NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Influence of Finite Element Software on Energy Release Rates Computed Using the Virtual Crack Closure TechniqueStrain energy release rates were computed along straight delamination fronts of Double Cantilever Beam, End-Notched Flexure and Single Leg Bending specimens using the Virtual Crack Closure Technique (VCCT). Th e results were based on finite element analyses using ABAQUS# and ANSYS# and were calculated from the finite element results using the same post-processing routine to assure a consistent procedure. Mixed-mode strain energy release rates obtained from post-processing finite elem ent results were in good agreement for all element types used and all specimens modeled. Compared to previous studies, the models made of s olid twenty-node hexahedral elements and solid eight-node incompatible mode elements yielded excellent results. For both codes, models made of standard brick elements and elements with reduced integration did not correctly capture the distribution of the energy release rate acr oss the width of the specimens for the models chosen. The results suggested that element types with similar formulation yield matching results independent of the finite element software used. For comparison, m ixed-mode strain energy release rates were also calculated within ABAQUS#/Standard using the VCCT for ABAQUS# add on. For all specimens mod eled, mixed-mode strain energy release rates obtained from ABAQUS# finite element results using post-processing were almost identical to re sults calculated using the VCCT for ABAQUS# add on.
Document ID
20060056392
Acquisition Source
Langley Research Center
Document Type
Contractor Report (CR)
Authors
Krueger, Ronald
(National Inst. of Aerospace Hampton, VA, United States)
Goetze, Dirk
(University of Stuttgart Stuttgart, Germany)
Ransom, Jonathon
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 7, 2013
Publication Date
October 1, 2006
Subject Category
Composite Materials
Report/Patent Number
NIA Reprt No. 2006-06
NASA/CR-2006-214523
Funding Number(s)
CONTRACT_GRANT: NAS1-02117
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available