Abstract
In this paper, an advanced low-order solid–shell formulation is presented for modeling electro-active polymers (EAPs). This advanced finite element is of great importance due to the fact that EAPs actuators are typically designed as shell-like formations, in which the application of standard finite element formulation will lead to various locking pathologies (e.g. shear locking, trapezoidal locking, volumetric locking, etc.). Thus, for alleviating the various locking pathologies, both the assumed natural inhomogeneous strains (ANIS) and the enhanced assumed strain (EAS) methods are adopted for modifying the strain measure. Within the modified kinematics, a strain energy function that accounts for the elastic and the viscoelastic response as well as the electromechanical coupling is adopted. The developed formulation is implemented in the finite-element software Abaqus for further numerical applications, in which the developed ANIS solid–shell is compared with the classical assumed natural strains solid–shell and the mixed finite element formulation.
Similar content being viewed by others
References
Abed-Meraim F, Combescure A (2009) An improved assumed strain solid–shell element formulation with physical stabilization for geometric non-linear applications and elastic-plastic stability analysis. Int J Numer Methods Eng 80:1640–1686
Andelfinger U, Ramm E (1993) EAS-elements for two-dimensional, three-dimensional, plate and shell structures and their equivalence to HR-elements. Int J Numer Methods Eng 36(8):1311–1337
Ask A, Menzel A, Ristinmaa M (2013) Inverse-motion-based form finding for quasi-incompressible finite electroelasticity. Int J Numer Methods Eng 94(6):554–572
Ausserer M, Lee S (1988) An eighteen node solid element for thin shell analysis. Int J Numer Methods Eng 26:1345–1364
Bar-Cohen Y (2001) Electroactive polymers as artificial muscles-reality and challenges, 1st edn. SPIE press, Bellingham
Batoz J, Dhatt G (1972) Development of two simple shell elements. AIAAJ 10:237–238
Betch P, Stein E (1997) An assumed strain approach avoiding artificial thickness straining for a nonlinear 4-node shell element. Comp Methods Appl Mech Eng 11:899–909
Bischoff M (2008) Modeling of shells with three-dimensional finite elements. In: 6th international conference on computation of shell & spatial structures (May), vol, 81
Bischoff M, Ramm E (1997) Shear deformable shell elements for large strains and rotations. Int J Numer Methods Eng 40:445–452
Bishara D, Jabareen M (2019) A reduced mixed finite-element formulation for modeling the viscoelastic response of electro-active polymers at finite deformation. Math Mech Solids 24(5):1578–1610
Bishara D, Jabareen M (2020) Does the classical solid–shell element with the assumed natural strain method satisfy the three-dimensional patch test for arbitrary geometry? Finite Elem Anal Des 168:103331
Blok J, Legrand D (1969) Dielectric breakdown of polymer films. J Appl Phys 40(1):288–293
Braess D (1998) Enhanced assumed strain elements and locking in membrane problems. Comput Methods Appl Mech Eng 165:155–174
Büchter N, Ramm E, Roehl D (1994) Three-dimensional extension of non-linear shell formulation based on the enhanced assumed strain concept. Int J Numer Methods Eng 37(15):2551–2568
Cardoso R, Yoon J, Mahardika M, Choudhry S, Alves de Sousa R, Valente R (2008) Enhanced assumed strain (EAS) and assumed natural strain (ANS) methods for one-point quadrature solid–shell elements. Int J Numer Meth Eng 75:156–187
Carpi F, Menon C, De Rossi D (2009) Electroactive elastomeric actuator for all-polymer linear peristaltic pumps. IEEE/ASME Trans Mechatron 15(3):460–470
Caseiro J, Valente R, Reali A, Kiendl J, Auricchio F, Alves De Sousa R (2014) On the assumed natural strain method to alleviate locking in solid–shell NURBS-based finite elements. Comput Mech 53(6):341–1353
Chapelle D, Bathe K (1998) Fundamental considerations for the finite element analysis of shell structures. Comput Struct 66(1):19–36
Coleman B, Noll W (1963) The thermodynamics of elastic materials with heat conduction and viscosity. Arch Ration Mech Anal 13:167–178
Gil A, Ortigosa R (2016) A new framework for large strain electromechanics based on convex multi-variable strain energies: variational formulation and material characterisation. Comput Methods Appl Mech Eng 302:293–328
Green M, Tobolsky A (1946) A new approach to the theory of relaxing polymeric media. J Chem Phys 14:80–92
Hauptmann R, Schweizerhof K (1998) A systematic development of ’solid–shell’ formulations for linear and non-linear analysis employing only displacement degrees of freedom. Int J Numer Methods Eng 42:49–69
Hauptmann R, Schweizerhof K, Doll S (2000) Extension of the ‘solid–shell’ concept for application to large elastic and large elastoplastic deformations. Int J Numer Methods Eng 49:1121–1141
Jabareen M, Mtanes E (2016) A solid–shell Cosserat point element (SSCPE) for elastic thin structures at finite deformation. Comput Mech 2:1–31
Jordi C, Michel S, Fink E (2010) Fish-like propulsion of an airship with planar membrane dielectric elastomer actuators. Bioinspir biomim 5(2):026,007
Klinkel S, Wagner W (2006) A geometrically non-linear piezoelectric solid shell element based on a mixed multi-field variational formulation. IInt J Numer Methods Eng 65:349–382
Klinkel S, Zwecker S, Müller R (2013) A Solid Shell Finite Element Formulation for Dielectric Elastomers. J Appl Mech 80(2):021,026
Kornbluh R, Pelrine R, Gallagher P, Eckerle J, Czyzyk D, Shastri S, Pei Q (2003) Electroactive polymer animated devices. US Patent 6,586,859
Lee S, Goo N, Park H, Yoon K, Cho C (2003) A nine-node assumed strain shell element for analysis of a coupled electro-mechanical system. Smart Mater Struct 12:355–362
Lin-Quan Y, Li L (2005) An electric node concept for solid–shell elements for laminate composite piezoelectric structures. J Appl Mech 72:35–43
Lochmatter P (2007) Development of a shell-like electroactive polymer (eap) actuator. Ph.D. thesis, Swiss Federal Institute of Technology Zurich
Lubliner J (1985) A model of rubber viscoelasticity. Mech Res Commun 12:93–99
MacNeal R (1989) Toward a defect free four-noded membrane element. Finite Elem Anal Des 5:31–37
Mostafa M, Sivaselvan M, Felippa C (2013) A solid–shell corotational element based on ANDES, ANS and EAS for geometrically nonlinear structural analysis. Int J Numer Methods Eng 95:145–180
Ortigosa R, Gil A (2016) A new framework for large strain electromechanics based on convex multi-variable strain energies: conservation laws, hyperbolicity and extension to electro-magneto-mechanics. Comput Methods Appl Mech Eng 309:202–242
Ortigosa R, Gil A (2016) A new framework for large strain electromechanics based on convex multi-variable strain energies: finite element discretisation and computational implementation. Comput Methods Appl Mech Eng 302:329–360
Ortigosa R, Gil A (2017) A computational framework for incompressible electromechanics based on convex multi-variable strain energies for geometrically exact shell theory. Comput Methods Appl Mech Eng 317:792–816
Ortigosa R, Gil A, Lee C (2016) A computational framework for large strain nearly and truly incompressible electromechanics based on convex multi-variable strain energies. Comput Methods Appl Mech Eng 310:297–334
Parish H (1995) A continuum-based shell theory for nonlinear application. Int J Numer Methods Eng 38:1855–1883
Park H, Cho C, Lee S (1995) An efficient assumed strain element model with six dof per node for geometrically nonlinear shells. Int J Numer Methods Eng 38:4101–4122
Quak W (2007) A solid–shell element for use in sheet deformation processes and the EAS method. Master’s thesis, Mechanics of Forming Processes, Department of Mechanical Engineering University of Twente
Rah K, Van Paepegem W, Habraken A, Degrieck J, Alves de Sousa R, Valente R (2013) Optimal low-order fully integrated solid–shell elements. Comput Mech 51:309–326
Schwarze M, Reese S (2009) A reduced integration solid–shell element based on the EAS and the ANS concept—geometrically linear problems. Int J Numer Methods Eng 80:1322–1355
Schwarze M, Reese S (2011) A reduced integration solid–shell finite element based on the EAS and the ANS concept large deformation problems. Int J Numer Meth Eng 85:289–329
Senders C, Tollefson T (2010) Electroactive polymer actuation of implants. US Patent App. 12/733,077
Simo J, Armero F (1992) Geometrically non-linear enhanced strain mixed methods and the method of incompatible modes. Int J Numer Meth Eng 33:1413–1449
Simo J, Rifai M (1990) A class of mixed assumed strain methods and the method of incompatible modes. Int J Numer Methods Eng 29:1595–1638
Swayze J, Ortiz M (2008) Electroactive polymer-based pump. US Patent 7,353,747
Sze K, Ghali A (1993) A hexahedral element for plates, shells and beam by selective scaling. Int J Numer Methods Eng 36:1519–1540
Sze K, Tay M (1997) An explicit hybrid-stabilized eighteen node solid element for thin shell analysis. Int J Numer Methods Eng 40:1839–1856
Sze K, Zhu D (1999) An quadratic assumed natural strain curved triangular shell element. Comput Methods Appl Mech Eng 174:57–71
Valente R, Alves De Sousa R, Natal-Jorge R (2004) An enhanced strain 3D element for large deformation elastoplastic thin-shell applications. Comput Mech 34:38–52
Wissler M, Mazza E (2005) Modeling of a pre-strained circular actuator made of dielectric elastomers. Sens Actuators A 120:184–192
Wissler M, Mazza E (2007) Mechanical behavior of an acrylic elastomer used in dielectric elastomer actuators. Sens Actuators A Phys 134(2):494–504
Acknowledgements
Financial support for this work was provided by the Israel Science Foundation under Grant 1713/13, which is gratefully acknowledged. Also, M. Jabareen is supported by Neubauer Foundation.
Author information
Authors and Affiliations
Corresponding author
Additional information
Publisher's Note
Springer Nature remains neutral with regard to jurisdictional claims in published maps and institutional affiliations.
Appendices
Appendix A: details on the transformation matrices \(\underline{\underline{\mathbf {T}}}\) and \(\widetilde{\widetilde{\underline{\underline{\mathbf {T}}}}}\), and the interpolation matrix \(\underline{\underline{\mathbf {M}}}\)
The matrix \(\underline{\underline{\mathbf {T}}}\) in (53) is a \(6 \times 6\) transformation matrix with entries \(T_{i}^{j}=\mathbf {e}_{i}\cdot \mathbf {G}^{j}\) and it is reported by
Also, the transformation matrix \(\underline{\underline{{\widetilde{\mathbf {T}}}}}\) in (53) is defined by
where the transformation matrix \(\underline{\underline{\widetilde{\widetilde{\mathbf {T}}}}}\) consists of the differences between the constants \({G}_{ij}^{mn}\) and their interpolated counterparts \(\widetilde{G}_{ij}^{mn}\). Thus the rows of the in-plane components consists of zeros and it reads
The components \(\widetilde{\widetilde{G}}_{ij}^{mn} \) are defined by
The elements \(G_{33}^{mn}\), \(G_{13}^{mn}\) and \(G_{23}^{mn}\) of the matrix \(\underline{\underline{\widetilde{\widetilde{\mathbf {T}}}}}\) are defined by (37), while the elements \(\widetilde{G}_{33}^{mn}\), \(\widetilde{G}_{13}^{mn}\) and \(\widetilde{G}_{23}^{mn}\) are defined by (44).
Finally, the interpolation matrix \(\underline{\underline{\mathbf {M}}}\), which consists of the enhanced modes, is given by
Appendix B: developing the geometrical stiffness matrix
In this “Appendix”, the geometric matrix is derived. Thus, the dot product between the stress measure \(\overline{\mathbf {S}}\) and the linearization of the variation of the modified strain measure \(\varDelta \delta \mathbf {E}^{\textsf {Comp}}\) is rewritten using the Voigt notation as follows
where \(\underline{\overline{\mathbf {S}}}\) is a \(6 \times 1\) vector consisting of the modified second Piola-Kircchoff stress components defined by (87), and \({\varDelta \delta \underline{\mathbf {E}}^{\textsf {Comp}}}\) consists of the components of the linearized variation of the modified strain field, and it is defined by
Using (53), the vector \({\varDelta \delta \underline{\mathbf {E}}^{\textsf {Comp}}}\) is defined by
where the vectors \(\varDelta \delta \underline{\widetilde{\mathbf {E}}}^{\textsf {ANS}}\) and \(\varDelta \delta \underline{\widetilde{\mathbf {E}}}^{0}\) are defined by the following vectors
Substituting (104) into (102), it is possible to show that
where the two stress vectors \(\widetilde{\underline{\mathbf {S}}}\) and \(\widetilde{\widetilde{\underline{\mathbf {S}}}}\) are, respectively, given by
Applying the linearization operator on (67) and (73) yields
Moreover, the linearization of 68 takes the form,
Substituting (108) and (109) into (106) yields,
where the set of the coefficients \(G_{IJ}\) are given by
Finally, using (92), it can be shown that
where \(\underline{\underline{\mathbf {K}}}_{\text {G}}\) is the geometric stiffness matrix and takes the form
In which \(\underline{\underline{\mathbf {I}}}\) is the \(3\times 3\) identity matrix, and the set of the coefficients \(\overline{G}_{IJ}\) are defined by
Rights and permissions
About this article
Cite this article
Bishara, D., Jabareen, M. A solid–shell formulation based on the assumed natural inhomogeneous strains for modeling the viscoelastic response of electro-active polymers. Comput Mech 66, 1–25 (2020). https://doi.org/10.1007/s00466-020-01838-w
Received:
Accepted:
Published:
Issue Date:
DOI: https://doi.org/10.1007/s00466-020-01838-w