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Towards nonlinear imperfect interface models including micro-cracks and smooth roughness
Serge Dumont, Frédéric Lebon, Maria Letizia Raffa, Raffaella Rizzoni
To cite this version:
Serge Dumont, Frédéric Lebon, Maria Letizia Raffa, Raffaella Rizzoni. Towards nonlinear imper-
fect interface models including micro-cracks and smooth roughness. Annals of Solid and Structural
Mechanics, Springer Berlin Heidelberg, 2017, 9 (1-2), pp.13-27. �10.1007/s12356-017-0047-8�. �hal-
01697064�
Towards nonlinear imperfect interface models including micro-cracks and smooth roughness
S. Dumont
1· F. Lebon
2· M. L. Raffa
3· R. Rizzoni
4Keywords Asymptotic analysis · Nonlinear constitutive equations · Roughness · Imperfect interface · Nonlinear contact laws
1 Introduction
Nowadays structural bonding is a very common technique in numerous industrial domains as aeronautics or civil engi- neering. This technology consists in an adhesive assembly of two bodies. The main function of this assembly is to transmit mechanical stresses in a given environment dur- ing the whole life of the structure. The technology’s ben- efits are obvious: low costs, simplified industrial processes, increased lightness, etc. Conventional adhesives (epoxides, polyamides, acrylic, cyanoacrylates, etc.) come in the form of thin films. Therefore, it is very important to propose sim- ple as well as precise analytical and numerical models to simulate and predict the behavior of thin adhesive layers.
The present work aims at proposing a quite general meth- odology to describe the behavior of such a structure. Adhe- sive layers being often characterized by their low thickness, it seems natural to introduce an asymptotic model whose small parameter is the layers’ smallest characteristic length 𝜀. The problem of a thin adhesive joint is then classically replaced by a transmission problem with mechanical char- acteristics obtained from the mechanical and geometrical characteristics of the adhesive thin film (cf. [2, 12, 13, 15]).
In former papers by authors ([36, 38, 39, 45] and ref- erences therein), the illustrated methodology has been applied for a planar elastic thin adhesive interphase, pos- sibly anisotropic. Furthermore, in [37] this asymptotic technique within the small strains context was coupled to micromechanical homogenization concepts and Hertzian Abstract The present paper deals with a general asymp-
totic theory aimed at deriving some imperfect interface models starting from thin interphases. The novelty of this work consists in taking into account some non-standard constitutive behaviors for the interphase material. In par- ticular, micro-cracks, surface roughness and geometrical nonlinearity are included into the general framework of the matched-asymptotic-expansion theory. The elastic equilib- rium problem of a three-composite body comprising two elastic adherents and an adhesive interphase is investigated.
Higher order interface models are derived within the cases of soft and hard interphase materials. Simple FEM-based numerical applications are also presented.
F. Lebon
lebon@lma.cnrs-mrs.fr S. Dumont
serge.dumont@unimes.fr M. L. Raffa
maria-letizia.raffa@u-pec.fr R. Rizzoni
rizzoni.raffaella@unife.it
1 Université de Nîmes, Institut Montpellierain Alexander Grothendieck, CNRS UMR 5149, CC 051, Place Eugène Bataillon 34090 Montpellier, France
2 Aix-Marseille Univ., CNRS, Centrale Marseille, LMA, Marseille, France
3 CNRS, Laboratoire Modélisation et Simulation Multi Echelle, MSME UMR 8208 CNRS, 61 avenue du Général de Gaulle, 94010 Créteil Cedex, France
4 Department of Engineering, University of Ferrara, via Saragat 1, 44122 Ferrara, Italy
theory in order to formulate a model of contact between smoothly-rough surfaces in non-sliding conditions.
In the present paper, several additional new features are introduced. Particularly, an overview of simple techniques accounting for (smooth) roughness, micro-damage (micro- cracks) and geometrical nonlinearities is presented. Two main novelties are presented: (1) roughness is introduced in the asymptotic formulation within the framework of finite strain [36, 39, 44] as well as in the hard interface formula- tion; (2) two theories of micromechanical homogenization for micro-cracked materials, i.e., Kachanov’s theory [30, 48] and dilute scheme [4, 35], are studied and compared.
The paper is organized as follows. Firstly, a review of soft and hard imperfect interface models in linear elastic- ity is presented in Sect. 2. Next, a smooth roughness at the contacting interfaces between the two adherents and the adhesive interphase in introduced in Sect. 3. A simple methodology of micromechanical homogenization able to take into account micro-damage is presented in Sect. 4. In Sect. 5, an interphase consisting of a nonlinear elastic mate- rial, the Saint Venant–Kirchhoff material model, is studied.
Lastly, some simple numerical applications are proposed in Sect. 6, to validate the proposed interface models.
2 Soft and hard imperfect interface models in linear elasticity
We begin by specifying what we understand by “soft” and
“hard” interfaces. This notion is related to the stiffness ratio between the adhesive and the adherents. For example, in the case of two pieces of steel (with a stiffness close to 210 GPa) bonded by an araldite glue (a stiffness close to 2 GPa), the interphase is considered as soft. On the contrary, if two samples of maple wood (the stiffness is close to 10
GPa) are bonded by an epoxy resin (the Young’s modulus is close to 4 GPa), the interphase is considered as hard.
2.1 The three-dimensional equilibrium problem A thin interphase, B
𝜀, joining two adherents, Ω
𝜀±
, is consid- ered occupying a cylindrical region of small thickness and cross-section S, with S an open bounded set in IR
2with a smooth boundary 𝜕S. Introduced the Cartesian frame ( O , x
1
, x
2
, x
3
) with ( 𝐞
1
, 𝐞
2
, 𝐞
3
) the corresponding orthonor- mal basis, the domains B
𝜀and Ω
𝜀±
are defined as
with 0 < 𝜀 ∕ h << 1 and h the characteristic length of Ω. The surfaces between the adherents and the interphase of small thickness 𝜀 are
The geometrical configuration described above is shown in Fig. 1.
The adherents are subjected to a body force density 𝐟 :Ω
𝜀±↦ R
3and to a surface force density 𝐠 : Γ
𝜀g↦ R
3. Body forces are neglected in the adhesive.
On Γ
𝜀u= 𝜕 Ω
𝜀⧵ (Γ
𝜀g∪ 𝜕 Ω
𝜀∩ 𝜕 B
𝜀), homogeneous bound- ary conditions are prescribed:
where 𝐮
𝜀: Ω
𝜀↦ R
3is the displacement field defined on Ω
𝜀. Γ
𝜀gis assumed to be located far from the interphase and the fields of the external forces are endowed with sufficient B
𝜀= (1)
{
( x
1, x
2, x
3) ∈ Ω: − 𝜀 2 < x
3<
𝜀 2
} .
Ω
𝜀±= { (2)
( x
1, x
2, x
3) ∈ Ω: ± x
3>
𝜀 2
} ,
S
𝜀(3)
±
= {
( x
1, x
2, x
3) ∈ Ω: x
3= ± 𝜀 2
} .
𝐮
𝜀= 𝟎 on Γ
𝜀u, (4)
Fig. 1 Geometrical configura- tions of the three-composite system within the a the refer- ence model (interphase); b the rescaled model and c the limit model (interface)
regularity to ensure the existence of equilibrium configura- tion. In the following, the symbol (, ) means derivative. The equations governing the equilibrium problem of the com- posite structure are written as follows:
with 𝐮
𝜀= u
𝜀i
𝐞
ia displacement from Ω
𝜀±
∪ B
𝜀into IR
3, 𝛔
𝜀= 𝜎
𝜀ij
𝐞
i
⊗ 𝐞
j
the Cauchy stress, 𝐞 ( 𝐮
𝜀) the strain tensor under the small perturbations hypothesis (e
ij= 1∕2(u
i,j+ u
j,i)) and [[f ]]
±𝜀the jump of f at S
𝜀±
. The materials of the adherents and of the thin interphase are assumed to be homogeneous and linearly elastic and 𝐚
±
, 𝐛
𝜀are taken to denote the fourth-order elasticity tensors of the adherents and of the interphase, respectively. The tensors 𝐚
±, 𝐛
𝜀are assumed to be symmetric, with the minor and major symmetries, and positive definite. It is well known that the above equilibrium problem admits an unique solu- tion. At least two different methods are possible to study asymptotically the problem (5), by using the minimization of the total energy [18, 19, 42, 43, 45] or, directly, by using the equilibrium equations [9, 16, 17, 20–23, 34]. In this paper, the last method was preferred.
2.2 The rescaled equilibrium problem
Because the thickness of the interphase is very small, it is natural to seek an approximated solution of problem (5) as the small parameter 𝜀 vanishes. In this paper the method of matched asymptotic expansions is applied, which is based on a rescaling of the domains and on series expansions of the (rescaled) relevant fields (displacement and stress vector fields) with respect to 𝜀. In the following, the symbol (∧) will indicate the rescaled fields in the adhesive and the symbol (−) the rescaled fields in the adherents.
According to the method of matched asymptotic expan- sions, a classical change of scale is first applied to the adhe- sive and to the adherents [6]:
(5)
⎧ ⎪
⎪ ⎪
⎪ ⎪
⎨ ⎪
⎪ ⎪
⎪ ⎪
⎩ 𝜎
𝜀ij,j
+ f
i= 0 in Ω
𝜀±,
𝜎
𝜀ij
n
j= g
ion Γ
g,
𝜎
𝜀ij,j
= 0 in B
𝜀,
[[ 𝜎
𝜀i3
]]
±𝜀= 0 on S
𝜀±,
[[u
𝜀i]]
±𝜀= 0 on S
𝜀±, u
𝜀i= 0 on Γ
u, 𝜎
𝜀ij
= ( a
±)
ijkl
e
kl( 𝐮
𝜀) in Ω
𝜀±, 𝜎
𝜀ij
= (b
𝜀)
ijkle
kl( 𝐮
𝜀) in B
𝜀,
̂ (6)
𝐩:( x
1, x
2, x
3) ↦ ( z
1, z
2, z
3) = (
x
1, x
2, x
3𝜀 )
,
̄ (7)
𝐩:( x
1, x
2, x
3) ↦ ( z
1, z
2, z
3) = ( x
1, x
2, x
3± 1∕2 ∓ 𝜀 ∕2).
Let 𝐮 ̂
𝜀: = 𝐮
𝜀◦ 𝐩 ̂
−1be a displacement from the rescaled interphase
and let 𝐮 ̄
𝜀: = 𝐮
𝜀◦ 𝐩 ̄
−1be a displacement from the rescaled adherents
In (7) the plus (minus) sign applied in Ω
+(Ω
−). Under the change of variables, the domains Γ
uand Γ
gare transformed into the domains denoted by Γ ̄
uand Γ ̄
g, respectively. The external forces are assumed to be independent of 𝜀 , thus it is set f ̄ (z
1, z
2, z
3) = f (x
1, x
2, x
3), ̄ g(z
1, z
2, z
3) = g(x
1, x
2, x
3).
2.3 Asymptotic expansions
Within the rescaled configuration (cf. Fig. 1b), the asymp- totic expansions of the displacement fields in the adherents and in the interphase take the following form:
Starting from Eq. (11), the adhesive’s strain tensor is obtained:
with:
and
where 𝛼 = 1, 2, Sym( ⋅ ) gives the symmetric part of a tensor and k = 0, 1, …
The strain tensor in the adherents can be obtained as:
with:
B = (8) {
( x
1, x
2, x
3) ∈ Ω: − 1
2 < x
3< 1 2 }
,
Ω
±= { (9)
( x
1, x
2, x
3) ∈ Ω: ± x
3> 1 2
} .
(10) 𝐮
𝜀(z
1, z
2, z
3) = 𝐮
0+ 𝜀𝐮
1+ 𝜀
2𝐮
2+ o( 𝜀
2),
̂ (11)
𝐮
𝜀(z
1, z
2, z
3) = 𝐮 ̂
0+ 𝜀 ̂ 𝐮
1+ 𝜀
2𝐮 ̂
2+ o( 𝜀
2),
(12)
̄
𝐮
𝜀(z
1, z
2, z
3) = 𝐮 ̄
0+ 𝜀 ̄ 𝐮
1+ 𝜀
2𝐮 ̄
2+ o( 𝜀
2).
(13) 𝐞 ( 𝐮 ̂
𝜀) = 𝜀
−1𝐞 ̂
−1+ 𝐞 ̂
0+ 𝜀 ̂ 𝐞
1+ O ( 𝜀
2)
̂ (14) 𝐞
−1: =
⎡ ⎢
⎢ ⎣
0 1 2 u ̂
0𝛼,3
1 2 u ̂
0𝛼,3
u ̂
03,3
⎤ ⎥
⎥ ⎦
̂ (15) 𝐞
k: =
⎡ ⎢
⎢ ⎣
Sym(̂ u
k𝛼,𝛽)) 1
2 ( u ̂
k3,𝛼+ u ̂
k+1𝛼,3) 1
2 (̂ u
k3,𝛼+ u ̂
k+1𝛼,3) u ̂
k+13,3⎤ ⎥
⎥ ⎦ ,
(16) 𝐞 ( 𝐮 ̄
𝜀) = 𝜀
−1𝐞 ̄
−1+ 𝐞 ̄
0+ 𝜀 ̄ 𝐞
1+ O ( 𝜀
2)
̄ (17)
𝐞
−1= 𝟎,
and again k = 0, 1, … The stress fields in the rescaled adhe- sive and adherents, denoted 𝜎 𝜎 𝜎 ̂
𝜀= 𝜎 𝜎 𝜎 ◦ 𝐩 ̂
−1and 𝜎 𝜎 𝜎 ̄
𝜀= 𝜎 𝜎 𝜎 ◦ 𝐩 ̄
−1respectively, are represented in asymptotic expansions:
As body forces are neglected in the adhesive, the equi- librium equation can be written at the two first orders as:
where i = 1, 2, 3 .
Equation (22) shows that the stress vector 𝜎 𝜎 𝜎 ̂
0i3
is constant with respect to z
3in the adhesive, and thus it can be written:
where [ . ] denotes the jump between z
3=
1
2
and z
3= −
1 2
. Analogously, equation (23) can be rewritten in the fol- lowing integrated form:
All equations written so far are general in the sense that they are independent of the constitutive behavior of the materials.
The equilibrium equation in the adherents can be written as:
As a perfect contact law between the adhesive and the adherents is assumed, the continuity of the displacement and stress vector fields is enforced. In particular, the conti- nuity of the displacements leads to [45]:
̄ (18) 𝐞
k=
⎡ ⎢
⎢ ⎣
Sym(̄ u
k𝛼,𝛽) 1
2 (̄ u
k3,𝛼+ u ̄
k𝛼,3) 1
2 (̄ u
k3,𝛼+ u ̄
k𝛼,3) u ̄
k3,3⎤ ⎥
⎥ ⎦ ,
(19) 𝜎 𝜎 𝜎
𝜀= 𝜎 𝜎 𝜎
0+ 𝜀𝜎 𝜎 𝜎
1+ O ( 𝜀
2),
(20)
̂
𝜎 𝜎 𝜎
𝜀= 𝜎 𝜎 𝜎 ̂
0+ 𝜀 ̂ 𝜎 𝜎 𝜎
1+ O ( 𝜀
2),
(21)
̄ 𝜎
𝜎 𝜎
𝜀= 𝜎 𝜎 𝜎 ̄
0+ 𝜀 ̄ 𝜎 𝜎 𝜎
1+ O ( 𝜀
2) .
̂ (22) 𝜎 𝜎 𝜎
0i3,3
= 0,
̂ (23) 𝜎 𝜎 𝜎
0i1,1
+ 𝜎 ̂ 𝜎 𝜎
0i2,2
+ 𝜎 𝜎 ̂ 𝜎
1i3,3
= 0,
[ (24)
̂ 𝜎
0i3
]
= 𝟎 ,
[ 𝜎 𝜎 𝜎 ̂
1(25)
i3
] = −[ 𝜎 𝜎 𝜎 ̂
0i1,1
] − [ 𝜎 𝜎 𝜎 ̂
0i2,2
].
̄ (26) 𝜎
0ij,j
+ f
i= 0,
̄ (27) 𝜎
1ij,j
= 0.
(28) 𝐮
0(̄ 𝐱 , 0
±) = 𝐮 ̂
0(
̄ 𝐳 , ± 1
2 )
= 𝐮 ̄
0(
̄ 𝐳 , ± 1
2 )
,
(29) 𝐮
1(
𝐱 , 0
±)
± 1 2
𝐮
0,3
( 𝐱 , 0
±)
= ̂ 𝐮
1(
𝐳 , ± 1 2 )
= 𝐮
1(
𝐳 , ± 1 2 )
,
and the continuity of the stress vector gives the following conditions:
for i = 1, 2, 3.
Following [45], the matrices 𝐊
jl𝜀(with j, l = 1, 2, 3 ) are introduced, whose components are defined by the relation:
In view of the symmetry properties of the elasticity tensor 𝐛
𝜀, it results that 𝐊
jl𝜀= ( 𝐊
lj𝜀)
T, with j, l = 1, 2, 3.
2.4 Internal/interphase analysis
In the following, two specific cases of linearly elastic mate- rial are studied for the interphase. One, called “soft” material, is characterized by elastic moduli which are linearly rescaled with respect to the thickness 𝜀 ; the second case, called “hard”
material, is characterized by elastic moduli independent of the thickness 𝜀.
2.4.1 Soft interphase analysis
Assuming that the interphase is “soft”, one defines:
where the tensor 𝐛 does not depend on 𝜀. Accordingly to position (32), it is set:
Introducing the expansions in the constitutive equations leads to:
and
for j = 1, 2, 3, and
which represents the classical law for a soft interface.
Analogously, it is obtained:
𝜎 (30) 𝜎 𝜎
0i3
( 𝐱 , 0
±)
= 𝜎 ̂ 𝜎 𝜎
0i3
( 𝐳 , ± 1
2 )
= 𝜎 𝜎 𝜎
0i3
( 𝐳 , ± 1
2 )
(31) 𝜎 𝜎
𝜎
1i3
( 𝐱 , 0
±)
± 1 2 𝜎 𝜎 𝜎
0i3,3
( 𝐱 , 0
±)
= 𝜎 𝜎 𝜎 ̂
1i3
( 𝐳 , ± 1
2 )
= 𝜎 𝜎 𝜎
1i3
( 𝐳 , ± 1
2 )
(K
𝜀jl)
ki: = b
𝜀ijkl. (32)
𝐛
𝜀= 𝜀𝐛 , (33)
K
kijl: = b
ijkl. (34)
(35)
̂ 𝜎 𝜎
𝜎
0+ 𝜀 ̂ 𝜎 𝜎 𝜎
1= 𝐛 ( 𝐞 ̂
−1+ 𝜀 ̂ 𝐞
0) + o ( 𝜀 )
(36) 𝜎 ̂
𝜎 𝜎
0= b ( 𝐞 ̂
−1)
̂ 𝜎 𝜎
𝜎
1= b ( 𝐞 ̂
0)
̂ (37) 𝜎 𝜎
𝜎
0𝐢
j= 𝐊
3j𝐮 ̂
0,3
̂ (38) 𝜎 𝜎
𝜎
0𝐢
3= 𝐊
33[ 𝐮 ̂
0] ,
(39) [ 𝜎 𝜎 𝜎 ̂
1𝐢
3]
= − 𝐊
31[ 𝐮 ̂
0]
,1
− 𝐊
32[ 𝐮 ̂
0]
,2
Denoting < f > ( 𝐳 ̄ ): = 1 2
( f ( 𝐳 ̄ , 1
2 ) + f ( 𝐳 ̄ , − 1 2 ) )
, it is obtained:
where the sum over 𝛼 = 1, 2 is performed.
The complete problem for soft interface can be written at the two first orders as:
where << f >> ( 𝐱 ̄ ): = 1 2
( f ( 𝐱 ̄ , 0
+) + f ( 𝐱 ̄ , 0
−) ) . [ (40)
𝐮 ̂
1]
= ( 𝐊
33)
−1(
< ̂ 𝛔
1𝐢
3> − 𝐊
𝛼3< ̂ 𝐮
0>
,𝛼
)
(41)
⎧ ⎪
⎪ ⎪
⎨ ⎪
⎪ ⎪
⎩ 𝜎
0ij,j
+ f
i= 0 in Ω
±,
𝜎
0ij
n
j= g
ion Γ
g,
u
0i= 0 on Γ
u, 𝜎
0ij
= ( a
±)
ijkl
e
kl( 𝐮
0) in Ω
±, [
𝜎 𝜎 𝜎
0i3
] = 𝟎 on S, 𝜎
𝜎 𝜎
0i3
= 𝐊
33ik
[ u
0k]
on S.
(42)
⎧⎪
⎪⎪
⎪⎨
⎪⎪
⎪⎪
⎩ 𝜎1
ij,j=0 inΩ±,
𝜎1
ijnj=0 onΓg,
u1i =0 onΓu,
𝜎1
ij=𝜎1
ij=(
a±)
ijklekl(u1) inΩ±,
[𝜎𝜎𝜎1
i3
]= −𝐊3𝛼ik[ u0k]
,𝛼+<< 𝜎𝜎𝜎0
i3,3>> onS,
[u1i]
=( 𝐊33)−1
ij
(
<< 𝜎𝜎𝜎1
j3>>−𝐊𝛼3jk <<u0k>>,𝛼 )
+<<u0i,3>> onS,
Taking into account the first equation in (45) and using the positive definiteness of the tensor 𝐛, one obtains:
which corresponds to the kinematics of the perfect interface.
Analogously, it is obtained:
and
The complete problem for hard interface can be written at the two first orders as:
̂ (46) 𝐮
0,3
= 0 ⇒ [ 𝐮 ̂
0] = 𝟎,
[ 𝐮 ̂
1] = ( 𝐊
33)
−1(47) (
𝜎 ̂
𝜎 𝜎
0𝐢
3− 𝐊
𝛼3𝐮 ̂
0,𝛼
) ,
[ (48)
̂ 𝜎 𝜎 𝜎
1𝐢
3]
= (
− 𝐊
𝛼𝛽𝐮 ̂
0,𝛽
− 𝐊
3𝛼[̂ 𝐮
1] )
,𝛼
= ( (49)
− 𝐊
𝛼𝛽𝐮 ̂
0,𝛽
− 𝐊
3𝛼( 𝐊
33)
−1(
̂ 𝜎
𝜎 𝜎
0𝐢
3− 𝐊
𝛽3𝐮 ̂
0,𝛽
))
,𝛼
.
(50)
⎧ ⎪
⎪ ⎪
⎨ ⎪
⎪ ⎪
⎩ 𝜎
0ij,j
+ f
i= 0 in Ω
±,
𝜎
0ij
n
j= g
ion Γ
g,
u
0i= 0 on Γ
u, 𝜎
0ij
= ( a
±)
ijkl
e
kl(u
0) in Ω
±, [
𝜎 𝜎 𝜎
0i3
] = 𝟎 on S, [ u
0i]
= 0 on S.
(51)
⎧ ⎪
⎪ ⎪
⎪ ⎨
⎪ ⎪
⎪ ⎪
⎩
𝜎
1ij,j= 0 in Ω
±,
𝜎
1ijn
j= 0 on Γ
g,
u
1i= 0 on Γ
u,
𝜎
1ij= ( a
±)
ijkl
e
kl( 𝐮
1) in Ω
±,
[ 𝜎 𝜎 𝜎
1i3]
= (
K
ij𝛼𝛽u
0j,𝛽+ (
𝐊
3𝛼( 𝐊
33)
−1)
ij
(
̂ 𝜎 𝜎 𝜎
0j3− 𝐊
𝛽3jk
u
0k,𝛽))
,𝛼
+ << 𝜎 𝜎 𝜎
0i3,3>> on S, [ u
1i]
= ( 𝐊
33)
−1ij(
𝜎 𝜎 𝜎
0j3− 𝐊
𝛼3jk
u
0k,𝛼)
+ << u
0i,3>> on S.
2.4.2 Hard interphase analysis For a “hard” interphase, it is set:
where the tensor 𝐛 is independent of 𝜀, and 𝐊
jlis still taken to denote the matrices such that K
kijl: = b
ijkl.
Taking into account the relations (13) and (20), the stress-strain relationship takes the following form:
which gives 𝐛
𝜀= 𝐛 , (43)
(44) 𝜎 ̂
𝜎 𝜎
0+ 𝜀 ̂ 𝜎 𝜎 𝜎
1= 𝐛 ( 𝜀
−1𝐞 ̂
−1+ 𝐞 ̂
0+ 𝜀 ̂ 𝐞
1) + o ( 𝜀 ),
𝟎 = 𝐛 ( 𝐞 ̂
−1), (45) 𝜎 ̂
𝜎 𝜎
0= 𝐛 ( 𝐞 ̂
0).
3 How introduce roughness?
3.1 The three-dimensional equilibrium problem
In this Section, a general methodology is proposed to take into account the interphase roughness. In particular, two given positive-valued dimensionless roughness functions, 𝜂
±∈ C
0( S , IR
2), describing a smooth (i.e., 𝜂
±are independ- ent of 𝜀 ) surface roughness between the adherents and the interphase, are introduced. The domains B
𝜀, Ω
𝜀±
and S
𝜀±
are
then defined as:
and the interfaces between the adherents and the adhesive interphase are
We introduce two modified changes of variables:
Note that with these changes of variables, in the adhesive one has dx
3= 𝜂
±dz
3.
As a perfect contact law between the adhesive and the adherents is assumed, the continuity of the displacement and stress vector fields is enforced. In particular, the continuity of the displacements gives:
Expanding the displacement in the adherent, 𝐮
𝜀, in Taylor series along the x
3− direction and taking into account the asymptotic expansion, it results:
Thus it is obtained:
Identifying the terms with the same powers of 𝜀, Eq. (61) gives:
(52)
B𝜀={(x1,x2,x3) ∈ Ω: − 𝜀
2𝜂−(x1,x2)<x3 < 𝜀
2𝜂+(x1,x2)} ,
Ω
𝜀±= { (53)
( x
1, x
2, x
3) ∈ Ω: ± x
3> 𝜀
2 𝜂
±( x
1, x
2) } ,
S
𝜀(54)
±
= { ( x
1
, x
2
, x
3
) ∈ Ω: x
3
= ± 𝜀 2 𝜂
±( x
1
, x
2
) } .
̂ (55)
𝐩
𝜂:(x
1, x
2, x
3) ↦ (z
1, z
2, z
3) = (
x
1, x
2, x
3𝜂
+𝜀
) , x
3≥ 0,
̂ (56)
𝐩
𝜂:(x
1, x
2, x
3) ↦ (z
1, z
2, z
3) = (
x
1, x
2, x
3𝜂
−𝜀
) , x
3≤ 0,
(57)
𝐩̄𝜂:(x1,x2,x3)↦(z1,z2,z3) = (x1,x2,x3±1∕2−𝜂+𝜀∕2),x3≥0,(58)
𝐩̄𝜂:(x1,x2,x3)↦(z1,z2,z3) = (x1,x2,x3±1∕2+𝜂−𝜀∕2),x3≤0.(59) 𝐮
𝜀(
̄ 𝐱 , ± 𝜂
±𝜀
2 )
= 𝐮 ̂
𝜀(
̄ 𝐳 , ± 1
2 )
= 𝐮 ̄
𝜀(
̄ 𝐳 , ± 1
2 )
.
(60)
𝐮𝜀( 𝐱,̄ ±𝜂±𝜀
2 )
=𝐮𝜀(̄𝐱, 0±) ±𝜂±𝜀 2 𝐮𝜀
,3(𝐱, 0̄ ±) +⋯
=𝐮0(𝐱̄, 0±) +𝜀𝐮1(𝐱̄, 0±) ±𝜂±𝜀 2 𝐮0
,3(𝐱̄, 0±) +⋯
(61)
𝐮0(̄𝐱, 0±) +𝜀𝐮1(̄𝐱, 0±) ±𝜂±𝜀 2 𝐮0
,3
(𝐱, 0̄ ±) +⋯=̂𝐮0
(
̄ 𝐳,±1
2 )
+𝜀 ̂𝐮1 (
̄ 𝐳,±1
2 )
+⋯
=̄𝐮0 (
̄ 𝐳,±1
2 )
+𝜀 ̄𝐮1 (
̄ 𝐳,±1
2 )
+⋯
(62) 𝐮
0( 𝐱, 0 ̄
±) = 𝐮 ̂
0(
̄ 𝐳, ± 1
2 )
= 𝐮 ̄
0(
̄ 𝐳, ± 1
2 )
,
Following a similar analysis for the stress vector, analo- gous results are obtained:
for i = 1, 2, 3. Note that using this technique, the jump the stress vector at order zero is not modified. However, taking the derivatives along the third axis shows that the matching conditions at order one are modified as follows:
with <<< f >>> ( ⋅ ) = 1∕2 𝜂
+f ( ⋅ , 0
+) + 1∕2 𝜂
−f ( ⋅ , 0
−).
Now the equilibrium equation at order zero gives:
and thus,
At order one, the equilibrium equation leads to the condition
3.2 Soft interphase analysis
In this section, the interphase is assumed to be “soft”. The notation are the same as in Sect. 2. It is obvious to observe that Eq. (37) becomes
for j = 1, 2, 3, and
where 𝜂 = 𝜂
++ 𝜂
−2 . Equation (72) describes an imperfect interface mode taking into account roughness.
Combining Eqs. (70) and (71), it is obtained:
(63) 𝐮
1( 𝐱 , 0
±) ± 1
2 𝜂
±𝐮
0,3
( 𝐱 , 0
±) = ̂ 𝐮
1(
𝐳 , ± 1 2 )
= 𝐮
1(
𝐳 , ± 1 2 )
.
𝜎 (64) 𝜎 𝜎
0i3
( 𝐱 ̄ , 0
±) = 𝜎 𝜎 𝜎 ̂
0i3
( 𝐳 ̄ , ± 1
2 )
= 𝜎 𝜎 𝜎 ̄
0i3
( 𝐳 ̄ , ± 1
2 )
,
(65) 𝜎 𝜎
𝜎
1i3( 𝐱 ̄ , 0
±) ± 1
2 𝜂
±𝜎 𝜎 𝜎
0i3,3(̄ 𝐱 , 0
±) = 𝜎 𝜎 𝜎 ̂
1i3(
𝐳 ̄ , ± 1 2 )
= 𝜎 𝜎 𝜎 ̄
1i3(
𝐳 ̄ , ± 1 2 )
,
[ 𝐮
1]( 𝐱 ̄ ) = [ 𝐮 ̂
1]( 𝐱 ̄ )+ <<< 𝐮
0(66)
,3
>>> ( 𝐱 ̄ ),
[ 𝜎 𝜎 𝜎
1𝐞
3]( 𝐱 ̄ ) = [ 𝜎 𝜎 𝜎 ̂
1𝐞
3]( 𝐱 ̄ )+ <<< 𝜎 𝜎 𝜎
0(67)
,3
𝐞
3>>> ( 𝐱 ̄ ),
1 (68) 𝜂
±𝜎 𝜎 𝜎 ̂
0i3,3= 𝟎
[ (69)
̂ 𝜎 𝜎 𝜎
0i3
]
= 0.
̂ (70) 𝜎 𝜎
𝜎
1i3,3= − 𝜂
±𝜎 𝜎 𝜎 ̂
0i𝛼,𝛼.
𝜂
±𝜎 𝜎 𝜎 ̂
0𝐢
j= 𝐊
3j𝐮 ̂
0(71)
,3
̂ (72) 𝜎 𝜎 𝜎
0𝐢
3=
1 𝜂 𝐊
33[
̂
𝐮
0]
The constitutive equation gives:
Being 𝜎 𝜎 𝜎 ̂
1and 𝐮 ̂
0,𝛼
linear in z
3, we have [with j = 3 in Eq.
(74)]:
The complete problem for soft interface can be written at the two first orders as:
(73) [ 𝜎 𝜎 𝜎 ̂
1𝐢
3]
= − 𝐊
31[ 𝐮 ̂
0]
,1
− 𝐊
32[ 𝐮 ̂
0]
,2
̂ (74) 𝜎
𝜎 𝜎
1𝐢
j= 𝐊
𝛼j𝐮 ̂
0,𝛼
+ 1 𝜂
±𝐊
3j𝐮 ̂
0,3
[ (75)
̂ 𝐮
1]
= 𝜂 ( 𝐊
33)
−1(
< ̂ 𝜎 𝜎 𝜎
1𝐢
3> − 𝐊
𝛼3< ̂ 𝐮
0>
,𝛼)
(76)
⎧ ⎪
⎪ ⎪
⎪ ⎨
⎪ ⎪
⎪ ⎪
⎩
𝜎
0ij,j+ f
i= 0 in Ω
±, 𝜎
0ijn
j= g
ion Γ
g, u
0i= 0 on Γ
u, 𝜎
0ij= (
a
±)
ijkl
e
kl( 𝐮
0) in Ω
±, [
𝜎 𝜎 𝜎
0i3]
= 𝟎 on S, 𝜎
𝜎 𝜎
0i3= 1 𝜂
𝐊
33ik
[ u
0k]
on S.
The integration of the constitutive equations gives:
and by combining with the equilibrium equation one obtains
The complete problem for hard interface can be written at the two first orders as:
4 How introduce microcracks?
A very simple technique is now proposed to account for the presence of microcracks in the interphase. The idea is to introduce these microcracks (or porosity) directly in the elastic constitutive equations. A heterogeneous mate- rial is considered made of an elastic material with cracks.
To model the macroscopic behavior of cracked materials, homogenization models can be used and then a new homo- geneous equivalent medium can be defined. The stiffness tensor depends on the crack length and orientation. In [11, 40, 41], the authors introduce cracks by applying the meth- odology developed by Kachanov and his collaborators [30, 48]. In this approach, a crack density 𝜌 is introduced. In two dimensions, this density is seen as the ratio between the square of the length of the crack l and the elementary volume describing the material at the microscale. Thus, the [̂ 𝐮
1] = 𝜂( 𝐊
33)
−1(79)
(
̂ 𝜎 𝜎
𝜎
0𝐢
3− 𝐊
𝛼3𝐮 ̂
0,𝛼
)
[ (80)
̂ 𝜎 𝜎 𝜎
1𝐢
3]
= (
− 𝐊
𝛼𝛽𝐮 ̂
0,𝛽
− 𝐊
3𝛼[̂ 𝐮
1] )
,𝛼
= − 𝜂 (81) (
𝐊
𝛼𝛽𝐮 ̂
0,𝛽
+ 𝐊
𝛼3( 𝐊
33)
−1(
𝜎 ̂
𝜎 𝜎
0𝐢
3− 𝐊
𝛼3𝐮 ̂
0,𝛼
))
,𝛼
(82)
⎧ ⎪
⎪ ⎪
⎨ ⎪
⎪ ⎪
⎩ 𝜎
0ij,j
+ f
i= 0 in Ω
±,
𝜎
0ij
n
j= g
ion Γ
g,
u
0i= 0 on Γ
u, 𝜎
0ij
= ( a
±)
ijkl
e
kl( 𝐮
0) in Ω
±, [
𝜎 𝜎 𝜎
0i3
] = 𝟎 on S, [ u
0i]
= 0 on S.
(83)
⎧ ⎪
⎪ ⎪
⎪ ⎨
⎪ ⎪
⎪ ⎪
⎩
𝜎
1ij,j= 0 in Ω
±,
𝜎
1ijn
j= 0 on Γ
g,
u
1i= 0 on Γ
u,
𝜎
1ij= ( a
±)
ijkl
e
kl(u
1) in Ω
±,
[ 𝜎 𝜎 𝜎
1i3]
= 𝜂 (
K
ij𝛼𝛽u
0j,𝛽+ (
𝐊
3𝛼( 𝐊
33)
−1)
ij
(
̂ 𝜎
𝜎 𝜎
0j3− 𝐊
𝛽3jku
0k,𝛽))
,𝛼
+ <<< 𝜎 𝜎 𝜎
0i3,3>>> on S, [ u
1i]
= 𝜂( 𝐊
33)
−1ij(
𝜎 𝜎 𝜎
0j3− 𝐊
𝛼3jku
0k,𝛼)
+ <<< u
0i,3>>> on S.
3.3 Hard interphase analysis
In this section, a “hard” interphase is considered. The jump in the displacements at order zero is not modified:
giving again the kinematics of the perfect interface.
(77)
⎧⎪
⎪⎪
⎪⎨
⎪⎪
⎪⎪
⎩
𝜎ij,j1 =0 inΩ±,
𝜎ij1nj=0 onΓg,
u1i =0 onΓu,
𝜎ij1=( 𝐚±
)
ijklekl(u1) inΩ±,
[𝜎𝜎𝜎1i3]
= −𝐊3𝛼
ik
[u0k]
,𝛼+<<< 𝜎𝜎𝜎0i3,3>>> onS,
[u1i]
=𝜂( 𝐊33)−1
ij
(
<< 𝜎𝜎𝜎1j3>>−𝐊𝛼3
jk <<u0k>>,𝛼 )
+<<<u0i,3>>> onS.
̂ (78) 𝐮
0,3