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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 |
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container_title | Journal of composite materials |
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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. |
doi_str_mv | 10.1177/0021998312450306 |
format | article |
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Applying post-test signal processing, acoustic emission accurately detected notch tip damage initiation and tracked its progression to ultimate failure.</description><subject>Acoustic emission</subject><subject>Airframes</subject><subject>Application fields</subject><subject>Applied sciences</subject><subject>Crack initiation</subject><subject>Damage</subject><subject>Exact sciences and technology</subject><subject>Fracture mechanics</subject><subject>Fuselages</subject><subject>Panels</subject><subject>Polymer industry, paints, wood</subject><subject>Progressions</subject><subject>Technology of polymers</subject><issn>0021-9983</issn><issn>1530-793X</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2013</creationdate><recordtype>article</recordtype><recordid>eNp1UE1LxDAQDaLgunr3mIvgpZo0bZMeZf2EBS8K3kqapmuWNKmZFvHoPzftLh4ET8PMe_PmzUPonJIrSjm_JiSlZSkYTbOcMFIcoAXNGUl4yd4O0WKCkwk_RicAW0IIp1mxQN-3etBqMG6DpWuw9UrOTSM7udHYODOYOPFuhvvgN0EDTL1xuB2tTUBJqzFE-NOod6x813swg44oaDuJ9NJpC3iE-YryIwxGYd2ZWegUHbXSgj7b1yV6vb97WT0m6-eHp9XNOlEZJUPC6zaXdd6kXFCa1SWrs4K0QtIszmkqZCkFa4RgNVcqbRkjTVo0LRdCFLzmjC3R5U43PvExahiqaEBpa6O7aKmijKdFnmecRirZUVXwAEG3VR9MJ8NXRUk1pV39TTuuXOzV5RRIG6RTBn73Up4xURQk8pIdD2Iy1daPwcWn_9f9AQtUjis</recordid><startdate>20130601</startdate><enddate>20130601</enddate><creator>Leone, Frank A</creator><creator>Ozevin, Didem</creator><creator>Awerbuch, Jonathan</creator><creator>Tan, Tein-Min</creator><general>SAGE Publications</general><general>Sage Publications</general><scope>IQODW</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>7SR</scope><scope>8FD</scope><scope>H8D</scope><scope>JG9</scope><scope>L7M</scope></search><sort><creationdate>20130601</creationdate><title>Detecting and locating damage initiation and progression in full-scale sandwich composite fuselage panels using acoustic emission</title><author>Leone, Frank A ; Ozevin, Didem ; Awerbuch, Jonathan ; Tan, Tein-Min</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c410t-7bf5ab5d278114b93b460f8a14f5a128a9a83d883b7cc2f330d26df788867b733</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2013</creationdate><topic>Acoustic emission</topic><topic>Airframes</topic><topic>Application fields</topic><topic>Applied sciences</topic><topic>Crack initiation</topic><topic>Damage</topic><topic>Exact sciences and technology</topic><topic>Fracture mechanics</topic><topic>Fuselages</topic><topic>Panels</topic><topic>Polymer industry, paints, wood</topic><topic>Progressions</topic><topic>Technology of polymers</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Leone, Frank A</creatorcontrib><creatorcontrib>Ozevin, Didem</creatorcontrib><creatorcontrib>Awerbuch, Jonathan</creatorcontrib><creatorcontrib>Tan, Tein-Min</creatorcontrib><collection>Pascal-Francis</collection><collection>CrossRef</collection><collection>Engineered Materials Abstracts</collection><collection>Technology Research Database</collection><collection>Aerospace Database</collection><collection>Materials Research Database</collection><collection>Advanced Technologies Database with Aerospace</collection><jtitle>Journal of composite materials</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Leone, Frank A</au><au>Ozevin, Didem</au><au>Awerbuch, Jonathan</au><au>Tan, Tein-Min</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Detecting and locating damage initiation and progression in full-scale sandwich composite fuselage panels using acoustic emission</atitle><jtitle>Journal of composite materials</jtitle><date>2013-06-01</date><risdate>2013</risdate><volume>47</volume><issue>13</issue><spage>1643</spage><epage>1664</epage><pages>1643-1664</pages><issn>0021-9983</issn><eissn>1530-793X</eissn><coden>JCOMBI</coden><abstract>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. 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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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