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From S-N to the Paris Law with a New Mixed-Mode Cohesive Fatigue ModelThe 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 mixed-mode cohesive laws. 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 in mode I and mixed mode were compared to experimental results for IM7/8552 graphite/epoxy tape. Several aspects of the results were investigated, including the effect of R-curves, the stress ratio R, and the difference between displacement control and force control.
Document ID
20180004395
Acquisition Source
Langley Research Center
Document Type
Technical Publication (TP)
Authors
Davila, Carlos G.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 10, 2018
Publication Date
June 1, 2018
Subject Category
Composite Materials
Report/Patent Number
NASA/TP-2018-219838
NF1676L-30358
Funding Number(s)
WBS: WBS 826611.04.07.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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