[en] NURBS-based isogeometric analysis was first extended to thin shell/membrane structures which allows for
finite membrane stretching as well as large deflection and bending strain. The assumed non-linear
kinematics employs the Kirchhoff-Love shell theory to describe the mechanical behaviour of thin to ultrathin
structures. The displacement fields are interpolated from the displacements of control points only, and
no rotational degrees of freedom are used at control points. Due to the high order Ck (k ≥ 1) continuity of
NURBS shape functions the Kirchhoff-Love theory can be seamlessly implemented. An explicit time
integration scheme is used to compute the transient response of membrane structures to time-domain
excitations, and a dynamic relaxation method is employed to obtain steady-state solutions. The versatility
and good performance of the present formulation is demonstrated with the aid of a number of test cases,
including a square membrane strip under static pressure, the inflation of a spherical shell under internal
pressure, the inflation of a square airbag and the inflation of a rubber balloon. The mechanical contribution
of the bending stiffness is also evaluated.
Disciplines :
Ingénierie, informatique & technologie: Multidisciplinaire, généralités & autres
Auteur, co-auteur :
Chen, Lei
Nguyen-Thanh, Nhon
Nguyen-Xuan, Hung
Rabczuk, Timon
BORDAS, Stéphane ; University of Luxembourg > Faculty of Science, Technology and Communication (FSTC) > Engineering Research Unit
Limbert, Georges
Langue du document :
Anglais
Titre :
Explicit finite deformation analysis of isogeometric membranes
Titre traduit :
[fr] Déformations explicites de membranes isogéométriques
Date de publication/diffusion :
2014
Titre du périodique :
Computer Methods in Applied Mechanics and Engineering
ISSN :
0045-7825
Maison d'édition :
Elsevier Science, Lausanne, Suisse
Peer reviewed :
Peer reviewed
Focus Area :
Computational Sciences
Projet européen :
FP7 - 279578 - REALTCUT - Towards real time multiscale simulation of cutting in non-linear materials with applications to surgical simulation and computer guided surgery
Organisme subsidiant :
European Office of Aerospace Research and Development (Air Force Office of Scientific Research) [Grant FA8655-12-1-2103] and the Engineering and Physical Sciences Research Council (EPSRC) [Grant EP/F034296/1]. CE - Commission Européenne