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A Cohesive Fatigue Model Based on the S-N DiagramThe relationship between fatigue life and fatigue crack propagation rate is explored with a new cohesive damage model. The parameters of the model are obtained from idealizations of S-N diagrams used in engineering design. The model is based on the hypothesis that both stable tearing damage and damage due to cyclic loading are representations of a density of microcracks and, therefore, a single damage variable can describe the state of damage. This assumption implies that the quasi-static cohesive law that describes tearing is also the envelope of the fatigue damage. Fatigue damage within the cohesive envelope is assumed to accumulate at a rate that depends on the displacement jumps. The fatigue model was implemented as a UMAT subroutine for Abaqus cohesive elements by adding fatigue damage accumulation to a cohesive model based on the Turon quasi-static cohesive law. The analyses were conducted using a simplified cyclic loading procedure in which the maximum applied load is kept constant and the computational expense of cycling the load is avoided. The predicted propagation rates for a double cantilever beam (DCB) specimen were compared to experimental results for IM7/8552 graphite/epoxy tape.
Document ID
20190033159
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Dávila, Carlos G.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
November 22, 2019
Publication Date
September 24, 2018
Subject Category
Structural Mechanics
Composite Materials
Report/Patent Number
NF1676L-29435
Meeting Information
Meeting: ASC Annual Technical Conference
Location: Seattle, WA
Country: United States
Start Date: September 24, 2018
End Date: September 26, 2018
Sponsors: American Society for Composites
Funding Number(s)
WBS: 826611.04.07.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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