eprintid: 19562 rev_number: 16 eprint_status: archive userid: 1903 dir: disk0/00/01/95/62 datestamp: 2014-05-06 16:56:44 lastmod: 2016-04-21 20:18:04 status_changed: 2014-05-06 16:56:44 type: conference_item metadata_visibility: show item_issues_count: 0 creators_name: Latorre Ferrus, Marcos creators_name: Montans Leal, Francisco Javier title: WYPIWYG Hyperelasticity rights: by-nc-nd ispublished: pub subjects: aeronautica full_text_status: public pres_type: paper abstract: In this paper we describe a new promising procedure to model hyperelastic materials from given stress-strain data. The main advantage of the proposed method is that the user does not need to have a relevant knowledge of hyperelasticity, large strains or hyperelastic constitutive modelling. The engineer simply has to prescribe some stress strain experimental data (whether isotropic or anisotropic) in also user prescribed stress and strain measures and the model almost exactly replicates the experimental data. The procedure is based on the piece-wise splines model by Sussman and Bathe and may be easily generalized to transversely isotropic and orthotropic materials. The model is also amenable of efficient finite element implementation. In this paper we briefly describe the general procedure, addressing the advantages and limitations. We give predictions for arbitrary ?experimental data? and also give predictions for actual experiments of the behaviour of living soft tissues. The model may be also implemented in a general purpose finite element program. Since the obtained strain energy functions are analytic piece-wise functions, the constitutive tangent may be readily derived in order to be used for implicit static problems, where the equilibrium iterations must be performed and the material tangent is needed in order to preserve the quadratic rate of convergence of Newton procedures. date_type: published date: 2012-11-16 pagerange: 403-414 pages: 12 event_title: Issues on Mechanical Engineering event_location: Madrid event_dates: 16/11/2012 - 16/11/2012 event_type: conference institution: Aeronauticos department: Vehiculos_Aeroespaciales refereed: TRUE isbn: 978-84-939196-7-2 book_title: Issues on Mechanical Engineering referencetext: [1] Bathe, K.J., Finite Element Procedures. Prentice-Hall, New Jersey, 1996. [2] Kojic, M. & Bathe, K.J. Inelastic Analysis of Solids and Structures. Springer, Berlin, 2005. [3] Ogden, R.W. Non-linear Elastic Deformations. Dover, New York, 1997. [4] Simó, J.C. & Hughes, T.J.R. 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