2015
DOI: 10.1002/nme.4873
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A computational framework for the simulation of high‐speed multi‐material fluid–structure interaction problems with dynamic fracture

Abstract: A robust computational framework for the solution of fluid-structure interaction problems characterized by compressible flows and highly nonlinear structures undergoing pressure-induced dynamic fracture is presented. This framework is based on the finite volume method with exact Riemann solvers for the solution of multi-material problems. It couples a Eulerian, finite volume-based computational approach for solving flow problems with a Lagrangian, finite element-based computational approach for solving structu… Show more

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Cited by 56 publications
(59 citation statements)
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References 66 publications
(105 reference statements)
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“…Development of numerical methods for shock‐dominated multiphase fluid‐solid interaction problems is still an active research area . In this work, a recently developed computational framework is applied to simulate shock‐bubble‐stone interaction in SWL. This computational framework couples a finite volume 2‐phase computational fluid dynamics (CFD) solver, namely FIVER, with a finite element computational solid dynamics (CSD) solver using a second‐order accurate partitioned procedure .…”
Section: Introductionmentioning
confidence: 99%
See 1 more Smart Citation
“…Development of numerical methods for shock‐dominated multiphase fluid‐solid interaction problems is still an active research area . In this work, a recently developed computational framework is applied to simulate shock‐bubble‐stone interaction in SWL. This computational framework couples a finite volume 2‐phase computational fluid dynamics (CFD) solver, namely FIVER, with a finite element computational solid dynamics (CSD) solver using a second‐order accurate partitioned procedure .…”
Section: Introductionmentioning
confidence: 99%
“…The surface of the stone is represented as a dynamic embedded boundary in the CFD solver. The location of this embedded boundary with respect to the unstructured, noninterface‐conforming CFD mesh is tracked using robust and efficient computational geometry algorithms . The surface of the bubble is represented as an embedded interface in the CFD solver.…”
Section: Introductionmentioning
confidence: 99%
“…The asymptotic complexity of the FMM and other marching type methods is scriptOfalse(NflogNffalse), which is a substantial improvement over that of the naive approach. However, it was shown in the work of Grimberg and Farhat that for unsteady, viscous, FSI computations based on the SA turbulence model, which requires the computation of the distance to the wall, performed using explicit‐explicit time stepping, which is typically the most robust and efficient approach for simulating highly nonlinear unsteady FSI problems with potentially material failure (for example, see the works of Wang et al and Farhat et al), the cost of the computation of the distance to the wall using a fast marching type method can dominate the total computational cost of an Eulerian FSI simulation performed using an EBM, even in the absence of AMR.…”
Section: Other Enablersmentioning
confidence: 99%
“…To this end, the Eulerian framework of the AERO Suite of codes developed at Stanford University for the simulation of highly nonlinear FSI phenomena with topological changes is chosen to perform the FSI simulations of parachute inflation dynamics (PID) reported herein. This computational framework is equipped with the FIVER (finite volume method with exact two‐phase Riemann problems) embedded boundary method for FSI, which has been extensively verified and validated for complex multimaterial problems …”
Section: Application To the Simulation Of Parachute Inflation Dynamicsmentioning
confidence: 99%