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Detecting and locating damage initiation and progression in full-scale sandwich composite fuselage panels using acoustic emission

In this study, acoustic emission was evaluated as a supplementary nondestructive testing method for detecting damage initiation and progression, identifying the site of damage, and anticipating ultimate fracture in notched full-scale honeycomb sandwich composite fuselage panels using redundant array...

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Published in:Journal of composite materials 2013-06, Vol.47 (13), p.1643-1664
Main Authors: Leone, Frank A, Ozevin, Didem, Awerbuch, Jonathan, Tan, Tein-Min
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Language:English
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cited_by cdi_FETCH-LOGICAL-c410t-7bf5ab5d278114b93b460f8a14f5a128a9a83d883b7cc2f330d26df788867b733
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creator Leone, Frank A
Ozevin, Didem
Awerbuch, Jonathan
Tan, Tein-Min
description In this study, acoustic emission was evaluated as a supplementary nondestructive testing method for detecting damage initiation and progression, identifying the site of damage, and anticipating ultimate fracture in notched full-scale honeycomb sandwich composite fuselage panels using redundant arrays of different acoustic emission sensor models. Each panel contained different damage scenarios and was subjected to combinations of quasi-static hoop and longitudinal loads. Damage progression and location were characterized with various inspection techniques, and the acoustic emission results were correlated with photogrammetric strain fields. Applying post-test signal processing, acoustic emission accurately detected notch tip damage initiation and tracked its progression to ultimate failure.
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subjects Acoustic emission
Airframes
Application fields
Applied sciences
Crack initiation
Damage
Exact sciences and technology
Fracture mechanics
Fuselages
Panels
Polymer industry, paints, wood
Progressions
Technology of polymers
title Detecting and locating damage initiation and progression in full-scale sandwich composite fuselage panels using acoustic emission
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