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International Journal of Non-Linear Mechanics 43 (2008) 264 – 276 www.elsevier.com/locate/nlm Mechanics of polymeric membranes subjected to chemical exposure A.P.S. Selvadurai , Q. Yu 1 Department of Civil Engineering and Applied Mechanics, McGill University, 817 Sherbrooke Street West, Montréal, Que., Canada H3A 2K6 Received 4 January 2007; received in revised form 3 November 2007; accepted 11 December 2007 Dedicated to the memory of Professor R.S. Rivlin (1915–2005) Abstract The mechanics of polymeric hyperelastic membranes that are subjected to uniform transverse pressure loading are discussed. The paper also focuses on the membrane behaviour when there is loss of hyperelasticity resulting from the removal of plasticizer from the polymeric material as a result of chemical exposure. Constitutive models presented describe the influence of both hyperelasticity and rate-sensitivity on the mechanical behaviour of the polymeric membrane in its natural and chemically exposed states. The constitutive models developed through experimental investigations are implemented in computational techniques to develop solutions to the membrane deformation problems. 2007 Elsevier Ltd. All rights reserved. Keywords: Polymeric membranes; Hyperelasticity; Chemical exposure; Rate-dependent constitutive models; Membrane deformations; Finite element modelling 1. Introduction Polymeric membranes are used extensively as components of geo-environmental barrier systems that are used to prevent the migration of contaminants and hazardous wastes. A char- acteristic feature of polymeric membranes is their hyperelas- ticity, which is a beneficial attribute particularly in situations where the engineered membrane barrier can experience large deformational behaviour during ground movement. The hyper- elasticity and the accompanying rate-dependency of polymeric membranes is a result of plasticizers that are introduced into the material during its manufacture; its depletion, particularly due to leaching by chemicals, can result in the embrittlement of the polymeric membrane. Fig. 1 illustrates the progressive time-dependent embrittlement of a PVC membrane material during exposure to pure ethanol. The loss of hyperelasticity during chemical action is a cause for environmental concern, particularly because geo-synthetic membranes are used exten- sively for perpetual geo-environmental containment, without due attention being paid to the issue of loss of hyperelasticity William Scott Professor and James McGill Professor. Corresponding author. Tel.: +1 514 398 6672; fax: +1 514 398 7361. E-mail addresses: [email protected] (A.P.S. Selvadurai), [email protected] (Q. Yu). 1 Currently at Boeing Canada Technology, Winnipeg Division, 99 Murray Park Road, Winnipeg, Man., Canada R3J 3M6. 0020-7462/$ - see front matter 2007 Elsevier Ltd. All rights reserved. doi:10.1016/j.ijnonlinmec.2007.12.004 due to embrittlement. This paper develops a constitutive the- ory that can describe the hyperelastic behaviour of the rate- sensitive polymeric membrane material in its intact condition and examines the changes that account for the loss of hy- perelasticity and embrittlement during exposure to chemicals such as ethanol. The constitutive theories, developed and val- idated by appeal to experimentation, are implemented in a research-category computer code to examine the mechanics of edge-supported circular membranes both in their intact and chemically exposed conditions. Both axisymmetric and off-axis indentations of polymeric membranes have been used to vali- date the constitutive models. In this paper, the computational procedures are applied to examine the mechanics of square and triangular edge-supported membranes that are subjected to uni- form pressure. Further applications include the fluid pressure loading of a membrane, where a circular patch of the membrane experiences embrittlement due to the leaching of the plasticizer by chemical exposure. The stress analysis of the problems is performed by implementing the relevant constitutive models in the ABAQUS finite element code. 2. Constitutive modelling Modern mechanics of hyperelastic materials can be traced to the seminal studies of Rivlin, which are documented in his

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Page 1: MechanicsofpolymericmembranessubjectedtochemicalexposureA.P.S. Selvadurai, Q. Yu / International Journal of Non-Linear Mechanics 43 (2008) 264–276 265 0 2 4 6 8 10 12 14 16 18 20

International Journal of Non-Linear Mechanics 43 (2008) 264–276www.elsevier.com/locate/nlm

Mechanics of polymeric membranes subjected to chemical exposure

A.P.S. Selvadurai∗, Q. Yu1

Department of Civil Engineering and Applied Mechanics, McGill University, 817 Sherbrooke Street West, Montréal, Que., Canada H3A 2K6

Received 4 January 2007; received in revised form 3 November 2007; accepted 11 December 2007

Dedicated to the memory of Professor R.S. Rivlin (1915–2005)

Abstract

The mechanics of polymeric hyperelastic membranes that are subjected to uniform transverse pressure loading are discussed. The paperalso focuses on the membrane behaviour when there is loss of hyperelasticity resulting from the removal of plasticizer from the polymericmaterial as a result of chemical exposure. Constitutive models presented describe the influence of both hyperelasticity and rate-sensitivity onthe mechanical behaviour of the polymeric membrane in its natural and chemically exposed states. The constitutive models developed throughexperimental investigations are implemented in computational techniques to develop solutions to the membrane deformation problems.� 2007 Elsevier Ltd. All rights reserved.

Keywords: Polymeric membranes; Hyperelasticity; Chemical exposure; Rate-dependent constitutive models; Membrane deformations; Finite element modelling

1. Introduction

Polymeric membranes are used extensively as componentsof geo-environmental barrier systems that are used to preventthe migration of contaminants and hazardous wastes. A char-acteristic feature of polymeric membranes is their hyperelas-ticity, which is a beneficial attribute particularly in situationswhere the engineered membrane barrier can experience largedeformational behaviour during ground movement. The hyper-elasticity and the accompanying rate-dependency of polymericmembranes is a result of plasticizers that are introduced intothe material during its manufacture; its depletion, particularlydue to leaching by chemicals, can result in the embrittlementof the polymeric membrane. Fig. 1 illustrates the progressivetime-dependent embrittlement of a PVC membrane materialduring exposure to pure ethanol. The loss of hyperelasticityduring chemical action is a cause for environmental concern,particularly because geo-synthetic membranes are used exten-sively for perpetual geo-environmental containment, withoutdue attention being paid to the issue of loss of hyperelasticity

∗ William Scott Professor and James McGill Professor. Correspondingauthor. Tel.: +1 514 398 6672; fax: +1 514 398 7361.

E-mail addresses: [email protected] (A.P.S. Selvadurai),[email protected] (Q. Yu).

1 Currently at Boeing Canada Technology, Winnipeg Division, 99 MurrayPark Road, Winnipeg, Man., Canada R3J 3M6.

0020-7462/$ - see front matter � 2007 Elsevier Ltd. All rights reserved.doi:10.1016/j.ijnonlinmec.2007.12.004

due to embrittlement. This paper develops a constitutive the-ory that can describe the hyperelastic behaviour of the rate-sensitive polymeric membrane material in its intact conditionand examines the changes that account for the loss of hy-perelasticity and embrittlement during exposure to chemicalssuch as ethanol. The constitutive theories, developed and val-idated by appeal to experimentation, are implemented in aresearch-category computer code to examine the mechanics ofedge-supported circular membranes both in their intact andchemically exposed conditions. Both axisymmetric and off-axisindentations of polymeric membranes have been used to vali-date the constitutive models. In this paper, the computationalprocedures are applied to examine the mechanics of square andtriangular edge-supported membranes that are subjected to uni-form pressure. Further applications include the fluid pressureloading of a membrane, where a circular patch of the membraneexperiences embrittlement due to the leaching of the plasticizerby chemical exposure. The stress analysis of the problems isperformed by implementing the relevant constitutive models inthe ABAQUS finite element code.

2. Constitutive modelling

Modern mechanics of hyperelastic materials can be tracedto the seminal studies of Rivlin, which are documented in his

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A.P.S. Selvadurai, Q. Yu / International Journal of Non-Linear Mechanics 43 (2008) 264–276 265

0

2

4

6

8

10

12

14

16

18

20

0 50 100 200

1-week exposure

2-week exposure

1-month exposure

2-month exposure

7-month exposure

9-month exposure

σ 0 (

MP

a)

ε0 = (l-l0) / l0 x 100%

150 250

Fig. 1. Uniaxial stress–strain behaviour of a PVC membrane material subjectedto chemical (ethanol) exposure.

collected works edited by Barenblatt and Joseph [1]. The ma-jority of research in the area is applicable to pure rubber-likehyperelastic materials, which have imperceptible irreversiblephenomena in terms of non-coincidence of loading and unload-ing paths, resulting in both energy dissipation during cycles ofloading and the development of irreversible deformations uponremoval of loads. The constitutive potentials associated withrubber-like hyperelastic materials including those attributed toMooney–Rivlin, neo-Hookean, Blatz–Ko, Yeoh, Ogden, Gentand others are well documented in classical literature in finiteelasticity [2–5]. Reviews and extensive discussions of the rangeof constitutive models that have been proposed to describe hy-perelastic responses of rubber-like materials can be found inthe articles by Deam and Edwards [6], Ogden [7], Lur’e [8],Drozdov [9], Dorfmann and Muhr [10], Boyce and Arruda [11],Fu and Ogden [12], Besdo et al. [13], Busfield and Muhr [14],Saccomandi and Ogden [15], Selvadurai [16] and Rivlin [17].In addition, the adequacy of the Mooney–Rivlin form of a strainenergy function for examining transverse deflections of rub-ber membranes that experience moderately large strains wasrecently documented by Selvadurai [18].

In contrast, glassy polymeric materials, such as PVC, exhibitappreciable irreversible effects that include the development ofpermanent strains during loading–unloading cycles and strainrate effects [19,20]. The modelling of materials that exhibit ir-reversible, path-dependent, rate-sensitive effects has been thesubject of much research, both past and recent, and examplesof the development of constitutive models are given by Boyceand Arruda [11], Arruda et al. [19], Sweeney and Ward [20],Boyce et al. [21], Wineman and Rajagopal [22], Rajagopal andWineman [23], Bergström and Boyce [24], Septanika and Ernst

[25,26], Makradi et al. [27], Amin et al. [28], Gurtin and Anand[29] and Selvadurai and Yu [30]. Also of interest are recentstudies by Shaw et al. [31] that examine the chemorheologicalbehaviour of elastomers at elevated temperatures. In this paperwe adopt and extend the model proposed by Boyce et al. [21]to develop plausible constitutive models for the PVC materialin both its intact and chemically exposed states. A fundamentalassumption in the modelling is that the path-dependency andirreversibility associated with the mechanics of the PVC ma-terial can be captured by a model that is used to describe thehyperelastic behaviour of an elastic material with added con-straints to account for the rate-sensitivity and path-dependencyeffects. Other examples along these lines are the studies by Og-den and Roxburgh [32,33] that use the concept of an internalvariable, associated with deformation-related damage develop-ment to provide a rational explanation of the Mullins effectobserved in the mechanical behaviour of certain types of hy-perelastic rubber-like materials (see also [34,35]).

The visco-plastic constitutive model for PVC proposed in thispaper considers large strain elasticity phenomena, irreversibledeformation and strain rate effects. The results of experimentsconducted for constitutive model development were presentedbyYu and Selvadurai [36] and the associated constitutive modeldevelopment was discussed in greater detail by Selvadurai andYu [30]. Studies presented in [30] and [36] suggest that PVCmaterials can undergo strains moderately large enough to renderan approach based on an incremental rate-dependent theory ofmaterial behaviour of limited value. Therefore, we formulatea constitutive model that accounts for finite deformations ofthe PVC material. The position of a generic particle in thereference configuration is denoted by the Cartesian coordinatesXA (A=1, 2, 3) and its position in the deformed configurationis denoted by xi (i = 1, 2, 3). The deformation gradient tensoris given by

F = �xi

�XA

. (2.1)

We restrict attention to PVC materials that are largely incom-pressible, which requires that det F = 1. Following the ap-proaches proposed by Kröner [37] and Lee [38] to describethe mechanics of continua undergoing finite deformations thatexhibit both reversible and irreversible components (see also[29,39–43]), we assume that the total deformation gradient ten-sor F admits a product decomposition into its elastic (e) andirreversible (u) components, i.e.

F = FeFu. (2.2)

The strain tensors associated with the elastic and irreversibledeformations are defined by Be and Bu, respectively, where

Be = Fe(Fe)T, Bu = Fu(Fu)T (2.3)

and the strain rates are defined by [44,45]

L = FF−1 = D + W = Fe(Fe)−1 + Fe[Fu(Fu)−1](Fe)−1,

Lu = Fu(Fu)−1, Du = 12 [Lu + (Lu)T]. (2.4)

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266 A.P.S. Selvadurai, Q. Yu / International Journal of Non-Linear Mechanics 43 (2008) 264–276

Rate-dependent elastic constitutive component C

We = C1 (γ0) (I1 - 3) + C'2 (γ0) (I2 - 3)

Viscoplastic component B ζ = g (τB)

Elastic recovery/restraint component A

TA

TB

T = TA + TB T = TA + TB

Wu (I1, I2) = E1 (I1-3) + E2 (I2-3)

Molecular chain network

' e e

u u u u''

·

··

Fig. 2. Schematic representation of the constitutive components.

The invariants of Be and Bu are

Ih1 = (�h

1)2 + (�h2)2 + (�h

3)2, I h2 = 1

(�h1)2

+ 1

(�h2)2

+ 1

(�h3)2

,

Ih3 = �h

1�h2�h

3 = 1, (h = e, u) (2.5)

and �ei and �u

i (i = 1, 2, 3) are, respectively, the principalstretches of the elastic and irreversible components. The gen-eral form of the constitutive model for the PVC material hasbeen selected to conform to a generic version with componentsas shown in Fig. 2.

2.1. A constitutive model for the untreated PVC

The calibration of experimental results [30,36] with a widerclass of strain energy functions indicates that for moderatelylarge strains, the constitutive behaviour of the PVC mate-rial can be adequately characterized by choosing an internalenergy function with a mathematical form similar to theMooney–Rivlin type [18,46–48]. Thus, component C of themodel shown in Fig. 2 is represented by a pseudo-elastic be-haviour with an internal energy function of the Mooney–Rivlintype. We also note that it is sufficient to characterize the consti-tutive behaviour of the PVC material during monotonic load-ing without unloading. In this case, there are no irreversibleeffects and the total deformation gradient F can be interpretedas an elastic deformation gradient Fe. The stress TC associatedwith the model C, which is the total Cauchy stress T in thematerial, is assumed to be an isotropic function of the elasticstrain tensor Be and takes the form

T = TC = −peI + �e1Be + �e

2(Be)2,

�e1 = 2

(�W e

�I e1

+ I e1�W e

�I e2

), �e

2 = −2�W e

�I e2

, (2.6)

where pe is a scalar pressure. Considering the approach pro-posed by Sweeney and Ward [20] to account for the influenceof the strain rate effects on the strain energy function, we adoptthe following form of internal energy function for the PVC ma-terial:

W e(I e1 , I e

2 ) = C′1(I

e1 − 3) + C′

2(Ie2 − 3), (2.7)

where

C′1 = C1 +

{�1 ln(|�0|/�c) (|�0|� �c),

0 (|�0| < �c),

C′2 = C2 +

{�2 ln(|�0|/�c) (|�0|� �c),

0 (|�0| < �c).(2.8)

The thermodynamic basis for introducing the dependency ofW e on �0 is discussed in Selvadurai and Yu [30]. In (2.8), �0is a generalized form of a combined stretch rate that dependsonly on the principal stretches �i (i = 1, 2, 3), such that

�0 = d�0

dt, �0 = [(�1 − 1)1/� + (�2 − 1)1/� + (�3 − 1)1/�]�,

(2.9)

where �i (i = 1, 2, 3) have a conditional dependence on thetotal principal stretches �i to take into consideration either thestretching or the unloading response, i.e.

�i ={

�i (�i �1) i = (1, 2, 3),

1 (�i < 1) i = (1, 2, 3)(2.10)

and � is a material parameter that accounts for combined stretch.We note that when a specimen is subjected to a uniaxial stretch,the principal stretches in the lateral directions are less than unityand therefore the definition of �0 reduces to that of the uniaxialstrain ε0. In (2.8), C′

1 and C′2 are the modified Mooney–Rivlin-

type parameters; �1 and �2 are parameters that define thestrain rate sensitivity and �c is defined as the rate-independent

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A.P.S. Selvadurai, Q. Yu / International Journal of Non-Linear Mechanics 43 (2008) 264–276 267

threshold strain rate, i.e. a parameter that controls the manifes-tation of strain rate effects. At loading rates |�0|� �c, the strainrate effects are disregarded. The loading behaviour was exam-ined by considering the uniaxial response of a specimen of PVCtested up to failure at loading rates ε0 = 0.4, and 40%/min.The material parameters required to define C′

1 and C′2 were de-

veloped using experimental data and the specific values deter-mined were as follows:

C1 ≈ 0.23 MPa; C2 ≈ 0.53 MPa; �1 = �2 = � ≈ 0.13;

�c ≈ 5.67 × 10−7 s−1.

PVC materials invariably exhibit permanent strains at any levelof applied strain. Therefore, a visco-plastic model, character-ized by an elastic recovery component A in parallel with a visco-plastic component B should be incorporated in series with thecomponent C. Since the component A accounts for elastic un-loading at moderately large strains, we can conclude that themodel, which accounts for the unloading response, can also bedescribed by an internal energy function of the Mooney–Rivlinform, i.e.

TA = −puI + �u1Bu + �u

2(Bu)2,

�u1 = 2

(�W u

�I u1

+ I u1

�W u

�I u2

), �u

2 = −2�W u

�I u2

, (2.11)

where pu is a scalar pressure and

W u(I u1 , I u

2 ) = E′1(I

u1 − 3) + E′

2(Iu2 − 3) (2.12)

with the superscript ‘u’ signifying the unloading mode. In(2.12), we apply a conditional constraint to E′

1, i.e.

E′1 =

{ → ∞ (�0 � − �vc ),

0 (�0 < − �vc )

(2.13)

and E′2 is treated as a constant. The strain rate-dependent E′

1in (2.13) takes into account the asymmetric behaviour of theelastic recovery component A during a loading–unloading re-sponse. The stress TB in the component B is defined in terms ofthe finite plastic strain rate Du, which is assumed to be relatedto the deviatoric component of the normalized effective stresstensor NB . Considering the component B, the visco-plastic ef-fects are modelled through a relationship of the form (see e.g.[49,29])

Du = �NB, NB = 3

2�B

T′B, �B =

{3

2tr[(T′

B)2]}1/2

(2.14)

and T′B is the deviatoric component of the Cauchy stress ten-

sor TB applicable to visco-plastic phenomena, as depicted inFig. 2. Also, in (2.14) the visco-plastic strain rate � is consid-ered to be a function of the effective stress �B and the strainrate �0, i.e.

� =(

�B

q

)1−s

|�0|{ 1

(|�0|/�vc )

s (|�0|� �vc ),

1 (|�0| < �vc ).

(2.15)

In (2.15), s is the viscous sensitivity to the strain rate effect. Atextremely low loading rates |�0|� �v

c , and the dependency of� on the strain rate �0 is neglected; therefore, the parameter qcan be interpreted as the static yielding stress of the material.We note that when s ≈ 0, the value of �v

c is inapplicable, andthe response of the material reduces to that of a purely plasticmaterial.

During a loading stage (�0 �0) and at extremely low loadingrates (|�0|� �v

c ), the visco-plastic deformation applicable to thecomponents A and B is constrained by the choice of an infinitevalue for E′

1, with the result that only the elastic deformation ofcomponent C is applicable to the PVC material. Upon unload-ing, however, the visco-plastic deformation is fully activateddue to the zero value of E′

1 chosen in (2.13). All three compo-nents A.C take effect during the unloading of the PVC mate-rial. Following Boyce et al. [21], the stress states in the elasticrecovery response A (denoted by TA) and the visco-plastic re-sponse B (denoted by TB ) are added to generate the Cauchystress T, i.e.

T = TC = TA + TB . (2.16)

The visco-plastic properties necessary to model the unloadingbehaviour of the PVC can also be determined from the resultsof uniaxial tests. The experiments were conducted at strainrates of ε0 =4 and ε0 =40%/ min up to a peak strain of 140%,followed by unloading. The specific material parameters appli-cable for the PVC are as follows: q ≈ 2.0 MPa; s ≈ 0; E′

2 ≈0.5 MPa.

The parameter �0 accounts for the influence of strain rates onthe mechanical response of untreated PVC. As is evident from(2.9), the strain rate influences are controlled by the materialparameter �. In order to determine �, it is necessary to conductexperiments where the PVC membrane material is subjected toa state of inhomogeneous strain. The details of the experimen-tal investigations are given in [30,36] and involve the uniaxialmonotonic stretching of a membrane fixed symmetrically alongoblique planes. A computational modelling of the experimen-tal configuration can be used to estimate �. Since the elasticityparameters C′

1 and C′2 have a logarithmic dependency on the

combined stretch rate �0 (see e.g. (2.8)), there appears to beonly a marginal sensitivity of the computational results to theparameter �. The correlations between the experimental resultsand computational modelling were performed with differentvalues of the parameters � conducted at axial stretching ratesof = 2 and 20 mm/min. At an extension of �7 mm, whichcorresponds to a maximum biaxial stretch �1 ≈ �2 ≈ 1.15,the computations show only marginal dependence on the valueof �. The parameter � has an influence on the computationalresults only at larger extensions ( > 7 mm) where slip takesplace between the metal grips and the PVC specimen leadingto unreliable estimates of the load—displacement responses. Acomparison between the computational predictions and the ex-perimental results obtained at two extension rates indicate thatthe parameter � ≈ 3.

The model parameters obtained were used to predict the be-haviour of the untreated PVC subjected to uniaxial stretching at

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268 A.P.S. Selvadurai, Q. Yu / International Journal of Non-Linear Mechanics 43 (2008) 264–276

0 50 1000

5

10

15

σ 0 (

MP

a)

ε0 = (l - l0) / l0 × 100%

150

Fig. 3. Uniaxial stress–strain behaviour of an untreated PVC membranematerial tested at a strain rate ε0 = 160%/ min. The symbols representexperimental results.

a strain rate of ε0 = 160%/ min. A comparison of experimentalresults and model predictions is shown in Fig. 3.

2.2. A model for the ethanol-treated PVC

Results of uniaxial tests conducted on the ethanol-treatedPVC membrane materials indicate the gradual loss of hypere-lasticity as the plasticizer leaches from the specimen (Fig. 1).Therefore, in order to develop a comprehensive model of theprogressive evolution of loss of hyperelasticity, it is necessaryto incorporate the influences of chemical diffusion on the con-stitutive responses. The experimental results, however, indi-cate that beyond a certain duration of exposure to ethanol, thestress–strain relationship for the PVC remains virtually unal-tered. Considering this observation, it is feasible to focus on thedevelopment of a constitutive model for the chemically treatedPVC by considering a threshold duration of a 7-month exposureperiod. Experimental observations also showed a drastic loss ofhyperelasticity as ethanol diffused into the PVC membrane andleached the plasticizer: In terms of the stress–strain response,the hyperelasticity of the untreated material is replaced by anearly linear elastic response with a pronounced yield pointaccompanied by both strain softening and strain hardening re-sponses. As the chemically treated PVC deforms it is capa-ble of sustaining appreciable post-yield strains without failureand fracture. The development of a constitutive model for theethanol-treated PVC can be approached in a variety of ways:for consistency, however, we develop a constitutive model fol-lowing the basic framework used in developing the constitutivemodel for the untreated PVC. We select a neo-Hookean formof the internal energy function, which can be derived from aninternal energy function with C′

2 ≡ 0, which reduces to theclassical neo-Hookean isotropic model in situations where aninfinitesimal strain measure is used. Therefore, for the ethanol-treated PVC, the internal energy function applicable to the

loading range associated with the experiments can be written as

W e(I e1 , I e

2 ) = C′1(I

e1 − 3), (2.17)

where

C′1 = C1 +

{�1 ln(|�0|/�c) (|�0|� �c),

0 (|�0| < �c).(2.18)

The results from a series of relaxation tests and uniaxial load-ing tests conducted at loading rates ε0=0.4, 4 and 40%/min areused to determine C′

1 [30] and provide the following set of pa-rameters defining the strain rate dependency: C1 ≈ 14.2 MPa;�1 ≈ 12.06; �c ≈ 5.67 × 10−7 s−1. (We note here that con-siderable time is required to reach failure; the experimental in-vestigations cited were conducted mainly to examine the linearelastic modulus of the chemically treated material, and the ex-periments were terminated once yield was observed.) The mag-nitude of the rate-independent threshold strain rate (�c) wasapproximately the same for both the untreated and the ethanol-treated PVC membrane materials. Furthermore, the departurefrom elastic behaviour initiates with the yield of the ethanol-treated PVC, with the yield strain roughly corresponding to�y ≈ 2.8%. This suggests that �y is relatively uninfluenced bythe duration of chemical exposure. The yield strain thus cor-responds to the state resulting from the fracture of the transi-tional link, which can occur at a critical strain ε0 = �0 = �y .Its dominant presence is then determined from the degree ofsusceptibility of the transitional link to ethanol exposure. Theduration of ethanol exposure, however, has little influence onthe elasticity characteristics of the elastic recovery model A.Changes in the elasticity characteristics of the recovery modelA will be influenced by the breakage of the transitional links.Following the modelling adopted for the untreated PVC, theelastic parameter E′

2 is considered to be a constant. The param-eter E′

1, however, takes into consideration material yield andcan be represented in the form

E′1 =

{ → ∞ (�0 � − �vc and �0 ��y),

E′y (�0 � − �v

c and �0 > �y),

0 (�0 < − �vc ).

(2.19)

In (2.19), �y is the yield strain and E′y can be interpreted as the

post-yield hardening modulus. This particular representation ofE′

1 takes into consideration the complete elastic behaviour ofthe treated material before yield at a loading rate �0 � − �v

c ,where the visco-plastic deformation is restricted by the valueof infinity assigned to E′

1. Beyond the yield point, E′1 has a

finite value. This, however, results in the development of visco-plastic deformations, contributing to the initial softening andsubsequent hardening behaviour, particularly in the large strainrange (e.g. ε0 = 100.150%). During unloading (i.e. �0 <− �v

c ),visco-plastic effects are fully activated due to the fact that E′

1 =0, and this contributes to significant irreversible visco-plasticstrains. We also consider the possible influences of the rate-dependency on the hardening modulus E′

y , which is modelledaccording to the relationship

E′y = Ey +

{�y ln(�0/�

vc ) (�0 � �v

c ),

0 (−�vc � �0 < �v

c ),(2.20)

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A.P.S. Selvadurai, Q. Yu / International Journal of Non-Linear Mechanics 43 (2008) 264–276 269

0 50 1000

5

10

15

20

25

σ 0 (

MP

a)

ε0 = (l - l0) / l0 × 100%

150

Fig. 4. Uniaxial stress–strain behaviour of a chemically treated PVC mem-brane material tested at a strain rate ε0 = 160%/ min. The symbols representexperimental results.

where �y is the rate-sensitivity and Ey is the rate-independenthardening modulus. To account for the visco-plastic responsesin the ethanol-treated PVC, we adopt the form of (2.15).In contrast to the untreated PVC material, the visco-plasticresponse dominates the unloading mode, and beyond theyield point �y , also takes into consideration the softeningresponse.

In the parameter identification exercise we first examine thetime-independent behaviour of the PVC. In the ethanol-treatedPVC, there is a noticeable yield point associated with the pro-posed time-independent stress–strain response. The absence ofsoftening suggests the applicability of the assumption concern-ing the absence of a viscous effect at limiting loading rates lessthan �v

c . We can determine the static yield stress q(=6C1�y) ≈2.4 MPa from the time-independent stress–strain curve. The pa-rameters Ey and E′

2 can be determined by matching the slopeof the hardening response of the time-independent stress–straincurve; using this procedure we obtain Ey ≈ 1.1 MPa andE′

2 ≈ 1.2 MPa. The parameter E′y that accounts for the rate-

dependency can be obtained by matching the slope of thehardening responses for a set of loading tests conducted at theloading rates ε0 = 4 and 40%/min. Considering such a proce-dure, the constitutive parameters required to characterize theethanol-treated PVC are obtained as follows: Ey ≈ 1.13 MPa;�y ≈ 0.13; �v

c ≈ 3.2 × 10−10 s−1. The viscous sensitivity s isthe only remaining parameter introduced in (2.15). As s → 0,the unloading behaviour of the material (with E′

1 = 0) is virtu-ally uninfluenced by the loading rate. Considering the soften-ing region, where E′

1 �= ∞, the rate-sensitivity is appreciableeven though s approaches zero. The value of s therefore hasa significant influence on the softening response of the mate-rial, since, beyond the yield point, E′

1 transforms abruptly froman infinite value to a finite value (i.e. ε0 = �y). The parameteridentification exercises performed on the stress–strain curvesderived at loading rates ε0 = 4 and 40%/min indicate that s ≈0.1. The visco-plastic behaviour of the chemically treated PVCcan be defined by the parameters: q ≈ 2.4 MPa; s ≈ 0.1; �v

c ≈3.2 × 10−10 s−1. The results for the time-independent response

Fig. 5. Fluid pressure loading of a PVC membrane fixed along a circularboundary.

and the stress–strain curves derived up to failure at loading ratesof ε0 =4 and 40%/min by material parameters indicate that ac-curate representations are obtained for the yield behaviour ofthe material, followed by a material softening and a moderateamount of hardening at large deformations (i.e. strains in therange ε0 = 100.150%). The material parameters were furtherused to evaluate the computational responses of a test speci-men fixed along oblique directions and subjected to an axial ex-tension rate of = 2 mm/ min. The computational evaluationswere performed with different values of the parameter �. Sincethe plasticizer loss appears to stabilize after 5 months of expo-sure [50], it may be concluded that the material parameter �is virtually uninfluenced by the duration of chemical exposure.Considering the discussion pertaining to the evaluation of theparameter � for the untreated material, it could be concludedthat the value � ≈ 3 is also applicable to the PVC membranematerial when exposed to ethanol for a period of 7 months.This value is possibly indicative of equal contributions fromthe three principal stretch directions of the polymeric materialin the definition of �0 in (2.19). The model parameters for theethanol-treated PVC membrane material developed using ex-perimental data from tests conducted at strain rates of ε0 = 4and 40%/min were used to predict the response that would beobtained for a ethanol-treated PVC material uniaxial test con-ducted at a strain rate of ε0 = 160%/ min. The comparison be-tween experimental results and computational predictions areshown in Fig. 4.

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270 A.P.S. Selvadurai, Q. Yu / International Journal of Non-Linear Mechanics 43 (2008) 264–276

Fig. 6. Hydraulic loading on an untreated circular membrane. Total numberof elements: 2402; maximum fluid pressure corresponds to 1 m of water.

3. Mechanics of PVC membranes

PVC membranes are used as engineered barriers; it is there-fore instructive to apply the constitutive models presentedpreviously to examine the mechanics of membranes, bothuntreated and ethanol-treated, to investigate the behaviourof typical membrane configurations. The forms of the con-stitutive models presented in the previous section are suchthat analytical solutions for even the simplest axisymmetricproblems cannot be obtained conveniently. Consequently, acomputational approach is adopted to examine a range ofproblems of engineering interest. The specific problems thatare examined here include the application of fluid pressuresto edge-supported membranes with circular, square and tri-angular planforms. An additional problem considers the fluidpressure-induced deflection of an edge-supported untreated cir-cular PVC membrane containing a circular patch that has beensubjected to chemical exposure. These computations were per-formed using the general-purpose finite element code ABAQUS(ABAQUS/Standard [51]). There are several computationalfeatures in ABAQUS/Standard relevant to the computationalmodelling of the axisymmetric/asymmetric membrane loading

0

5

10

15

20

25

30

35

40

45

50

-150 -50 50 100 150

H = 500mm (loading)

H = 250mm (loading)

H = 750mm (loading)

H = 1000mm (loading)

H = 750mm (unloading)

H = 250mm (unloading)

permanent shape

Y (

mm

)

0-100

X (mm)

Fig. 7. The deflected shape of the untreated circular membrane under the actionof fluid accumulation in the reservoir. Maximum fluid pressure correspondsto 1 m of water.

Fig. 8. Hydraulic loading on a chemically treated circular membrane. Totalnumber of elements: 2402; maximum fluid pressure corresponds to 1 m ofwater.

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A.P.S. Selvadurai, Q. Yu / International Journal of Non-Linear Mechanics 43 (2008) 264–276 271

Fig. 9. Hydraulic loading on an untreated square membrane. Total numberof elements: 2998; maximum fluid pressure corresponds to 1 m of water.

problems and include consideration of large strain phenomena,and, most importantly, the ability to implement the constitutivemodel derived in Section 2 in the computational algorithm.Complete descriptions of these procedures are contained in thesupplied document in ABAQUS/Standard, which is discussedin the User Subroutine UMAT (ABAQUS/Standard [51]). Inthis study, only the last feature will be discussed. In the non-linear analysis using the ABAQUS/Standard code, each step isdivided into iteration increments. In this analysis, we chose thesize of the first loading increment, and the ABAQUS/Standardcode automatically assigns the size of subsequent increments.During each increment, the code employs a Newton–Raphsonalgorithm to perform the iterations and the equilibrium isdetermined through consideration of the principle of virtualwork, i.e.

∫V 〈t+�t〉

T〈t+dt〉: D〈t+dt〉 dV 〈t+dt〉

=∫

S〈t+�t〉t〈t+dt〉 • v dS〈t+dt〉

+∫

V 〈t+�t〉f 〈t+dt〉 • v dV 〈t+dt〉, (3.1)

H = 500mm (loading)

H = 250mm (loading)

H = 750mm (loading)

H = 1000mm (loading)

H = 750mm (unloading)

H = 250mm (unloading)

permanent shape

0

10

20

30

40

50

60

50 100 150

Y (

mm

)

-150 -100 -500 0

X (mm)

Fig. 10. The deflected shape of the untreated square membrane under theaction of fluid accumulation in the reservoir. Maximum fluid pressure corre-sponds to 1 m of water.

where T is the Cauchy stress, D is the incremental strain rate,v is a vector of virtual displacements, t is a vector of externallyapplied surface tractions on a unit surface of S, f is a body forcevector on a unit volume of V and 〈t+dt〉 denotes a state evaluatedat time t + dt . For the Newton–Raphson algorithm, we requirethe Jacobian of the finite element equilibrium equations. TheJacobian, which is obtained by taking the variation of Eq. (3.1),can be written as∫

V 〈t+dt〉(dT〈t+dt〉: D〈t+dt〉 + T〈t+dt〉: dD〈t+dt〉) dV 〈t+dt〉

=∫

S〈t+dt〉

(dt〈t+dt〉 • v + t〈t+dt〉 • v

dA

A

)dS〈t+dt〉

+∫

V 〈t+dt〉

(df 〈t+dt〉 • v + f 〈t+dt〉 • v

dJ

J

)dV 〈t+dt〉

(3.2)

with

A = dS〈t+dt)

dS〈t〉 , J = dV 〈t+dt)

dV 〈t〉 , (3.3)

where A is the surface area ratio between time t +dt and t, andJ is the volume ratio between time t + dt and t. The right sideof Eq. (3.2) is defined by the boundary conditions involvingthe loading conditions and displacement constraints. On the leftside, the expressions for the strain measure D and its variationsdD and dD in terms of the virtual displacement are definedby the displacement interpolation function used in the elementdefinition. It has been shown (ABAQUS/Standard [51]) that the

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272 A.P.S. Selvadurai, Q. Yu / International Journal of Non-Linear Mechanics 43 (2008) 264–276

left side of Eq. (3.2) can be expressed in a more explicit form:∫V 〈t+dt〉

{dD〈t+dt〉: C〈t+dt〉: D〈t+dt〉 − 1

2T〈t+dt〉

: [2D〈t+dt〉 • D〈t+dt〉 − (Lt+dt )T • Lt+dt ]}

dV 〈t+dt〉,

where C is the tangential stiffness and a fourth-order tensordefined by

C = �(dT)

�(dD). (3.4)

The data on both C and T are defined by the constitutiveresponses of the PVC material implemented through the sub-routine UMAT available in the ABAQUS/Standard code. TheABAQUS/Standard further utilizes a backward-Euler schemeas a default finite difference scheme to update variables. Thosevariables that are determined from previous iterations and donot change during the iteration between [t, t + dt] can bedefined as state variables. The state variables adopted in thisanalysis include the components of the irreversible deforma-tion gradient Fu at time t and the stress tensors at time t, in thevisco-plastic component including models A and B. When afully backward-Euler finite difference scheme in time is imple-mented, the updating of �0 requires information on the materialconfiguration at t + dt . The updated value of �0 will have adirect influence on the elasticity parameters for the element Cin the chosen constitutive model, with the result that the com-putations will exhibit non-convergence. The value of �0 is thusassumed to remain unchanged during iteration and is taken asa further state variable. For the problems examined here, thePVC membrane only experiences incremental loading duringthe initial stage where irreversible deformations are absent; theinitial values of the state variables can therefore be obtainedby treating the material as fully elastic. The state variables areupdated only when the iteration converges. Both a quadratictriangular membrane element (3M6) and a linear solid triangu-lar prism element (C3D6) were utilized in the computationalmodelling. The results indicated no noticeable differences be-tween the two types of elements. The computations presentedin the paper were developed using the solid triangular prismelement.

3.1. Uniform loading of an edge-supported circular membrane

In this example we consider the fluid loading of a circularPVC membrane of radius 125 mm, which is fixed at the bound-ary (Fig. 5). The membrane is loaded by fluid (water at a densityof �=1 g/cc) pressures that are applied through accumulation offluid in a reservoir at a prescribed rate Q=12 L/ min. Since themembrane deflects a substantial amount during the applicationof the fluid loading, the applied fluid pressure is non-uniformwith an axisymmetric variation roughly corresponding to theheight of the fluid in the reservoir. The maximum fluid pressureapplied to the membrane corresponds to 1 m of water. This isa departure from the usual uniform air-pressurization approxi-mation used in the testing of membranes but the example rep-

Fig. 11. Hydraulic loading on chemically treated square membrane. Totalnumber of elements: 2998; maximum fluid pressure corresponds to 1 m ofwater.

resents a useful model of a condition that can be encounteredin practice. The unloading is carried out by the removal of thefluid at the same emptying rate. The computational modellinguses the finite element discretization of the circular membraneregion shown in Fig. 6. Fig. 7 shows the deflected shape of theuntreated PVC circular membrane for various levels of fluidaccumulation and fluid withdrawal. Analogous results for thecase involving the ethanol-treated PVC circular membrane areshown in Fig. 8. It may be noted that the computational mod-elling illustrates the development of permanent deformationsin both untreated and chemically treated membranes during theloading–unloading process.

3.2. Uniform loading of an edge-supported square membrane

In the second example we consider the problem of a squarePVC membrane that is fixed at the boundary and subjected tofluid loading similar to that described in Section 3.1. The fi-nite element model of the membrane region is shown in Fig. 9.The deflected shapes of the square membrane along one of theaxes of symmetry, for both loading and unloading paths and forboth the treated and untreated PVC membranes are shown in

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A.P.S. Selvadurai, Q. Yu / International Journal of Non-Linear Mechanics 43 (2008) 264–276 273

Fig. 12. Hydraulic loading on an untreated equilateral triangular membrane.Total number of elements: 1712; maximum fluid pressure corresponds to 1 mof water.

Fig. 10. The maximum fluid pressure applied to the membranecorresponds to 1 m of water. The deflection of the chemicallytreated PVC is significantly lower (see Fig. 11). The results forthe deflection of the membrane during the loading–unloadingprocess display characteristics similar to those observed in con-nection with the fluid loading of the untreated and chemicallytreated circular membrane.

3.3. Uniform loading of an edge-supported equilateraltriangular membrane

In the third example we examine the deflection of an equi-lateral triangular membrane that is fixed at the boundary andsubjected to fluid loading similar to that described previously.The finite element model of the membrane region is shown inFig. 12. The deflected shapes of the untreated equilateral mem-brane, along an axis of symmetry, for both loading and unload-ing paths are shown in Fig. 13. The deflection of the chemicallytreated PVC is limited (see Fig. 14). The results for the de-flection of the membrane during the loading–unloading processdisplay characteristics similar to those observed in connectionwith the fluid loading of the untreated and chemically treatedcircular and square membranes.

H = 500mm (loading)

H = 250mm (loading)

H = 750mm (loading)

H = 1000mm (loading)

H = 750mm (unloading)

H = 250mm (unloading)

permanent shape

0

5

10

15

20

25

30

35

40

50 100

Y (

mm

)

-50-100-150 0

X (mm)

150

Fig. 13. The deflected shape of the untreated equilateral triangular membraneunder the action of fluid accumulation in the reservoir. Maximum fluidpressure corresponds to 1 m of water.

Fig. 14. Hydraulic loading on a chemically treated equilateral triangular mem-brane. Total number of elements: 1712; maximum fluid pressure correspondsto 1 m of water.

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274 A.P.S. Selvadurai, Q. Yu / International Journal of Non-Linear Mechanics 43 (2008) 264–276

Fig. 15. Hydraulic loading on an untreated circular membrane with a centralcircular patch. Total number of elements: 3770; maximum fluid pressurecorresponds to 1 m of water; ratio between diameter of patch and that of themembrane: 0.32.

3.4. Fluid pressure loading of a membrane containing acircular patch subjected to chemical exposure

In this section we examine the problem of the fluid pressureloading of a PVC membrane that contains a circular patch thathas been subjected to chemical exposure. The ratio betweenthe diameter of the patch and that of the membrane is 0.32.The geometry of the problem is shown in Fig. 15. The max-imum fluid height applied to the membrane is 1 m. Fig. 16shows the deflected shape of the untreated PVC circular mem-brane for various levels of the fluid accumulation and fluidwithdrawal. The central patch zone deflects as a rigid regionand this contributes to a reduction in the overall deflectionsand the corresponding permanent deflections. The junction be-tween the two regions invariably exhibits sharp changes in thecurvature, which can be a source for concern, especially withregard to the development of fracture and damage at thoselocations.

0

5

10

15

20

25

30

35

40

45

50 150

H = 500mm (loading)

H = 250mm (loading)

H = 750mm (loading)

H = 1000mm (loading)

H = 750mm (unloading)

H = 250mm (unloading)

permanent shapeY

(m

m)

X (mm)

-50 0-100-150 100

Fig. 16. The deflected shapes of the untreated circular membrane with acentral circular patch under the action of fluid accumulation in the reservoir.Ratio between diameter of patch and that of the membrane: 0.32; maximumfluid pressure corresponds to 1 m of water.

4. Concluding remarks

The use of PVC membranes as liners or engineered barriersfor landfill implicitly assumes that the hyperelastic attributes ofthe liners remain unaltered throughout the lifetime of the barrier.Experimental research points to the loss of hyperelasticity thatcan result from direct contact of the PVC with chemicals suchas acetone and ethanol. The chemical leaching of plasticizerfrom the PVC also results in a barrier material that exhibits dis-tinct yield-like stress–strain characteristics. It is shown that themechanical behaviour of the untreated PVC can be modelled asa rate-sensitive hyperelastic material with internal energy func-tions that are loading path-dependent. The ethanol-treated PVCcan also be modelled using the general approach developed todescribe the constitutive behaviour of the untreated PVC. Thematerial parameters required to describe both responses can beexperimentally determined and the constitutive models them-selves are amenable for implementation in general-purposefinite element computational schemes that accommodate hy-perelasticity and strain rate sensitivity. The computationalschemes are used to examine the mechanics of edge-supportedPVC membranes that are subjected to loading by fluid pres-sure. The computational results show trends that are consistentwith those obtained from experiments involving transverseindentation of both untreated and treated edge-supported PVCmembranes by fluid pressure. The problems examined pro-vide further experimental arrangements for examining thevalidity of the constitutive models and their computationalimplementations.

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A.P.S. Selvadurai, Q. Yu / International Journal of Non-Linear Mechanics 43 (2008) 264–276 275

Acknowledgements

The work described in the paper was supported through aDiscovery Grant awarded by the Natural Sciences and Engi-neering Research Council of Canada awarded to the first au-thor, who would also like to acknowledge the research supportreceived by the Max Planck Gesellschaft through the Award ofthe 2003 Max Planck Forschungspreis in the Engineering Sci-ences. Both authors are grateful for the assistance of StanfordUniversity towards to development of the computational solu-tions.

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