 Þ
The dimensionless velocity vector V is given by: V ¼ V ð Þ= t, where t is the
kinematic viscosity. The dimensionless temperature is given by h ¼ T T av
ð Þ= DT ,
where T av is the average temperature given by T av ¼ T H þ T Fu ð Þ= 2. T is the
dimensional temperature, and DT ¼ T H T Fus . The Prandtl number is given by
Pr = t/a, and a is the thermal diffusivity. P is the dimensionless pressure, given by
P ¼ P ðÞ H 2 ; q ref is the reference density (equal to the average density of the
interval imposed by the temperature of the walls) and k is the unitary vector in the
vertical direction. At the moving interface, the energy balance equation is given by:
r h n ¼ o c
os
ð 12 : 6 Þ
The t erm oc = o ð Þ represents the local velocity of the melting front along the
vector n, normal to the interface and s = Ste 9 Fo, with Stefan number given by
Ste = (c p DT)/L F , where c p is the specific heat and L F the latent heat. Fo is the
Fourier number.
12.2.1.1 Density Approximation in the Buoyancy Term
As mentioned earlier, for fluids that reach an extreme density value at a specific
temperature, it is not suitable to assume the hypothesis that the density varies
linearly with temperature. Contrary to the linear estimate that predicts a unicellular
flow, the maximum density formulation predicts a bicellular flow. As for water, the
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