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A MODEL FOR MOISTURE-CONTENT EVOLUTION IN POROUS BUILDING ELEMENTS: TREATMENT OF IRREGULAR REGIONS
A MODEL FOR MOISTURE-CONTENT EVOLUTION IN POROUS BUILDING
ELEMENTS: TREATMENT OF IRREGULAR REGIONS
Regina Katsman ,
NRC/IRC, Bld. M-24, Montreal Rd., Ottawa
ON K1A 0R6, Canada
Rachel Becker
Department of Civil Engineering, Technion
Israel Institute of Technology, Haifa, 32000,
Israel
Becker@tx.technion.ac.il
Regina.Katsman@nrc.ca
ABSTRACT
The effects of moisture movement and residual
moisture content are becoming a recognized part of a
performance based design of buildings. Despite the
long-time existence of a basic 3-D formulation of heat
and mass transfer within porous materials, the
generalized hygrothermal behavior of construction
elements that contain hygrothermal bridges and/or air
voids has not been studied. Neither have the processes,
which occur at the interfaces between different
materials, been investigated. Relying on basic energy
and mass conservation principles, a general integral
form of presentation was applied to establish the
coupled heat and mass transfer field equations, which
were
further transformed to a discrete set of algebraic
equations. This form of presentation is more suitable
for treatment of irregular regions, such as material
interfaces and internal air voids. To treat these regions,
specific mathematical procedures were implemented.
Two Software packages were written to simulate the
evolution of moisture content in non-homogeneous flat
planar walls, without and with air voids. Finally, the
results
of modeling are presented for both types of
constructions, thus enabling one to analyse a
hygrothermal behavior of irregular wall's regions.
building material [4 to 9]. Despite the long-time
existence of a basic 3-D formulation of heat and mass
transfer within porous materials, the generalized
hygrothermal behavior of construction elements that
contain hygrothermal bridges and air voids has not been
studied yet. Neither have the processes, which occur at
the interfaces between different materials, been
investigated. Moreover, the effects of commonly
existing air-voids (in the form of large hollow-cores or
small deffects) within the materials composing the wall,
or at the interfaces between the materials (as usually
stems from the construction methods for the jointing),
have not been studied either.
This paper is devoted to the mathematical modeling and
numerical solution of the moisture-content evolution in
walls with hygrothermal bridges, including the case of a
construction with air voids, concentrating mainly on
methods of mathematical treatment of irregular wall's
regions.
MATHEMATICAL MODEL
The basic physical considerations and previous research
indicate that the mutual influence of the heat and mass
transfer is an inherent property of the explored system.
Moreover, the mutual influence of these phenomena on
the moisture-content evolution may be particularly
significant at the boundaries, where solid meets humid
air with variable humidity, and at interfacial zones
between different materials.
Generally, the above-mentioned Philip and De-Vries
differential equations are actually an outcome of the
energy and mass conservation principles. However, for
the present aims, the integral form of presenting these
basic priciples is the most suitable, as it enables easy
inclusion of interfaces between different materials,
internal air-voids and their internal boundaries.
INTRODUCTION
For most planar building elements (usually designated
by the general term walls), the main moisture
movement is in the direction perpendicular to the
element’s air-exposed surfaces. However, the non-
homogeneous structure of the element within its main
plane causes multidirectional moisture movement. The
general formulation of simultaneous heat and mass
transfer in a porous material has been performed by
Luikov [1] in order to analyze moisture transport
phenomena in soils. It has then been implemented for
building materials by Philip and De-Vries [2] and since
then by others [3,4]. The field equations, which
emerge from this formulation, have been used since
then for analyzing various cases. These works include
investigations of 1-D heat and mass transfer phenomena
in building elements composed of a homogenous
General Scheme
The heat and mass field equations at every material
point are derived from the basic energy and mass
conservation principles:
Q
=
Q
I
+
Q
+
Q
(1)
S
T
v
E
=
E
+
E
+
E
t
2
∂
T
S
I
T
W
E
=
dt
⋅
D
⋅
⋅
dS
(2)
T
T
∂
n
Where:
Q
t
1
S
is the heat stored in an arbitrary control-
volume V (with a total surface area S) during
the time interval dt
(7)
t
2
∂
W
E
=
dt
⋅
D
⋅
⋅
dS
W
W
∂
n
t
S
1
Q
is the total resultant in-flowing heat across S
caused by the temperature gradient
(8)
Conducting several transformations, the field equations
are thus given by:
n (at
the surface, with the normal n to S pointing
outwards at every point on S)
∂
T/
∂
t
2
∂
T
t
∂
T
Q
is the total resultant heat produced within the
volume V by internal heat sources and sinks
(e.g. due to heat of hydration of cementitious
compounds)
dt
⋅
c
⋅
ρ
⋅
⋅
dV
=
dt
⋅
λ
⋅
⋅
dS
+
I
∂
t
∂
n
t
V
t
S
1
1
t
2
∂
T
dt
⋅
L
⋅
D
⋅
⋅
dS
vT
∂
n
Q
is the total resultant in-flowing latent heat
(associated with vaporization and
condensation processes) across S, caused by
the partial water-vapor pressure gradient
t
1
S
t
2
∂
W
+
dt
⋅
L
⋅
D
⋅
⋅
dS
vW
∂
n
∂
p/
∂
n
t
1
S
(at the surface, with the normal n as above)
(9)
E
is the total moisture stored in the same volume
V during the time interval dt
S
t
2
∂
W
t
2
∂
W
dt
⋅
⋅
dV
=
dt
⋅
D
⋅
⋅
dS
+
∂
t
W
∂
n
E
is the total resultant moisture produced within
the volume V by internal moisture sources and
sinks ( e.g. due to the hydration process of
cementitious materials)
t
V
t
S
I
1
1
t
2
∂
T
dt
⋅
D
⋅
⋅
dS
T
∂
n
t
1
S
E
is the total resultant in-flowing moisture across
S caused by the temperature gradient
(10)
The system of partial differential equations for the
simultaneous heat and mass transfer at a regular point
within the porous material, which is obtained from the
integral equations 9 and 10 when
E
is the total resultant in-flowing moisture across
S caused by the moisture-gradient
∂
W/
∂
n (at
V
, corresponds
to the classical Philip and De-Vries formulations and to
those given by the IEA Annex 24. However, as
presented in the following sections, the integral
presentation is more suitable for the general
development of the equations in irregular regions, such
as material interfaces and internal voids. Moreover, it is
more amenable for establishing the numerical
integration procedures at irregularities and at all the
internal and external boundary points.
→
0
the surface, with the normal n as above).
For the case without internal sources or sinks,
delineation of each factor then yields the following
integral presentations:
t
2
∂
T
Q
=
V
dt
c
⋅
ρ
⋅
⋅
dV
S
∂
t
t
1
(3)
t
2
∂
T
Q
=
dt
⋅
λ
⋅
⋅
dS
T
∂
n
Analytical Treatment of Irregular Regions
The following continuity equations emerge at materials’
interfaces when the zero-limit is reached for two
infinitesimal control volumes that have a mutual
interface S:
t
1
S
(4)
t
2
∂
p
Q
=
dt
⋅
L
⋅
D
⋅
⋅
dS
v
v
∂
n
t
S
1
T
=
T
(5)
−
S
+
S
t
2
∂
W
(11)
E
=
V
dt
⋅
dV
p
=
p
S
∂
t
−
S
+
S
t
1
(12)
(6)
2
t
2
∂
T
Derivation of the equations for an element with air-
voids is now straightforward. Figure 1 depicts the
schemes for the relevant control volumes within the
regular porous material (Volume 1) and within the air-
void (Volume 2).
[
dt
(
λ
+
L
⋅
D
)
dS
vT
∂
n
t
1
S
t
2
∂
W
+
dt
L
⋅
D
⋅
dS
]
vW
∂
n
−
S
t
1
S
t
2
∂
T
+
[
dt
(
λ
+
L
⋅
D
)
dS
vT
∂
n
t
1
S
dS
n
Volume 2
t
2
∂
W
V
aV
,
S
aV
+
dt
L
⋅
D
⋅
dS
]
=
0
T
aV
,
ρ
aV
,
p
aV
vW
∂
n
+
S
t
1
S
n
(13)
dS
t
∂
W
Volume 1
2
V
S
[
dt
D
⋅
dS
+
T
,
W
W
∂
n
t
1
S
t
2
∂
T
dt
D
⋅
dS
]
+
T
∂
n
−
S
t
1
S
Figure 1:
Scheme of general control-volumes within
the element’s regular material region (Volume 1)
and an air-void (Volume 2).
t
2
∂
W
[
dt
D
⋅
dS
+
W
∂
n
t
1
S
As a first order approximation, it is assumed that within
the void the air temperature and partial water-vapor
pressure distributions are uniform, except for an
extremely thin boundary layer at the interface with the
surrounding solid. Thus, across the void the
temperature and partial water-vapor pressure are
represented by unique values,
t
2
∂
T
dt
D
⋅
dS
]
=
0
T
∂
n
+
S
t
1
S
(14)
The following boundary-condition equations emerge at
material-air boundaries when the zero-limit is reached
for an infinitesimal control volume with an air-exposed
surface S:
p
. Wherever
part of the solid material continuum is replaced by an
air-void, equations 9 and 10 re-written for the total
entrained air volume
T
and
aV
aV
t
2
V
that is bounded by the
dt
h
s
dT
aS
dS
+
aV
S
(with a normal n into the porous medium).
After substitution of 15 and 16 this yields:
t
1
S
surface
aV
t
2
∂
T
dt
(
λ
+
L
⋅
D
)
⋅
dS
+
(15)
t
vT
∂
n
2
∂
T
aV
V
⋅
c
⋅
ρ
⋅
⋅
dt
=
t
S
1
aV
aV
aV
∂
t
t
2
∂
W
1
dt
L
⋅
D
⋅
dS
=
0
t
t
vW
∂
n
2
∂
T
2
∂
T
dt
⋅
λ
⋅
⋅
dS
+
dt
⋅
L
⋅
D
⋅
⋅
dS
+
t
S
1
∂
n
vT
∂
n
t
2
1
S
aV
1
S
aV
dt
β
s
⋅
dp
aS
⋅
dS
+
2
∂
W
t
2
dt
⋅
L
⋅
D
⋅
⋅
dS
=
−
dt
h
dT
dS
t
S
1
vW
s
aS
∂
n
aV
t
2
∂
W
1
S
aV
t
1
S
aV
dt
D
⋅
⋅
dS
+
(16)
(17)
W
∂
n
t
1
S
t
2
∂
T
dt
D
⋅
⋅
dS
=
0
T
∂
n
t
1
S
,
t
t
t
t
t
t
2
∂
ρ
2
∂
W
22
i,j+1
33
V
⋅
aV
dt
=
dt
⋅
D
⋅
⋅
dS
+
aV
∂
t
W
∂
n
t
t
S
G
g
H
1
1
aV
dy(j)
2
∂
T
dt
⋅
D
⋅
⋅
dS
=
A
C
T
∂
n
2
3
1
S
aV
i-1,j
i+1,j
i,
j
t
1
4
2
B
D
−
dt
β
⋅
dp
⋅
dS
s
aV
aS
dy(j-1)
1
S
aV
E
F
(18)
This model does not take into account gravitational
moisture movement that occurs in pores or cracks
outside the capillary range, or within vertical air-voids.
Neither does it address the convection inside the porous
material, effects of direct rainfall, solar radiation or air
transport.
11
dx(i-1)
i,j-1
dx(i)
44
Figure 2:
Scheme of the mesh at a general point i,j.
The integration points (nodes i,j) are on an orthogonal
grid, with main grid line along all material boundaries.
The grid is composed between its main lines by a
variable-size mesh. The control volume around every
node extends until the mid-distance to the next mesh-
node in every direction (rectangle ABEFDCHG in
Figure 2). Each of the four parts of the control volume,
1 to 4, may be composed of a different material.
NUMERICAL SOLUTION
General Scheme
The solution procedure adopted here is based on the
presentation of the integral equations in a discrete form,
including the boundaries and air-voids. An implicit
scheme was chosen for the numerical integration
process. The ensuing discrete set of algebraic equations
with non-constant coefficients is solved by means of an
iterative convergence process. In addition, at this stage
the solution was limited to the case of an orthogonal x-y
coordinate system, as most building walls have only
orthogonal internal and external surfaces.
Using an implicit scheme for the linearized set of
equations provides the stability of the numerical
solution without dependence on time and space steps.
In particular, for the iterative process used to solve the
equations with variable coefficients this scheme is
preferred because of its monotonous behavior. The
examples presented in this paper were solved using the
“optimal” time steps that stem from the spatial mesh,
which was chosen in accordance with the geometric
features of the analyzed construction, where the term
“optimal” refers in this case to the time step that would
be recommended as maximal in order to render an
explicit
Numerical Treatment of Irregular Regions
In establishing the field and boundary condition
equations, the temperature and moisture content within
each part are presented by their values at the node i,j. If
at a certain node nm different materials meet (nm
≤
4),
moisture-content in these materials at the node,
W
,
k
(
j
k=1,…,nm), is different, while the temperature,
T
,
j
,
and the partial water-vapor pressure,
p
,
j
, are identical
, are also identical).
The different moisture-contents at the node, generally
presented by the four points 1 to 4, are inter-dependent.
Their dependence is obtained via the sorption isotherms
of the different materials. The following procedure was
used for instantaneous linearization of the discrete set
of equations: At every iteration-step, m, undertaken
within a given time step,
ϕ
i
,
j
scheme
stable
(i.e.
dt
, from n to n+1 (with n=0
n
t
, where dn designates a
mesh step in any direction and
∆
=
min[(
dn
)
2
/(
2
⋅
α
)]
at t=0):
max
k
k
1
,
∂
W
∂
W
∂
W
any of the relevant
diffusivity coefficients in the equations).
The scheme for the numerical model is shown in Figure
2.
α
(
i
,
j
)
n
+
1
=
(
i
j
)
m
⋅
(
i
j
)
n
+
1
=
∂
t
∂
W
1
,
∂
t
i
j
∂
W
k
∂ϕ
∂
W
1
,
(
i
,
j
⋅
)
m
⋅
(
i
j
)
n
+
1
=
∂ϕ
∂
W
1
,
∂
t
i
j
t
t
t
t
(i.e. Relative-Humidity values,
,
ξ
k
∂
W
∂
1
,
EXAMPLES
Two examples are given to demonstrate the effects
occurring in the irregular regions that are highlighted by
the suggested 2-D analysis for a drying process of a
block-wall with joints and surface-renderings. These
examples are restricted to the case of a symmetrical
AAC wall with cementitous-mortar joints and
renderings, without and with air-voids, drying
symmetrically from a nearly saturated initial state.
(
i
,
j
)
m
⋅
(
i
j
)
n
+
1
ξ
1
,
t
i
j
(19)
for k that runs from 2 to 4.
Or, re-written in the discrete form:
ξ
k
(
W
k
)
n
+
1
=
(
W
k
)
n
+
(
i
,
j
)
m
⋅
i
,
j
i
,
j
ξ
1
,
i
j
((
W
1
,
)
n
+
1
−
(
W
1
,
)
n
)
Construction data
The element without air-voids is shown in Figure 3,
i
j
i
j
(20)
For the sake of brevity,
(
W
)
1
,
n
and
(
W
1
,
)
n
+
are
y
j
j
Joint
Rendering
AAC Block
n
,
+
1
W
.
For equations at internal and external boundaries, the
values of
W
,
and
j
j
20
p
are unknowns. They depend, however,
non-linearly on the unknowns
n
,
+
1
j
100
W
.
Disceretization and linearization are thus performed by
the following:
T
and
,
+
1
,
+
1
j
j
17
18
19 20
21
240
p
n
+
1
(
T
n
+
1
,
W
n
+
1
)
=
p
n
(
T
n
,
W
n
)
+
12
13
14 15
16
80
i
,
j
i
,
j
i
,
j
i
,
j
i
,
j
i
,
j
fs
m
⋅
(
T
n
+
1
−
T
n
)
+
gs
m
⋅
(
W
n
+
1
−
W
n
)
7
9
8
11
10
20
20
i
,
j
i
,
j
i
,
j
i
,
j
i
,
j
i
j
5
6
(21)
1 2 3
Rendering
4
x
(24)
(32)
Where:
p
n
(
T
n
,
W
n
)
=
p
n
(
T
n
)
⋅
ϕ
n
(
T
n
,
W
n
)
,
5
5
245
i
,
j
i
,
j
i
,
j
sat
,
i
,
j
i
,
j
i
,
j
i
,
j
i
,
j
(22)
fs
m
=
(
∂
p
i
,
j
)
m
Figure 3:
The element without air-voids.
while the one with air-voids is depicted in Figure 4.
i
,
j
∂
T
i
,
j
y
(23)
Joint
Rendering
AAC Block
∂
p
p
m
20
gs
m
=
(
i
,
j
)
m
=
sat
,
i
,
j
i
,
j
∂
W
ξ
m
j
Void 1
Void 2
i
,
j
i
,
100
(24)
The local instantaneous values of all the terms on the
RHS of equations 23 and 24, at the intermediate time
step m, are thus derived from the local instantaneous
values
50
19 20
22
21
2
240
50
23
3
127
80
12
13
14 15
16
m
j
m
j
W
,
. These parameters are further
calculated by means of additional inherent series of
sub-iterations applied for each iterative convergence
stage, from time step n to n+1.
Two Software packages, MA2DW and MA2DWV,
were written to solve numerically the evolution of
moisture content in flat planar walls and verified by
specific examples. The first one is designed for the
solution of walls without air voids and the second for
those with.
T
,
and
7
9
8
11
10
20
20
5
6
1 2 3
Rendering
4
x
5
5
245
255
Figure 4:
The element with air-voids.
Air-void No. 1 represents a cavity in the joint-mortar in
accordance with the manner of construction frequently
adopted for block-walls. Air-void No. 2 represents a
1
n
denoted in the sequel by
n
n
,
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