A virtual test facility for simulating detonation- and shock-induced deformation and fracture of thin flexible shells
A virtual test facility for simulating detonation- and shock-induced deformation and fracture of thin flexible shells
The coupling of a dynamically adaptive Eulerian Cartesian detonation solver with hierarchical time-step refinement to a Lagrangian thin-shell finite element solver with fracture and fragmentation capabilities is presented. The approach uses a level-set function to implicitly represent arbitrarily evolving solid structures on the Cartesian mesh. The auxiliary algorithm used to efficiently transform the shell solver mesh on the fly into a distance function is sketched briefly. We detail the derivation of the employed engineering combustion model that eliminates the numerical stiffness otherwise inherent to detonation waves and describe our approach to modeling fracture. The thin-shell solver utilizes a subdivision finite element discretization and achieves element separation with interface edges and a cohesive law. For method validation and benchmarking, the simulation of the deformation of a circular thin copper plate under impulsive pressure loading is presented. As a realistic computational application, we consider a three-dimensional setup in which the passage of an ethylene-oxygen detonation wave induces large plastic deformations and rupture of a thin-walled tubular specimen made of aluminum. Special attention is paid to the verification of the hydrodynamic loading conditions. The computational fluid-structure interaction results are found to be in agreement with experimental observations.
fluid-structure interaction, detonation model, thin-shells, large deformations, fracture, dynamic mesh adaptation, parallelization, water hammer
47-63
Deiterding, Ralf
ce02244b-6651-47e3-8325-2c0a0c9c6314
Cirak, Fehmi
2a142615-bc73-4c77-804b-fae9e420b88d
Mauch, Sean P.
ff8ca171-0843-4f64-b29f-05f7fd83777a
Meiron, Daniel I.
07cc49bc-9ca8-43b3-beb6-da2d1fd874f9
2007
Deiterding, Ralf
ce02244b-6651-47e3-8325-2c0a0c9c6314
Cirak, Fehmi
2a142615-bc73-4c77-804b-fae9e420b88d
Mauch, Sean P.
ff8ca171-0843-4f64-b29f-05f7fd83777a
Meiron, Daniel I.
07cc49bc-9ca8-43b3-beb6-da2d1fd874f9
Deiterding, Ralf, Cirak, Fehmi, Mauch, Sean P. and Meiron, Daniel I.
(2007)
A virtual test facility for simulating detonation- and shock-induced deformation and fracture of thin flexible shells.
International Journal for Multiscale Computational Engineering, 5 (1), .
(doi:10.1615/IntJMultCompEng.v5.i1.60).
Abstract
The coupling of a dynamically adaptive Eulerian Cartesian detonation solver with hierarchical time-step refinement to a Lagrangian thin-shell finite element solver with fracture and fragmentation capabilities is presented. The approach uses a level-set function to implicitly represent arbitrarily evolving solid structures on the Cartesian mesh. The auxiliary algorithm used to efficiently transform the shell solver mesh on the fly into a distance function is sketched briefly. We detail the derivation of the employed engineering combustion model that eliminates the numerical stiffness otherwise inherent to detonation waves and describe our approach to modeling fracture. The thin-shell solver utilizes a subdivision finite element discretization and achieves element separation with interface edges and a cohesive law. For method validation and benchmarking, the simulation of the deformation of a circular thin copper plate under impulsive pressure loading is presented. As a realistic computational application, we consider a three-dimensional setup in which the passage of an ethylene-oxygen detonation wave induces large plastic deformations and rupture of a thin-walled tubular specimen made of aluminum. Special attention is paid to the verification of the hydrodynamic loading conditions. The computational fluid-structure interaction results are found to be in agreement with experimental observations.
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Published date: 2007
Keywords:
fluid-structure interaction, detonation model, thin-shells, large deformations, fracture, dynamic mesh adaptation, parallelization, water hammer
Organisations:
Aerodynamics & Flight Mechanics Group
Identifiers
Local EPrints ID: 380618
URI: http://eprints.soton.ac.uk/id/eprint/380618
ISSN: 1543-1649
PURE UUID: c1e5fb2d-7ddc-4b41-9f64-b37ff59cbb7e
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Date deposited: 09 Sep 2015 10:59
Last modified: 15 Mar 2024 03:52
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Author:
Fehmi Cirak
Author:
Sean P. Mauch
Author:
Daniel I. Meiron
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