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  reference  ©2012 Civil-Comp Ltd |  |  |  | S. Dumont1 and F. Jourdan2 1LAMFA, CNRS UMR 6140, Université de Picardie Jules Verne, France
 2LMGC, CNRS UMR 5508, Université Montpellier 2, France
 
 
Keywords: finite elements, space-time, four-dimensional mesh generation, elastodynamics, mesh adaptation.
 
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A space-time finite element method (STFEM) is proposed, in this paper,
for the resolution of mechanical problems including three dimensions in space
and one in time. For that purpose, we have developed a technique of four-dimesnional  mesh
generation adapted to space-time remeshing. The method has been tested on a
linearized elastodynamics problem. This original technique does not require
coarse-to-fine and fine-to-coarse mesh transfer operators and does not increase
the size of the linear systems to be solved, compared to the traditional finite
 element methods. Space-time meshes are made of simplex  finite elements.
Computations are realized in the context of the continuous Galerkin method.
The technique of mesh adaptation, propsed by the authors,  was applied to a problem of mobile loading.
The evolutionary mesh is able to follow the mobile loading zone.
 
The STFEM  can be regarded as an
extension of the classical  finite element method, applied to a boundary problem
resulting from a non-stationary problem. Currently, several approaches
exist. For example the large time increment method (LATIN), the Discontinuous Galerkin method, and the method proposed by the authors which
is a continuous Galerkin method. In most publications on the discontinuous
Galerkin method, the functions of interpolation are assumed to be
the product of functions of space variables and functions of time variables.
In this paper special attention is paid to  the non-separation of
the space and time variables. The reason of this choice is not
motivated by the accuracy of numerical results, but rather by what constitutes
the aim of this study: the remeshing. It can be seen that this kind of
interpolation is well-suited to mesh adaptation. The space-time mesh adaptation
developed is based on a method of mesh generation not structured
in space and time. The construction of four-dimesnional  meshes collides with the limits of
the representation. To overcome this drawback,  an automatic method
of construction, is propsed that is inspired by the two- and three-dimensional technique. The authors' technique of mesh
adaptation was applied to a problem of mobile load such as  contact forces. The
approach makes it possible to build an evolutionary mesh able to follow
the clamping zone. However, this technique does not require a mesh-to-mesh transfer operator
and makes it possible to preserve the same size of linear system on each
time slab.
 
It should be noted that one of the drawbacks of the STFEM  is the size of the systems to be solved. The
use of a laminated mesh does not require  the assembly of the total matrix of the
problem, but only the submatrices. This reduces the size of the systems to be
solved. The size of these linear systems is exactly the same as that obtained
in the case of approaches coupling an incremental method of the finite difference type to solve time integration,
with the "classic" finite element method to solve the space problem.
 
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