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NASA NTRS · 20140011508

Investigating Delamination Migration in Composite Tape Laminates

Abstract

A 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.

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BibTeXRIS

Ratcliffe, James G., DeCarvalho, Nelson V.. 2014-07-01. Investigating Delamination Migration in Composite Tape Laminates. https://ntrs.nasa.gov/citations/20140011508

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