17.12.2019  Original Research  Ausgabe 6/2020 Open Access
A shell model for resin flow and preform deformation in thinwalled composite manufacturing processes
 Zeitschrift:
 International Journal of Material Forming > Ausgabe 6/2020
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Introduction
The class of liquid composite molding (LCM) processes has been widely employed for manufacturing fiber reinforced polymer composite materials (FRPCMs) and helps manufacturers to carve out a niche amid the keen market competition. Since the mid1980s, the automotive industries started to utilize the resin transfer molding (RTM) method to produce high volume production net shape structural components. Then the vacuum assisted resin transfer molding (VARTM) process sprung up in marine, energy and aerospace industries. The VARTM process can reduce the emission of volatile organic compounds, and produce highquality FRPCM parts with flexible, handy and lowcost tooling. However, the challenges of defects also appear during LCM processes, e.g., dry spots, springin, microvoids and thickness variations [
1]. The resin flow distribution arrangement dramatically influences the whole filling process, so it is keen to model and simulate the process numerically instead of relying on trial and error physically.
Between the late 80s and early 90s, Chan and Hwang [
2] started to solve the pressure distribution in the RTM process based on the Darcy’s law, which describes the fluid transfer in porous media. Fracchia et al. [
3] employed the control volume finite element method (CVFEM) together with the concept of volume of fraction (VOF) to simulate the mold filling in the RTM process using conforming finite elements. Since then, many results following this approach have been published, e.g., [
4,
5]. The modified CVFEM, e.g., [
6–
8], have been proposed. The boundary element method (BEM), e.g., Um and Lee [
9], the level set method, e.g., Soukane and Trochu [
10] or Gantois et al. [
11] and the smoothed particle hydrodynamics (SPH) method, e.g., [
12,
13] are also among the methods of LCM process modeling. What’s more, Remacle et al. [
14] presented a highorder model using the discontinuous Galerkin method (DGM). Wu and Larsson [
15] proposed a homogenized flow model based on the theory of porous media (TPM) to simulate the wetout RTM process. Another interesting study has been done recently by Dammann and Mahnken [
16] who used the phasefield models to model the RTM process.
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The research is not just limited to simulate the mold filling flow, but it is also extended to model the fiber preform response coupled with the resin flow. Niaki et al. [
17] developed a threephase integrated flowstress model. Li and Tucker [
18] reported a method to model the consolidation problem. Besides, Wysocki et al. [
19–
21] have modeled the coupled resin flow/perform deformation problems. As an extension, Rouhi et al. [
22–
25] presented a series of works based on the continuum mechanics framework.
In contrast to the rigid upper mold used in RTM processes, a plastic membrane is placed on top of the preform in the VARTM process. Thus, the preform deforms due to the difference between the internal and external pressure, which leads to thickness variations in final products. Due to this complexity, the VARTM process is more complicated to model than the RTM process. To simulate the VARTM process, Blais et al. [
26] modeled the process as StokesDarcy coupled problem. Andriamananjara et al. [
27] considered the effect of capillary pressure in their model. Besides, various studies on both resin flow and preform response were reported by researches e.g., [
28–
33]. However, to solve the full 3D fluid and solid problems, it demands enormous computational efforts. What’s more, it is also a challenge to mesh thin parts and keep the elemental skewness, aspect ratio and warpage in proper quality. On the other hand, the process optimization is an interesting topic for discussion. Hsiao et al. [
34] built an optimization framework of flow distribution arrangement by using genetic algorithms. From the industry point of view, the speed of the optimization is vital, which relies on the computational efficiency of the process model.
To simplify the LCM process model for thinwalled FRPCMs, it is assumed that the resin flow is confined to the inplane of the preform, and that the preform deforms solely along the normal of the mold. Consequently, the preform deformation is represented by a normal stretch variable. Based on the packing law [
35,
36], an explicit solution of the stretch is derived in terms of the fluid and atmosphere pressure. As a result, the LCM process is simplified to the 2D inplane resin flow in the 3D deformable preform. Also, inplane elements are used based on shell kinematics. The resulting shell model for resin flow and preform deformation in thinwalled process applications significantly reduces the number of degrees of freedom, while the primary physical phenomena of the process can still be represented. The model can be applied at the preliminary process design stage to help industries improving both efficiency and quality of the production. Lastly, the validity of assumptions and the capabilities of the model are illustrated through two numerical examples.
Mass and momentum conservations for nonsaturated porous media
Following the developments in [
15], we model the wetout process of the RTM based on the theory of porous media. A two phase porous media is considered, which consists of the solid fiber preform phase and the homogenized resin/gas fluid phase. Let
n
^{s} indicate the volume fraction of solid phase, whereas
n
^{f} represents the volume fraction of the (homogenized) fluid phase. So that
n
^{s} and
n
^{f} are interrelated through
where the liquid volume fraction
φ
^{l} and the gas volume fraction
φ
^{g} further subdivide the fluid volume fraction
n
^{f}. We introduce the saturation degree, 0 ≤
ξ ≤ 1, to indicate the case of partial saturation. We thus express the liquid and gas volume fraction in Eq.
1b in terms of
n
^{f} and
ξ as
The dry (
n
^{f} =
φ
^{g}) and fullsaturated (
n
^{f} =
φ
^{l}) cases are represented as
ξ → 0 and
ξ → 1, respectively. As shown in Fig.
1, the dry and fullsaturated parts are separated by a thin boundary, which indicates the flow front position where the gradient of saturation degree exists.
$$ \begin{array}{@{}rcl@{}} && n^{s}+n^{f} =1\text{ ,} \end{array} $$
(1a)
$$ \begin{array}{@{}rcl@{}} && n^{f} =\varphi^{l}+\varphi^{g} \text{ ,} \end{array} $$
(1b)
$$ \begin{array}{@{}rcl@{}} && \varphi^{l} =\xi n^{f}\text{ ,} \end{array} $$
(2a)
$$ \begin{array}{@{}rcl@{}} && \varphi^{g} =(1\xi )n^{f} \text{ .} \end{array} $$
(2b)
×
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Using Fig.
1, let us introduce the deformation mapping
x =
φ[
X] for the solid particles and
\(\boldsymbol {x}=\boldsymbol {\varphi }[\boldsymbol {X}]=\boldsymbol {\varphi }^{f}\left [\boldsymbol {X}^{f}\right ]\) for the fluid particles. The solid phase velocity and the homogenized fluid velocity are then obtained by virtue of the material time derivatives
where
\(D^{s}\bullet /D t=\dot {\bullet }\) and
D
^{f} ∙ /
D
t denote material time derivatives related to the solid reference configuration
B
_{0} and fluid reference configuration
\({B_{0}^{f}}\), respectively. Regarding solid particles, we introduce the deformation gradient
F and its Jacobian
J as
where ∇
_{X} is the material gradient operator with respect to the solid phase.
$$ \begin{array}{@{}rcl@{}} && \boldsymbol{v} =\frac{D^{s}\boldsymbol{\varphi }[\boldsymbol{X}]}{D t} = \dot{\boldsymbol{\varphi }}[\boldsymbol{X}] \text{ , } \end{array} $$
(3a)
$$ \begin{array}{@{}rcl@{}} && \boldsymbol{v}^{f} = \frac{D^{f}\boldsymbol{\varphi }^{f}\left[\boldsymbol{X}^{f}\right] }{D t}\text{ ,} \end{array} $$
(3b)
$$ \boldsymbol{F}=\boldsymbol{\varphi } \otimes \nabla_{X} \text{ with } J=\det [\boldsymbol{F}]>0\text{ ,} $$
(4)
From the principle of mass conservation, we find that the solid contents
M
^{s} =
J
n
^{s}
ρ
^{s} and fluid contents
M
^{f} =
J
n
^{f}
ρ
^{f} conserve as
where
ρ
^{s} and
ρ
^{f} are the intrinsic densities of the solid and fluid phases, respectively. In particular, the stationarity of
M
^{s} in Eq.
5a yields
\(n^{s}\rho ^{s}J ={n_{0}^{s}}{\rho _{0}^{s}}\), whereby the solid volume fraction is governed by
\(n^{s}=J^{1}{n_{0}^{s}}\), where ∙
_{0} represents the variable in the reference configuration.
$$ \begin{array}{@{}rcl@{}} && \dot{M}^{s} = 0\text{ , } \end{array} $$
(5a)
$$ \begin{array}{@{}rcl@{}} && \dot{M}^{f}+J\nabla \cdot \left( n^{f}\rho^{f}\boldsymbol{v}^{\textit{rf}}\right) = 0 \text{ ,} \end{array} $$
(5b)
Moreover, based on the arguments of homogenization, see [
15], we obtain the homogenized fluid density as
where
ρ
^{l} denotes the intrinsic density of the liquid (resin) that is assumed as incompressible;
ρ
^{g} is the intrinsic density of the compressible gas. Thus the mixture fluid density is considered as compressible.
$$ \rho^{f}=\xi \rho^{l}+(1\xi )\rho^{g} \text{ ,} $$
(6)
Considering the fluid mass flux
ρ
^{f}
v
^{f}, it can be expressed as a linear combination of the liquid and gas mass fluxes, scaled by the saturation degree,
Multiplying
v on both sides of Eq.
6, we obtain
ρ
^{f}
v =
ξ
ρ
^{l}
v + (1 −
ξ)
ρ
^{g}
v; subtracting this by Eq.
7, and introducing the homogenized relative fluid velocity
v
^{rf} :=
v
^{f} −
v, we obtain
$$ \rho^{f}\boldsymbol{v}^{f}=\xi \rho^{l}\boldsymbol{v}^{l}+(1\xi )\rho^{g}\boldsymbol{v}^{g} \text{ .} $$
(7)
$$ \rho^{f}\boldsymbol{v}^{\textit{rf}} = \xi \rho^{l}\boldsymbol{v}^{\textit{rl}}+(1\xi )\rho^{g}\boldsymbol{v}^{\textit{rg}} \text{ with } \boldsymbol{v}^{\textit{rl}} := \boldsymbol{v}^{l} \boldsymbol{v} \text{ and } \boldsymbol{v}^{\textit{rg}} := \boldsymbol{v}^{g}\boldsymbol{v} \text{ .} $$
(8)
$$ \rho^{f}\boldsymbol{v}^{\textit{df}}= \rho^{l}\boldsymbol{v}^{\textit{dl}}+\rho^{g}\boldsymbol{v}^{\textit{dg}}\text{ ,} $$
(9)
$$ \boldsymbol{v}^{\textit{df}} := n^{f}\boldsymbol{v}^{\textit{rf}} \text{ , } \boldsymbol{v}^{\textit{dl}} := \varphi^{l}\boldsymbol{v}^{\textit{rl}} \text{ , } \boldsymbol{v}^{\textit{dg}} := \varphi^{g}\boldsymbol{v}^{\textit{rg}} \text{ .} $$
(10)
(11)
$$ \dot{M}^{l}+J\nabla\cdot \left( \rho^{l}\boldsymbol{v}^{\textit{dl}}\right)=0 \text{ .} $$
(12)
Given the fact that the liquid resin phase is incompressible, Eq.
12 can be formulated as an evolution equation of the saturation degree, see also [
22] and [
15],
Finally, from quasistatic momentum conservation of the mixture porous media, the linear momentum balance yields
where
\(\hat {\rho }=n^{s}\rho ^{s}+n^{f}\rho ^{f}\), and the total stress
\(\hat {\boldsymbol {\sigma }}\) relates to the effective (constitutive) stress
σ of the fiber network and the fluid pressure
p, viz., Terzaghi effective stress principle,
From ref.
15, it implies that the deviatoric parts of total stress and effective stress are same, i.e.,
\(\hat {\boldsymbol {\sigma }}_{dev} =\boldsymbol {\sigma }_{dev}\), whereby the total pressure
\(\hat {p}\) is obtained as the summation of the fluid pressure
p and the effective pressure
p
^{e} as
As to the fluid stress response, it is assumed that the fluid is ideal with negligible shear stress. Thereby the intrinsic fluid stress is represented by the fluid pressure
p, which is homogenized between the pressures of the liquid resin and the gas. It follows from the homogenization in [
15], that the (mixture) fluid pressure is an interaction in the degree of saturation
ξ between the intrinsic liquid and gas pressures (
p
^{l} and
p
^{g}) written as
(13)
(14)
$$ \hat{\boldsymbol{\sigma}} = \boldsymbol{\sigma}  p \boldsymbol{1} \text{ .} $$
(15)
$$ \hat{p} =p^{e} +p \text{ .} $$
(16)
$$ p=\xi p^{l}+(1\xi )p^{g} \text{ .} $$
(17)
Preform deformation and resin flow analysis
In this section, we consider the LCM process of a deformable thinwalled preform resting on a fixed lower surface. The preform undergoes the atmospheric pressure
p
^{a} through a flexible membrane, as shown in Fig.
2a. Given the nature of a thinwalled preform, it is considered as a single director shell surface Ω
_{0} with the unit normal
N as indicated in both Figs.
1 and
2b, see also [
37]. Under the pressure loading in Fig.
2a, we shall assume that the preform can compress or expand only along the normal
N via the thickness stretch defined as
where
h is the current thickness of the preform whereas
h
_{0} is the undeformed thickness. It is also assumed that the fluid pressure
p and the saturation degree
ξ keep constant along the thickness direction. We thereby simplify the 3D Darcy flow to the inplane flow in an arbitrary curved surface Ω.
$$ {{\lambda := \frac {h} {h_{0}}}} \text{ ,} $$
(18)
Geometry of the thinwalled pressure loaded preform
In order to define the geometry of the thinwalled pressure loaded preform, its current geometry
B is assumed to deform solely with the normal stretch
λ in Eq.
18 so that
B =
B[
λ]. The normal stretch field is parameterized in the curvelinear coordinates
\(\left (\theta ^{1},\theta ^{2},\theta ^{3}=\theta \right )\) in Fig
2b defined as
where the initial position vector
\(\boldsymbol {\Phi }\left [\theta ^{1},\theta ^{2}\right ]\) defines material points on the lower surface Ω
_{0} of the preform. Next, based on the assumption that only normal direction deformation is allowed, the current geometry
B[
λ] is defined in terms of the normal stretch on Ω
_{0} as
In particular, the initial undeformed geometry
B
_{0} =
B[1] is obtained as
From Eq.
21, we find that
where the covariant basis vectors (inplane
G
_{α} and outofplain
N) are defined as
where
α = 1,2 and
\(\boldsymbol {G}_{3}=\boldsymbol {G}^{3}=\boldsymbol {N}\), and the curvature of the preform
K
_{αβ} is defined as
Moreover, in Eq.
23 we introduced the contravariant basis vectors
G
^{i} (
i = 1,2,3), which are defined from the identity relationship
where
G
_{ij} is the metric tensor. Finally, the infinitesimal area element
\(\mathop {} \mathrm {d} A\) on the Ω
_{0} and volume element
\(\mathop {} \mathrm {d} V\) in the
B
_{0} are formulated in the curvelinear coordinates as
Likewise, from the current geometry in Eq.
20 and the curvelinear coordinates of the preform, we identify the deformation gradient from the linearization
where the covariant basis vectors are identified as
In the following, let us assume that bending effects of the preform can be neglected corresponding to (
λ
N)
_{, α} ≈
0 and
K
_{αβ} ≈
0, see [
37]. Consequently, we can obtain
g
_{α} =
G
_{α}, whereby the deformation gradient of the preform is simplified to
where
\(\overline {\boldsymbol {1}}\) and
\(\boldsymbol {1} = \overline {\boldsymbol {1}}+ \boldsymbol {N} \otimes \boldsymbol {N}\) are the inplane and 3D identity tensor respectively. From Eq.
29, it follows that the normal stretch
λ is the Jacobian of the deformation gradient
\(\lambda = J=\det \boldsymbol F\).
$$ \lambda [\boldsymbol{X}_{0}]>0 \forall \boldsymbol{X}_{0}\in {\Omega}_{0} \text{ with } {\Omega}_{0}=\left\{\boldsymbol{X}_{0}=\boldsymbol{\Phi }\left[\theta^{1},\theta^{2}\right] ,\text{}\left[\theta^{1},\theta^{2}\right] \in \mathcal{A}\right\} \text{ ,} $$
(19)
$$ B[\lambda ]=\left\{\boldsymbol{x}=\boldsymbol{\Phi }\left[\theta^{1},\theta^{2}\right]+\theta \lambda \left[\theta^{1},\theta^{2}\right] \boldsymbol{N}\left[\theta^{1},\theta^{2}\right] \text{ , }\left[\theta^{1},\theta^{2}\right] \in \mathcal{A} \text{ and } \theta \in [0,h_{0}]\right\}\text{ ,} $$
(20)
$$ B_{0}=\left\{\boldsymbol{X}=\boldsymbol{\Phi }\left[\theta^{1},\theta^{2}\right]+\theta \boldsymbol{N}\left[\theta^{1},\theta^{2}\right] \text{ with } \left[\theta^{1},\theta^{2}\right] \in \mathcal{A} \text{ and } \theta \in [0,h_{0}]\right\} \text{ .} $$
(21)
$$ d \boldsymbol{X}= \boldsymbol{G}_{\alpha }\left[\theta^{1},\theta^{2}\right]d\theta^{\alpha }+\boldsymbol{N}\left[\theta^{1},\theta^{2}\right]d\theta=\left( \boldsymbol{G}_{\alpha }\otimes \boldsymbol{G}^{\alpha }+\boldsymbol{N}\otimes \boldsymbol{N}\right)\cdot d \boldsymbol{X} \text{ ,} $$
(22)
$$ \boldsymbol{G}_{\alpha }=\frac{\partial \boldsymbol{\Phi }}{\partial\theta^{\alpha}}+\theta \frac{\partial \boldsymbol{N}}{\partial \theta^{\alpha}}= \frac{\partial \boldsymbol{\Phi }}{\partial\theta^{\alpha}}\theta K_{\alpha\beta}\boldsymbol{G}^{\beta} \text{ , } $$
(23)
$$ K_{\alpha \beta} = \frac{\partial \boldsymbol{G}_{\alpha}}{\partial \theta^{\beta}}\cdot \boldsymbol{N} =  \frac{\partial \boldsymbol{N}}{\partial \theta^{\beta}}\cdot \boldsymbol{G}_{\alpha} \text{ .} $$
(24)
$$ \boldsymbol{1} = \underbrace{ \frac{\partial \boldsymbol{X}}{\partial \theta^{i}} }_{\boldsymbol{G}_{i}} \otimes \underbrace{ \frac{\partial \theta^{i}}{\partial \boldsymbol{X}} }_{\boldsymbol{G}^{i}} = \boldsymbol{G}_{i}\otimes \boldsymbol G^{i} \leadsto \boldsymbol{G}^{j}= G^{ij} \boldsymbol{G}_{i} \text{ with } G^{ij} =\boldsymbol{G}^{i} \cdot \boldsymbol{G}^{j} \text{ ,} $$
(25)
$$ \begin{array}{@{}rcl@{}} \mathop{} \mathrm{d} A & =& \left\boldsymbol{G}_{1}\times \boldsymbol{G}_{2}\right d\theta^{1} d\theta^{2} = \sqrt{G} d\theta^{1} d\theta^{2} \text{ , } \end{array} $$
(26a)
$$ \begin{array}{@{}rcl@{}} \mathop{} \mathrm{d} V & =& \left( \boldsymbol{G}_{1} \times \boldsymbol{G}_{2}\right)\cdot \boldsymbol{N} d\theta^{1} d\theta^{2} d\theta^{3} = \sqrt{G} d\theta^{1} d\theta^{2} d\theta \text{ .} \end{array} $$
(26b)
$$ \mathop{} \mathrm{d} \boldsymbol{x}= \left( \frac{\partial \boldsymbol{\Phi }}{\partial \theta^{\alpha}}+ \theta \frac{\partial \left( \lambda \boldsymbol{N}\right) }{\partial \theta^{\alpha}}\right) d\theta^{\alpha }+ \lambda \boldsymbol{N}\boldsymbol{ } d\theta =(\boldsymbol{g}_{i}\otimes \boldsymbol{G}^{i})\cdot d \boldsymbol{X} = \boldsymbol{F}\cdot d \boldsymbol{X} \text{ ,} $$
(27)
$$ \begin{array}{@{}rcl@{}} \boldsymbol{g}_{\alpha} & =& \frac{\partial \boldsymbol{\Phi }}{\partial \theta^{\alpha}}+ \theta \frac{\partial \left( \lambda \boldsymbol{N}\right) }{\partial \theta^{\alpha}} \text{ with } \alpha =1,2 \text{ ,}\\ \boldsymbol{g}_{3} & =& \lambda \boldsymbol{N} \text{ .} \end{array} $$
(28)
$$ \begin{array}{@{}rcl@{}} \boldsymbol{F} &=& \boldsymbol{g}_{i} \otimes \boldsymbol{G}^{i}\\ &=& \boldsymbol{G}_{\alpha} \otimes \boldsymbol{G}^{\alpha } + \lambda \boldsymbol{N}\otimes \boldsymbol{N}\\ &=& \overline{\boldsymbol{1}} + \lambda \boldsymbol{N}\otimes \boldsymbol{N}\\ &=& \boldsymbol{1}+(\lambda 1)\boldsymbol{N}\otimes \boldsymbol{N}\\ &&\text{with}\ i=1,2,3;\ \alpha =1,2 \text{ ,} \end{array} $$
(29)
×
Inplane resin flow in thinwalled preform
To describe 2D LCM wetout process of the thinwalled preform, we consider the fluid resin flow in
B
_{0} as an inplane flow that is projected to the surface Ω
_{0}. To this end, the following form of the divergence theorem is considered for the fluid flow
where
\(\overline {\boldsymbol {\nabla }}\) is the inplane gradient operator,
\(\overline {\boldsymbol {N}}\) is the outward unit normal of the boundary line Γ
_{0} on the surface Ω
_{0} (in Fig.
1), and
\(\overline {\boldsymbol {v}}^{\textit {df}}\) is the inplane fluid Darcy velocity. Please note that the second order tensors and vectors in Ω
_{0} satisfy the orthogonality properties, e.g.,
\(\overline {\boldsymbol {v}}^{\textit {df}}\cdot \boldsymbol {N}=0\), and
\(\overline {\boldsymbol {N}}\cdot \boldsymbol {N}=0\), see also [
38]. In view of Eq.
30, we therefore obtain the inplane pressure gradient Grad
p as
$$ {\int}_{B_{0}}\boldsymbol{\nabla} \cdot \boldsymbol{v}^{\textit{df}}\mathop{} \mathrm{d} V= h_{0}{\int}_{{\Omega}_{0}} \overline{\boldsymbol{\nabla}} \cdot \overline{\boldsymbol{v}}^{\textit{df}}\mathop{} \mathrm{d} A = h_{0}{\int}_{{\Gamma}_{0}}\overline{\boldsymbol{N}}\cdot \overline{\boldsymbol{v}}^{\textit{df}}\mathop{} \mathrm{d} S \text{ ,} $$
(30)
$$ \begin{array}{@{}rcl@{}} \text{Grad} p := \overline{\boldsymbol{\nabla}} p = \frac{\partial p}{\partial \theta^{\alpha }}\frac{\partial \theta^{\alpha }}{\partial {\boldsymbol{X}} }= p_{,\alpha }\boldsymbol{G}^{\alpha } \text{ .} \end{array} $$
(31)
Constitutive relations
Fiber packing law
Considering the mechanical behavior of the deformable fiber preform during the LCM process, a major mechanism is the fiber packing induced by applied pressure. Thus, we consider the Toll’s model [
35], which is an exponential law in terms of the fiber volume fraction
n
^{s}. In the present model, we limit the analysis to hyperelastic with the stored free energy defined as
$$ \psi [J]=\frac{k^{s}E}{m1} \left( n^{s}\right)^{m}\left( J+m(J1)J^{m}J^{m+1}\right) \text{ with } n^{s}=\frac{{n_{0}^{s}}}{J} \text{ ,} $$
(32)
$$ p^{e}=\frac{\partial \psi }{\partial J}=k^{s}E \left( \frac{{n_{0}^{s}}}{J}\right)^{m} \left( 1J^{m}\right)\text{ .} $$
(33)
×
Inplane Darcy flow
As to the Darcy flow, we postulate that the 3D flow is simplified to an effective 2D flow by ignoring the throughthickness flow, whose transformation is defined by Eq.
30 as
where
K
^{α} is the permeability of the preform relating to the liquid/gas transportation. As suggested by Gebart [
39], in turn,
K
^{α} is defined in terms of the intrinsic permeability
\(\hat {\boldsymbol {k}}\), the viscosity of the liquid resin/gas
μ
_{α} and the relative permeabilitties
k
_{rα} as according to Burdine [
40] are defined as
Regarding the intrinsic permeability tensor
\(\hat {\boldsymbol {k}}\), for simplicity, we consider the isotropic permeability represented by
\(\hat {\boldsymbol {k}}=\hat {k}\boldsymbol {1}\). Here,
\(\hat {k}\) is the deformation dependent isotropic permeability, whose deformation dependence is assumed to follow the KozenyCarman equation, see also [
39]. Thereby, the permeability is obtained in terms of the fiber volume fraction
n
^{s} as
where
r
_{s} is the particle (or fiber bundle) radius, and
C is the Kozeny constant. From that, we can derive the relation between the deformed preform permeability
\(\hat {k}\) and the undeformed preform permeability
\(\hat {k}_{0}\) as
Moreover, by virtue of Eq.
30 and the derivations in [
15], the inplane gradients of the liquid and gas pressure in Eq.
34 are obtained as functions of capillary pressure
p
^{c}, fluid pressure
p and saturation degree
ξ,
We thus conclude that the inplane Darcy law for the liquid transportation is expressed as
and for the gas transportation we obtain
Combining Eqs.
10,
39 and
40, we now obtain the homogenized fluid Darcy velocity as
where the mixture permeabilities
\({K_{p}^{f}}\) and
\(K_{\xi }^{f}\) are obtained as
$$ \begin{array}{@{}rcl@{}} {\overline{\boldsymbol{v}}}^{\textit{dl}} & =& \varphi^{l} {\overline{\boldsymbol{v}}}^{\textit{rl}} =  K^{l} \overline{\boldsymbol{\nabla}} p^{l} \text{ , }\\ {\overline{\boldsymbol{v}}}^{\textit{dg}} & =& \varphi^{g}{\overline{\boldsymbol{v}}}^{\textit{rg}} =  K^{g} \overline{\boldsymbol{\nabla}} p^{g} \text{ , }\\ K^{\alpha } & =& \left\{ k_{r \alpha} \frac{ \hat{\boldsymbol{ k}} } {\mu_{\alpha }} \right\}_{\alpha =l,g} \text{ , } \end{array} $$
(34)
$$ \begin{array}{@{}rcl@{}} k_{\textit{rl}} & =& \xi^{3+\frac{2}{n_{b}}} \text{ , } \\ k_{\textit{rg}} & =& (1\xi )^{2}\left( 1\xi^{1+\frac{2}{n_{b}}}\right) \text{ .} \end{array} $$
(35)
$$ \hat{k}=\frac{r_{s}}{4~C}\frac{\left( 1n^{s}\right)^{3}}{n^{s}} \ \text{ with } n^{s}=\frac{{n_{0}^{s}}}{J} \text{ ,} $$
(36)
$$ \frac{\hat{k}_{0}}{\hat{k}}=\frac{(1{n^{s}_{0}})^{3}}{(1\frac{{n_{0}^{s}}}{J})^{3}}\mathop \frac{\frac{{n_{0}^{s}}}{J}}{{n_{0}^{s}}}={J^{2} \left( \frac{1{n_{0}^{s}}}{J{n_{0}^{s}}}\right)^{3}=\frac{1}{J}\left( \frac{{n_{0}^{f}}}{n^{f}}\right)^{3} \leadsto {\hat{k} = \hat{k}_{0} J\left( \frac{n^{f}}{{n_{0}^{f}}}\right)^{3}}} \text{ .} $$
(37)
$$ \begin{array}{@{}rcl@{}} &&\overline{\boldsymbol{\nabla}} p^{l} = \overline{\boldsymbol{\nabla}} p+\left( 1(1\xi ) \log_{{, \xi}}\left[p^{c}\right]\right)p^{c} \overline{\boldsymbol{\nabla}} \xi \text{ , } \\ &&\overline{\boldsymbol{\nabla}} p^{g} = \overline{\boldsymbol{\nabla}} p + \left( 1+\xi \log_{{, \xi}}\left[p^{c}\right]\right)p^{c} \overline{\boldsymbol{\nabla}} \xi \text{ .} \end{array} $$
(38)
$$ \begin{array}{@{}rcl@{}} &&{\overline{\boldsymbol{v}}}^{\textit{dl}} = {K_{p}^{l}} \overline{\boldsymbol{\nabla}} p  K_{\xi }^{l} \overline{\boldsymbol{\nabla}} \xi \ \text{ with, } \\ &&{K_{p}^{l}} = K^{l} \ \text{ and, }\\ &&K_{\xi }^{l} = K^{l} \left( 1(1\xi ) \log_{,\xi }\left[p^{c}\right]\right)p^{c} \text{ , } \end{array} $$
(39)
$$ \begin{array}{@{}rcl@{}} &&{\overline{\boldsymbol{v}}}^{\textit{dg}} = {K_{p}^{g}} \overline{\boldsymbol{\nabla}} p  K_{\xi }^{g} \overline{\boldsymbol{\nabla}} \xi \ \text{ with, } \\ &&{K_{p}^{g}} = K^{g} \ \text{ and, } \\ &&K_{\xi }^{g} = K^{g}\left( 1+\xi \log_{,\xi }\left[p^{c}\right]\right)p^{c} \text{ .} \end{array} $$
(40)
$$ {\overline{\boldsymbol{v}}}^{\textit{df}} = \frac{\rho^{l}}{\rho^{f}}{{\overline{\boldsymbol{v}}}}^{\textit{dl}} + \frac{\rho^{g}}{\rho^{f}}{{\overline{\boldsymbol{v}}}}^{\textit{dg}}= {K_{p}^{f}} \overline{\boldsymbol{\nabla}} p  K_{\xi }^{f} \overline{\boldsymbol{\nabla}}\xi \text{ ,} $$
(41)
$$ \begin{array}{@{}rcl@{}} {K_{p}^{f}} & =&\frac{\rho^{l}}{\rho^{f}} {K_{p}^{l}}+\frac{\rho^{g}}{\rho^{f}}{K_{p}^{g}} \text{ , } \\ K_{\xi }^{f} & =&\frac{\rho^{l}}{\rho^{f}}K_{\xi }^{l}+\frac{\rho^{g}}{\rho^{f}}K_{\xi }^{g} \text{ .} \end{array} $$
(42)
Capillary pressure and universal gas law
The capillary pressure in Eqs.
38 to
40 represents the difference between the gas and liquid pressure, we apply the phenomenological model by Brooks [
41]
where
p
^{ent} > 0 denotes the entry pressure and
n
_{b} > 0 controls the shape of the capillary curve. By combining Eqs.
43 and
17, the intrinsic pressures of liquid and gas are obtained completely in terms of fluid pressure
p and saturation degree
ξ as
As to the compressible gas density
ρ
^{g}, the universal gas law shows
where
R is the universal gas constant and
T is the absolute temperature.
$$ p^{c}[\xi]=p^{g}\boldsymbol{}p^{l} = p^{ent} \xi^{\frac{1}{n_{b}}} \text{ ,} $$
(43)
$$ \begin{array}{@{}rcl@{}} p^{l} & =&p(1\xi )p^{c}[\xi ] \text{ ,} \\ p^{g} & =&p+\xi p^{c}[\xi ] \text{ .} \end{array} $$
(44)
$$ \rho^{g}=k^{g}p^{g}=k^{g}\left( p+\xi p^{c}[\xi ]\right) \text{ with } k^{g}=\frac{m^{g}}{R T} \text{ ,} $$
(45)
Boundary value problems
To solve the present process model, we introduce the mass balance relations Eqs.
11 and
13 and the quasistatic momentum balance Eq.
14 in weak form. The weak forms are formulated in terms of the shell kinematics and the coordinate systems introduced in “
Geometry of the thinwalled pressure loaded preform”. From “
Fiber packing law”, we also notice that it suffices to represent deformation gradient
F and its Jacobian
\(J=\det [ \boldsymbol {F} ]\) by the stretch field
\(\lambda \in \mathcal L_{2} [{\Omega }_{0}]\). So the present model aims to solve the fields of fluid pressure
p, saturation degree
ξ and stretch
λ.
Weak form of momentum balance
The weak form of the momentum balance Eq.
14 is equivalent to the principle of virtual work, which is formulated in the reference configuration
B
_{0} and in the absence of the gravitational force as
where
\(\bar {\boldsymbol {t} }_{1}\) is the nominal traction vector acting on a surface element
\(\mathop {} \mathrm {d} A \in {\Omega }_{0}\). In particular,
\(\boldsymbol {N}\cdot \bar {\boldsymbol {t} }_{1} :=  p^{a}\) is the prescribed atmospheric pressure at the top surface of the preform, as shown in Fig.
2a. We also introduced the symmetric total second PiolaKirchhoff stress
\(\hat {\boldsymbol {S}}\) from the pullback transformation of the total Cauchy stress
\(\hat {\boldsymbol {S}} =J \boldsymbol {F}^{1}\cdot \hat {\boldsymbol {\sigma }} \cdot \boldsymbol {F}^{t}\). By implementing the Terzaghi stress principle Eq.
15, we obtain
$$ {\int}_{B_{0}} \hat{\boldsymbol{S}} \colon \delta \boldsymbol{E} \mathop{} \mathrm{d} V = {\int}_{B_{0}} \left( \boldsymbol{S}  J p \boldsymbol{C}^{1} \right) \colon \left( \delta \boldsymbol{F}^{t}\cdot \boldsymbol{F}\right) \mathop{} \mathrm{d} V = h_{0} {\int}_{{\Omega}_{0}} \boldsymbol{N}\cdot \bar{\boldsymbol{t} }_{1} \delta \lambda \mathop{} \mathrm{d} A \ \ \forall \delta \lambda \text{ ,} $$
(46)
$$ \hat{\boldsymbol{S}} = J \boldsymbol{F}^{1}\cdot (\boldsymbol{\sigma}  p\boldsymbol{1})\cdot \boldsymbol{F}^{t} = \boldsymbol{S}  J p \boldsymbol{C}^{1} \text{ with } \boldsymbol{S} =J \boldsymbol{F}^{1}\cdot \boldsymbol{\sigma} \cdot \boldsymbol{F}^{t} \text{ ,} $$
(47)
As mentioned in Eq.
29, the deformation gradient simplifies to
consequently, the packing law Eq.
32 yields the effective stress response as
Moreover, we also obtain the explicit expressions for the right CauchyGreen deformation
C =
F
^{t} ⋅
F and its inverse
C
^{− 1} from Eq.
48
where the last equality was obtained using the ShermanMorrison formula.
$$ \boldsymbol{F}=\boldsymbol{1}+(\lambda 1)\boldsymbol{N} \otimes \boldsymbol{N} \text{ with } \lambda = J = \det [ \boldsymbol{F} ] \text{ ,} $$
(48)
$$ \boldsymbol{S} = 2\frac{\partial \psi }{\partial \boldsymbol{C}} = p^{e} J \boldsymbol{C}^{1} = p^{e} \lambda \boldsymbol{C}^{1} \text{ .} $$
(49)
$$ \begin{array}{@{}rcl@{}} && \boldsymbol{C} = \boldsymbol{1}+\left( \lambda^{2}1\right)\boldsymbol{N} \otimes \boldsymbol{N} \text{ ,} \end{array} $$
(50a)
$$ \begin{array}{@{}rcl@{}} && \boldsymbol{C}^{1} = \boldsymbol{1}+\left( \lambda^{2}1\right) \boldsymbol{N} \otimes \boldsymbol{N} \text{ ,} \end{array} $$
(50b)
$$ \begin{array}{@{}rcl@{}} {\int}_{B_{0}} \left( \delta \boldsymbol{F}^{t}\cdot \boldsymbol{F}\right)\colon \left( \boldsymbol{S}J p \boldsymbol{C}^{1}\right)\mathop{} \mathrm{d} V & =& {\int}_{B_{0}} \left( \boldsymbol{N} \otimes \boldsymbol{N}\right) \colon \left( \boldsymbol{S}\lambda p \boldsymbol{C}^{1}\right) \lambda \delta \lambda \mathop{} \mathrm{d} V \\ & = & {\int}_{B_{0}} \left( \boldsymbol{N} \cdot \boldsymbol{ S} \cdot \boldsymbol{ N}  \boldsymbol{N} \cdot \boldsymbol{C}^{1} \cdot \boldsymbol{N} \lambda p \right) \lambda \delta \lambda \mathop{} \mathrm{d} V \\ &=& {\int}_{B_{0}} \left( p^{e}  p \right) \boldsymbol{N} \cdot \boldsymbol{C}^{1} \cdot\boldsymbol{N} \lambda^{2} \delta \lambda \mathop{} \mathrm{d} V \\ &=& {\int}_{B_{0}} \left( p^{e}  p \right) \lambda^{2} \lambda^{2} \delta \lambda \mathop{} \mathrm{d} V \\ &=&  h_{0}{\int}_{{\Omega}_{0}}\left( p^{e}+ p\right) \delta \lambda \mathop{} \mathrm{d} A \\ &=& h_{0}{\int}_{{\Omega}_{0}} \boldsymbol{N}\cdot {\bar{\boldsymbol{t}}}_{1} \delta \lambda \mathop{} \mathrm{d} A \\ &=&h_{0}{\int}_{{\Omega}_{0}} p^{a} \delta \lambda \mathop{} \mathrm{d} A \text{ .} \end{array} $$
(51)
Hence, we find that the applied pressure
p
^{a} balances with the effective and the fluid pressures,
p
^{e} and
p. From this balance relationship together with the constitutive relation Eq.
33, relating the effective pressure
p
^{e} and the stretch
λ, we obtain
whereby the normal stretch field can be resolved explicitly from the hyperelastic fiber packing law as
$$ p^{e} [ \lambda ] = k^{s}E \left( {n_{0}^{s}}\right)^{m} \left( \lambda^{m}1\right) = p^{a}  p \text{ ,} $$
(52)
(53)
Weak formulation of mass balance
Let’s consider the inplane flow in “
Inplane Darcy flow” on the surface Ω
_{0} that is bounded by Γ
_{0}. We introduce the test functions for the fields of fluid pressures and saturation degrees as
where we prescribe the fluid pressure and the saturation degree along the boundaries
∂
_{p}Ω
_{0} and
∂
_{ξ}Ω
_{0}, which satisfy that
\(\left (\partial _{p} {\Omega }_{0} \cup \partial _{\xi } {\Omega }_{0}\right ) \subset {\Gamma }_{0}\). By using the relation
J =
λ in Eqs.
11 and
13, we thus obtain the weak form of the pressure and saturation equation projected onto the surface Ω
_{0} as
$$ \begin{array}{@{}rcl@{}} && P=\left\{\eta [x]\in \mathcal{H}^{1}[{\Omega}_{0}]  \eta=0 \text{ on } \partial_{p} {\Omega}_{0}\right\}\text{ , }\\ && S=\left\{\chi [x]\in \mathcal{H}^{1}[{\Omega}_{0}]  \chi=0 \text{ on } \partial_{\xi} {\Omega}_{0} \right\}\text{ ,}\ \end{array} $$
(54)
$$ \begin{array}{@{}rcl@{}} h_{0}{\int}_{{\Omega}_{0}}\left( \eta \left( \dot{\lambda }\rho^{f} + \left( \lambda {n_{0}^{s}})\right) \left( \left( \rho^{l}\rho^{g}\right)\dot{\xi } + (1\xi )\dot{\rho}^{g} \right)\right)  \lambda \rho^{f} \overline{\boldsymbol{\nabla}} \eta \cdot {\overline{\boldsymbol{v}}}^{\textit{df}} \right)\mathop{} \mathrm{d} A\\ = h_{0} {\int}_{{\Gamma}_{0}} \eta Q \mathop{} \mathrm{d} S \quad \forall \eta \in P \text{ ,} \end{array} $$
(55)
$$ \begin{array}{@{}rcl@{}} h_{0}{\int}_{{\Omega}_{0}} \left( \chi \left( \left( \lambda {n_{0}^{s}} \right) \dot \xi + \xi \dot{J} \right)  \lambda \overline{\boldsymbol{{\nabla}}}\chi \cdot {\overline{\boldsymbol{v}}}^{\textit{dl}} \right) \mathop{} \mathrm{d} A = h_{0} {\int}_{{\Gamma}_{0}} \chi H \mathop{} \mathrm{d} S \quad \forall \chi \in S \text{ ,} \end{array} $$
(56)
where
\(Q={\overline {\boldsymbol {N}}} \cdot \overline {\boldsymbol {v}}^{\textit {df}}\),
\(H={\overline {\boldsymbol {N}}}\cdot \overline {\boldsymbol {v}}^{\textit {dl}}\), which are the inplane fluxes across the boundary Γ
_{0}.
FE interpolations
The weak forms Eqs.
55 and
56 are solved by the finite element method, which is stabilized by the streamline upwind/PetrovGalerkin (SUPG) method, as discussed in [
15]. The domain Ω
_{0} is discretized by bilinear fournode element. The primary variables
p and
ξ are interpolated as nodal summation forms,
where
\(\left \{N^{I}\right \}{}_{I=1,...,\text {NNO}}\) are shape functions, and
ξ
^{I} and
p
^{I} are the timedependent nodal saturation degree and fluid pressure respectively. Furthermore, we obtain the discretized inplane gradient from Eq.
57 as
$$ \begin{array}{@{}rcl@{}} p\leadsto p_{h}[ \boldsymbol{X} ,t] & =& \sum\limits_{I=1}^{\text{NNO}} N^{I}[ \boldsymbol{X} ] p^{I}[t] \text{ , } \eta [ \boldsymbol{X} ] \leadsto \eta_{h}[ \boldsymbol{X} ]\text{ ,} \\ \xi \leadsto \xi_{h}[ \boldsymbol{X} , t ] & =&\sum\limits_{I=1}^{\text{NNO}} N^{I}[ \boldsymbol{X} ] \xi^ I [t] \text{ , } \chi [ \boldsymbol{X} ]\leadsto \chi_{h}[ \boldsymbol{X} ] \text{ , } \end{array} $$
(57)
$$ \begin{array}{@{}rcl@{}} \overline{\boldsymbol{\nabla}} \xi & \leadsto& \overline{\boldsymbol{\nabla}} \xi_{h} =\sum\limits_{I=1}^{\text{NNO}} \overline{\boldsymbol{\nabla}} N^{I}[ \boldsymbol{X} ] \xi^{I}[t] \text{ , }\\ \overline{\boldsymbol{\nabla}} p & \leadsto& \overline{\boldsymbol{\nabla}} p_{h} =\sum\limits_{I=1}^{\text{NNO}} \overline{\boldsymbol{\nabla}} N^{I}[ \boldsymbol{X} ] p^{I}[t] \text{ , } \end{array} $$
(58)
According to the Eq.
53, we can write out the elemental stretch
λ
^{el} as
Hence, the nodal stretch can be calculated from the average of neighboring elements,
where
NE denotes the number of elements that is adjacent to
λ
^{I}. Thus, the field
λ is interpolated as
$$ \lambda^{el}= \left( 1+\frac{p^{a}  \displaystyle{\sum\limits_{i=1}^{4}} N^{i}[x] p^{i}[t]}{ k^{s} E ({n_{0}^{s}})^{m}}\right)^{1/m} \text{ .} $$
(59)
$$ \lambda^{I}= \frac{1}{\text{NE}}\sum\limits_{I=1}^{\text{NE}} \lambda^{el}_{I} \text{ ,} $$
(60)
$$ \lambda \leadsto \lambda_{h}[ \boldsymbol{X} ,t] = \sum\limits_{I=1}^{\text{NNO}} N^{I}[ \boldsymbol{X} ] \lambda^{I}[t] \text{ .} $$
(61)
Numerical examples
Two representative examples are presented to validate the 2D assumptions and demonstrate the model. Table
1 lists the parameters used in both examples. At the infusion inlet, the pressure is set to
p
_{0} = 1 atm and the corresponding saturation degree is given as
ξ
_{0} = 1.0. At the outlet, the boundary conditions are determined by
p
_{1} = 3.2 mbar and
∂
_{x}
ξ = 0; the initial values are set to
^{0}
ξ =
ξ(
x,0) = 0.001 and
^{0}
p =
p(
x,0) = 3.2 mbar. Ideally, the initial field
^{0}
ξ is very close to zero, but numerical singularity problems appear when
^{0}
ξ is chosen too small. Thus the current value of
^{0}
ξ has been chosen small enough, while it avoids numerical singularity.
Table 1
Parameters of the fiber preform, resin and environment
Parameters

Unit

Identification

Value


\({n^{s}_{0}}\)

–

Fiber volume fraction

0.411

\(\hat {k}_{0}\)

[
m
^{2}]

Intrinsic permeability

2.537× 10
^{− 9}

ρ
^{l}

[
k
g/
m
^{3}]

Resin density

1010

μ
_{l}

[
P
a ⋅
s]

Resin viscosity

0.1

μ
_{g}

[
P
a ⋅
s]

Gas viscosity

1.983× 10
^{− 5}

n
_{b}

–

Capillary pressure constant

1.9

p
^{ent}

[
P
a]

Entry pressure

0.134 × 10
^{6}

m
^{g}

[
k
g/
m
o
l]

Gas molar mass

2.897 × 10
^{− 2}

R

[
J/
K ⋅
m
o
l]

Ideal gas constant

8.314

T

[
K]

Absolute temperature

293

k
^{s}

–

Packing law factor

0.01

E

[
P
a]

Young’s modulus of fibers

7.0 × 10
^{10}

m

–

Packing law exponent

15

Comparison of the resin flow in thick and thinwalled fiber preforms
To verify the inplane flow assumption in thinwalled preforms, we studied two different models when the preform is considered fixed with
λ = 1. The considered preform is a curved tunnel that starts and ends with a 0.2 meters long straight path to steady the flow; there is an 0.8 meters radius curve in between that introduces an unevenly distributed throughthickness flow as shown in Fig.
4. Following [
15], a 2D model is first made for capturing both the inplane and throughthickness resin flow of the curved preform in Fig. 4a. Second, a 3D shell model is built for the same geometry; however; because there is no flow along the transverse and throughthickness direction of the preform, the flow can be considered as 1D in the longitudinal direction, as shown in Fig.
4b. The infusion starts from the inlet and ends at the outlet as depicted in Fig.
4. In order to study the influence of the through the thickness flow as induced by the curved preform, a global saturation degree measure
\(\tilde {\xi }\) is introduced to represent overall significance of the through the thickness flow effect. The measure
\(\tilde {\xi }\) is defined as
where the
NNO is the number of nodes, and the
ξ
^{i} denotes the saturation degree at the
i th node.
$$ \tilde{\xi}=\frac{{\sum}_{i=1}^{NNO} \xi^{i}}{NNO}\text{ ,} $$
(62)
×
By comparing the
\(\tilde {\xi }\) in the 2D plane and shell models, we thus measure the importance of the throughthickness flow for various thickness to length ratios,
t/
L, of the preform. The thickness
t varies among 0.05, 0.1, 0.15 and 0.2 meters. For each
t/
L case, the global saturation degree
\(\tilde {\xi }\) is computed and compared between two models. For the very thick preform
t/
L = 12
%, Fig.
4a shows the unevenly distributed throughthickness flow for the 2D plane model, i.e., due to the curved geometry the inner radius flow is faster than the outer radius flow. Figure
5 shows that the percent error,
\(\delta =\left  \left (\overline {\boldsymbol {\xi }}_{plane}\overline {\boldsymbol {\xi }}_{shell}\right ) / {\overline {\boldsymbol {\xi }}_{shell}}\right  \times 100\%\), decreases linearly as the preform thickness decreases. When the ratio
t/
L is reduced below 6
%, the throughthickness flow effect is significantly reduced. For example, a thin preform of
t/
L = 3
% yields a difference of 1.5
%, which justifies the inplane flow assumption made for the present thinwalled case.
×
LCM process of doubly curved thinwalled preform
To investigate the capabilities of the proposed model for simulating the infusion of a deformable thinwalled preform, we consider a LCM process example as shown in Fig.
6. The black edges including the hole are impervious, in contrast, the blue edges are the resin inlet and outlet. The curvature
R and side length
l of the surface Ω
_{0} are 1 meter. The inlet is 0.25 meters wide and locates in the middle of the northwest edge, and the opening has the diameter
d = 0.2 meters located at the center.
×
We choose four paths to represent the results. The first one is the line from the middle of the inlet to the outlet middle, viz.,
Center; the second path is the “northeast” edge in the Fig.
6, viz.,
Side; the next one is the line that equally splits the partition between the
Center and
Side, viz.,
Middle; and last, the “northwest” edge is named as
Front.
Four meshes are employed to discretize the preform, which are the coarse mesh (mesh 1: 163 elements), the regular mesh (mesh 2: 436 elements), the fine mesh (mesh 3: 1067 elements) and the finest mesh (mesh 4: 1882 elements). In addition, four different time step sizes are chosen as, 5 × 10
^{− 2} (time step 1) , 1 × 10
^{− 2} (time step 2), 1 × 10
^{− 3} (time step 3) and 5 × 10
^{− 4} (time step 4) seconds.
The mesh size convergence study is based on the difference of the global saturation degree
\(\tilde \xi \) of the coarse, regular and fine meshes relating to the finest mesh. The time step Δ
t = 1 × 10
^{− 3} seconds is selected and the infusion ends at 150 seconds. Because the number of time steps is fixed, the error with respect to the spatial discretization
e
_{m} is defined as the rootmeansquare error (RMSE) as,
where
n is the total number of time steps;
\(\tilde {\xi }_{mesh i, t}\) denotes the global saturation degree of the
ith mesh scheme at
tth second. Figure
7a shows that the convergence rate decreases as the element number increases. The error dropping from the coarse to the regular mesh is much higher than the dropping from the regular to the fine mesh. Especially, the error reduction from the regular to the fine mesh is limited small. Thus, the fine mesh is “fine enough” for the given case.
$$ e_{m} = \sqrt{\frac{{\sum}_{t=1}^{n} (\tilde{\xi}_{mesh i, t}\tilde{\xi}_{mesh 4, t})^{2}}{n}} \text{ with } i =1,2,3 \text{ ,} $$
(63)
×
Figure
7b shows the convergence study of the time step size when the fine mesh is chosen. Since the mesh size is fixed in this study, the error is compared with the nodal saturation degree
ξ of the time steps 1, 2 and 3 relating to the time step 4. With respect to the time discretization, the error
e
_{t} is defined as,
$$ e_{t} = \sqrt{\frac{{\sum}_{i=1}^{NNO} ({\xi}_{time step n, i}{\xi}_{time step 4, i})^{2}}{NNO}} \text{ with } i=1,2,3 \text{ ,} $$
(64)
It is also interesting to track the flow in the deformable preform. Figure
8 plots the resin flow patterns during the infusion process. The red regions represent the fullsaturated parts of the preform; and the blue regions indicate the dry parts; the gradients between red and blue illustrate the process zone, where the flow front locates. The tiny white lines show the flow directions in each element.
×
At the beginning of the process (0 – 50 seconds), the resin flow moves towards all directions simultaneously and forms a sector pattern. Once the flow reaches the hole (50 – 140 seconds), the hole drags down the neighboring flow speed. As a result, the side flow gradually moves faster than the center flow. At 137 seconds, the outside flow has already caught up the inner flow around the hole. When the entire flow front has passed the hole, the flow front forms a nearly straight line as shown at 217 seconds.
Figure
9 shows the pressure distribution. We can notice that there are local bands of lowpressure zones (blue bands) around flow fronts. The pressure drops to the bottom where the global minimum pressure locates, then just after the flow front, it rises again and forms a local pressure peak.
×
We also plot the preform profiles along different paths in Fig.
10, by using the finest mesh and 1 × 10
^{− 3} seconds as time step size. Due to the vacuum, the preform is compressed when the process just begins; after that, the resin moves into and inflates the preform up. From the front section, we can see that the inflation occurs in the vicinity of the inlet. This significant expansion happens immediately after the resin moves in. As the process going, the resin flow moves from the center to sides, which makes the swollen part expanding outwards gradually; and the depth of the swollen part reducing in the meanwhile. What is more, around the inlet, the inflation speed consistently slows down as the pressure approaches the atmospheric pressure.
×
The center, middle and side section mainly exhibit similar deformation profiles. The longitudinal profiles compress first then expand. The left side parts (
x < 0) have larger expansion than the right side parts (
x > 0). At 50, 100, and 200 seconds, there are local jumps around the flow front regions in the middle and side section. This behavior reflects low pressure bands in Fig.
9. After 200 seconds, the local jumps disappear and profiles turn smoother.
Conclusion
In this paper, we have presented a novel finite element based model for the LCM process of the thinwalled FRPCM components. The model contributes a shell element in the context of the theory of porous media to model both the preform deformation and the inplane resin flow. In this fashion, the full 3D fluidstructure interaction problem is reduced to a 2D porous media problem, which significantly reduces the number of the degrees of freedom. The model solves for three primary variables: 1) the saturation degree
ξ and 2) the fluid pressure
p are solved from the mass balance relations that describe the homogenized Darcy flow transporting in the porous media; 3) the normal stretch
λ is then obtained from the explicit formulation Eq.
53, which is derived from the linear momentum balance. The coupled Eqs.
55 and
56 are solved using the StreamlineUpwind/PetrovGalerkin stabilized finite element method following the staggered approach, as proposed in [
15]. The inplane flow assumption has been justified through the comparison between the 2D plane and shell models. The convergence studies for the doubly curved specimen shows that the method is converging with respect to the saturation degree for reasonable spatial and temporal discretizations. The model shows the ability to predict different mold filling settings, e.g., multiple resin inlets and different outlet positions. Besides, if the stretch field is prescribed, the same model can also be applied to the RTM process. Thus, this study proposes a simulation tool to optimize the wetout process in the deformable thinwalled fiber preform for largescale FRPCM components, which can substitute for the costly physical trial and error approaches.
Acknowledgments
The authors would like to acknowledge partial support by Swedish Research Council Grant 62120133907 and Chalmers University Area of Advance: Production. The simulations were performed on resources provided by the Swedish National Infrastructure for Computing (SNIC) at Chalmers Center for Computational Science and Engineering (C3SE).
Compliance with Ethical Standards
Conflict of interests
The authors declare that they have no conflict of interest.
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