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Analysis of the Influence of Layer Shifting on the Elastic Response and Damage Nucleation and Growth in Woven Composite LaminatesThe influence of relative layer shifting on the elastic and damage response of plain weave composite laminates is analyzed using a continuum damage mechanics approach in combination with the finite element method. First, the homogenized properties of the woven composite as a function of the number of layers and of layer shifting are presented. Next, the damage development in various shifting configurations is studied using different damage constitutive models for the matrix and the fiber bundles. It is shown that the impact of layer shifting on both the elastic response and the nonlinear damage response is significant. Most notably, the model captures changes in the damage mechanisms within the woven composite that occur due to layer shifting, resulting in stiffer, more brittle behavior, which has been shown experimentally in the literature. Model results in the linear and nonlinear regimes are shown to be consistent with both an independent analytical model and reported experiments.
Document ID
20180007181
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Espadas-Escalante, Juan Jose
(Uppsala Univ. Uppsala, Sweden)
Bednarcyk, Brett A.
(NASA Glenn Research Center Cleveland, OH, United States)
Isaksson, Per
(Uppsala Univ. Uppsala, Sweden)
Date Acquired
October 30, 2018
Publication Date
September 1, 2018
Subject Category
Composite Materials
Report/Patent Number
GRC-E-DAA-TN54147
NASA/TM-2018- 219950
E-19561
Funding Number(s)
WBS: WBS 409492.02.03.01.30.01
CONTRACT_GRANT: CONACYT 383215
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
layer shifting
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