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Full-Field Strain Methods for Investigating Failure Mechanisms in Triaxial Braided CompositesRecent advancements in braiding technology have led to commercially viable manufacturing approaches for making large structures with complex shape out of triaxial braided composite materials. In some cases, the static load capability of structures made using these materials has been higher than expected based on material strength properties measured using standard coupon tests. A more detailed investigation of deformation and failure processes in large-unit-cell-size triaxial braid composites is needed to evaluate the applicability of standard test methods for these materials and to develop alternative testing approaches. This report presents some new techniques that have been developed to investigate local deformation and failure using digital image correlation techniques. The methods were used to measure both local and global strains during standard straight-sided coupon tensile tests on composite materials made with 12- and 24-k yarns and a 0 /+60 /-60 triaxial braid architecture. Local deformation and failure within fiber bundles was observed and correlations were made between these local failures and global composite deformation and strength.
Document ID
20080043606
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Littell, Justin D.
(Akron Univ. Akron, OH, United States)
Binienda, Wieslaw K.
(Akron Univ. Akron, OH, United States)
Goldberg, Robert K.
(NASA Glenn Research Center Cleveland, OH, United States)
Roberts, Gary D.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
August 24, 2013
Publication Date
September 1, 2008
Subject Category
Composite Materials
Report/Patent Number
E-16413-1
NASA/TM-2008-215197
Report Number: E-16413-1
Report Number: NASA/TM-2008-215197
Funding Number(s)
WBS: WBS 877868.02.07.03.05.03
CONTRACT_GRANT: NNX07AK57H
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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