TY - JOUR
T1 - An adaptive space-time finite element model for oxidation-driven fracture
AU - Carranza, F. L.
AU - Fang, B.
AU - Haber, R. B.
N1 - Funding Information:
This work was supportedi n part by NASA Grant No. NGT-70374 and a researcha ssistantshipa wardedb y the Computational Science & Engineering Program of the University of Illinois at Urbana-Champaign. Computations were performed on the Silicon Graphics POWER CHALLENGE array at the National Center for Supercomputing Applications, Urbana, Illinois.
PY - 1998/5/11
Y1 - 1998/5/11
N2 - This paper presents an adaptive, space-time finite element model for oxidation-driven fracture. The model incorporates finite-deformation viscoplastic material behaviour, stress-enhanced diffusive transport of reactive chemical species and a cohesive interface fracture criterion. We describe in detail the variational formulation of the coupled system, with particular attention to stabilized discontinuous Galerkin formulations for the chemical diffusion and the material evolution equations. We describe a new computational approach for simulating fracture that uses space-time finite elements to track continuous crack-tip motion. This provides an accurate representation of the deformation history in ductile fracture, as is required for the reliable integration of the evolution equations for history-dependent materials. The space-time model supports both transient and direct steady-state calculations. It promotes efficient computations by eliminating the need for extensive mesh refinement away from the current crack-tip location and by exploiting the temporal coherence availabel in problems formulated in a moxing crack-tip frame. An h-adaptive finite element procedure reveals the potential of the space-time model for controlling element distortion and maintaining solution accuracy. Numerical studies of mode-III fracture, plane-strain mode-I fracture and stress-enhanced diffusion illustrate the importance of stabilization and adaptivity for obtaining accurate and reliable solutions.
AB - This paper presents an adaptive, space-time finite element model for oxidation-driven fracture. The model incorporates finite-deformation viscoplastic material behaviour, stress-enhanced diffusive transport of reactive chemical species and a cohesive interface fracture criterion. We describe in detail the variational formulation of the coupled system, with particular attention to stabilized discontinuous Galerkin formulations for the chemical diffusion and the material evolution equations. We describe a new computational approach for simulating fracture that uses space-time finite elements to track continuous crack-tip motion. This provides an accurate representation of the deformation history in ductile fracture, as is required for the reliable integration of the evolution equations for history-dependent materials. The space-time model supports both transient and direct steady-state calculations. It promotes efficient computations by eliminating the need for extensive mesh refinement away from the current crack-tip location and by exploiting the temporal coherence availabel in problems formulated in a moxing crack-tip frame. An h-adaptive finite element procedure reveals the potential of the space-time model for controlling element distortion and maintaining solution accuracy. Numerical studies of mode-III fracture, plane-strain mode-I fracture and stress-enhanced diffusion illustrate the importance of stabilization and adaptivity for obtaining accurate and reliable solutions.
UR - http://www.scopus.com/inward/record.url?scp=0032507578&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=0032507578&partnerID=8YFLogxK
U2 - 10.1016/S0045-7825(97)00248-X
DO - 10.1016/S0045-7825(97)00248-X
M3 - Conference article
AN - SCOPUS:0032507578
SN - 0045-7825
VL - 157
SP - 399
EP - 423
JO - Computer Methods in Applied Mechanics and Engineering
JF - Computer Methods in Applied Mechanics and Engineering
IS - 3-4
T2 - Proceedings of the 1996 7th Conference on Numerical Methods and Computational Mechanics in Science and Engineering, NMCM 96
Y2 - 15 July 1996 through 19 July 1996
ER -