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Investigating Delamination Migration in Composite Tape LaminatesA modification to a recently developed test specimen designed to investigate migration of a delamination between neighboring ply interfaces in tape laminates is presented. The specimen is a cross-ply laminated beam consisting of 40 plies with a polytetrafluoroethylene insert spanning part way along its length. The insert is located between a lower 0-degree ply (specimen length direction) and a stack of four 90-degree plies (specimen width direction). The modification involved a stacking sequence that promotes stable delamination growth prior to migration, and included a relocation of the insert from the specimen midplane to the interface between plies 14 and 15. Specimens were clamped at both ends onto a rigid baseplate and loaded on their upper surface via a piano hinge assembly, resulting in a predominantly flexural loading condition. Tests were conducted with the load-application point positioned at various locations along a specimen's span. This position affected the sequence of damage events during a test.
Document ID
20140011508
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Ratcliffe, James G.
(NASA Langley Research Center Hampton, VA, United States)
DeCarvalho, Nelson V.
(National Inst. of Aerospace Hampton, VA, United States)
Date Acquired
September 10, 2014
Publication Date
July 1, 2014
Subject Category
Composite Materials
Report/Patent Number
NF1676L-19197
L-20432
NASA/TM-2014-218289
Funding Number(s)
WBS: WBS 794072.02.07.03.03
Distribution Limits
Public
Copyright
Public Use Permitted.
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