| Reference : Explicit finite deformation analysis of isogeometric membranes |
| Scientific journals : Article | |||
| Engineering, computing & technology : Multidisciplinary, general & others | |||
| Computational Sciences | |||
| http://hdl.handle.net/10993/16438 | |||
| Explicit finite deformation analysis of isogeometric membranes | |
| English | |
| [fr] Déformations explicites de membranes isogéométriques | |
| 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 [> >] | |
| 2014 | |
| Computer Methods in Applied Mechanics and Engineering | |
| Elsevier Science | |
| Yes (verified by ORBilu) | |
| International | |
| 0045-7825 | |
| Lausanne | |
| Switzerland | |
| [en] explicit ; isogeometric ; membrane | |
| [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. | |
| 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]. | |
| Researchers ; Professionals ; Students ; General public ; Others | |
| http://hdl.handle.net/10993/16438 | |
| FP7 ; 279578 - REALTCUT - Towards real time multiscale simulation of cutting in non-linear materials with applications to surgical simulation and computer guided surgery |
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