An Experimental on Honeycomb Core in the Axial Direction under the Quasi-Static Loading
This paper focuses on the quasi-static response of the aluminum honeycomb core based on an experimental work. The load-compression and energy absorb characteristics of the out-of-plane aluminium honeycomb core are studied for three varieties of the core cell sizes which are 0.01905, 0.0127 and 0.006...
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Veröffentlicht in: | Applied Mechanics and Materials 2014-11, Vol.699 (Sustainable Energy and Development, Advanced Materials), p.405-410 |
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creator | bin Ahmad, Fauzi bin Pokaad, Alif Zulfakar bin Said, Md Radzai bin Kamaruddin, Mohd Nazeri |
description | This paper focuses on the quasi-static response of the aluminum honeycomb core based on an experimental work. The load-compression and energy absorb characteristics of the out-of-plane aluminium honeycomb core are studied for three varieties of the core cell sizes which are 0.01905, 0.0127 and 0.00635 m. The crushing tests were conducted on the Instron machine with a displacement control of 5 mm/min. The initial part in the load-displacement graph shows linear elastic characteristic, followed by a non-linear elastic-plastic regime before it collapses. Based on the observation, the cell sized 0.01905 m shows the global buckling collapse, but the cell sized 0.0127 and 0.00635 m collapse as progressive buckling mode. The cell size 0.00635 m shows highest energy absorption due to it has the highest density and it collapses like the progressive buckling mode compared with the others specimen. |
doi_str_mv | 10.4028/www.scientific.net/AMM.699.405 |
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The load-compression and energy absorb characteristics of the out-of-plane aluminium honeycomb core are studied for three varieties of the core cell sizes which are 0.01905, 0.0127 and 0.00635 m. The crushing tests were conducted on the Instron machine with a displacement control of 5 mm/min. The initial part in the load-displacement graph shows linear elastic characteristic, followed by a non-linear elastic-plastic regime before it collapses. Based on the observation, the cell sized 0.01905 m shows the global buckling collapse, but the cell sized 0.0127 and 0.00635 m collapse as progressive buckling mode. The cell size 0.00635 m shows highest energy absorption due to it has the highest density and it collapses like the progressive buckling mode compared with the others specimen.</description><identifier>ISSN: 1660-9336</identifier><identifier>ISSN: 1662-7482</identifier><identifier>ISBN: 3038353191</identifier><identifier>ISBN: 9783038353195</identifier><identifier>EISSN: 1662-7482</identifier><identifier>DOI: 10.4028/www.scientific.net/AMM.699.405</identifier><language>eng</language><publisher>Zurich: Trans Tech Publications Ltd</publisher><subject>Aluminium ; Aluminum ; Buckling ; Collapse ; Density ; Displacement ; Graphs ; Honeycomb cores</subject><ispartof>Applied Mechanics and Materials, 2014-11, Vol.699 (Sustainable Energy and Development, Advanced Materials), p.405-410</ispartof><rights>2015 Trans Tech Publications Ltd</rights><rights>Copyright Trans Tech Publications Ltd. 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The load-compression and energy absorb characteristics of the out-of-plane aluminium honeycomb core are studied for three varieties of the core cell sizes which are 0.01905, 0.0127 and 0.00635 m. The crushing tests were conducted on the Instron machine with a displacement control of 5 mm/min. The initial part in the load-displacement graph shows linear elastic characteristic, followed by a non-linear elastic-plastic regime before it collapses. Based on the observation, the cell sized 0.01905 m shows the global buckling collapse, but the cell sized 0.0127 and 0.00635 m collapse as progressive buckling mode. The cell size 0.00635 m shows highest energy absorption due to it has the highest density and it collapses like the progressive buckling mode compared with the others specimen.</description><subject>Aluminium</subject><subject>Aluminum</subject><subject>Buckling</subject><subject>Collapse</subject><subject>Density</subject><subject>Displacement</subject><subject>Graphs</subject><subject>Honeycomb cores</subject><issn>1660-9336</issn><issn>1662-7482</issn><issn>1662-7482</issn><isbn>3038353191</isbn><isbn>9783038353195</isbn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2014</creationdate><recordtype>article</recordtype><sourceid>BENPR</sourceid><recordid>eNqNkU9r2zAYh0W3QZt038FQKLs4kaw_li9lIU2XQcoYa-lRyLLcqiRSJskk-fZ91xQ6dtrJh9_DI1kPQpcETxiu5HS3202ScdZn1zsz8TZPZ7e3E9E0sPMTdEaEqMqayeoDGlFMJeWUNOTj64DLhlJxikYpPWMsGGHyDD3MfLHYb210G7DqdRF8sQzeHkzYtMU8RFs4X-QnW8z2DuZrF63JDqjBdza-Lj8HnVz5K-vsTLEKunP-8Rx96vU62c9v3zG6v1nczZfl6se37_PZqjSkprxsW8waZnlb912vpbZcE9bVFTWGacl70wrGSUs63rFeUoobXDWaVjXDreh5Tcfoy9G7jeH3YFNWG5eMXa-1t2FIighOWAU_3gB68Q_6HIbo4XZAVRJkQgqgro6UiSGlaHu1hbfR8aAIVn8iKIig3iMoiKAggoIIsHMQfD0KctQ-ZWue_jrn_xQvUv-Vsw</recordid><startdate>20141126</startdate><enddate>20141126</enddate><creator>bin Ahmad, Fauzi</creator><creator>bin Pokaad, Alif Zulfakar</creator><creator>bin Said, Md Radzai</creator><creator>bin Kamaruddin, Mohd Nazeri</creator><general>Trans Tech Publications Ltd</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7SR</scope><scope>7TB</scope><scope>8BQ</scope><scope>8FD</scope><scope>8FE</scope><scope>8FG</scope><scope>ABJCF</scope><scope>ABUWG</scope><scope>AFKRA</scope><scope>BENPR</scope><scope>BFMQW</scope><scope>BGLVJ</scope><scope>CCPQU</scope><scope>D1I</scope><scope>DWQXO</scope><scope>FR3</scope><scope>HCIFZ</scope><scope>JG9</scope><scope>KB.</scope><scope>KR7</scope><scope>L6V</scope><scope>M7S</scope><scope>PDBOC</scope><scope>PQEST</scope><scope>PQQKQ</scope><scope>PQUKI</scope><scope>PRINS</scope><scope>PTHSS</scope></search><sort><creationdate>20141126</creationdate><title>An Experimental on Honeycomb Core in the Axial Direction under the Quasi-Static Loading</title><author>bin Ahmad, Fauzi ; 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The load-compression and energy absorb characteristics of the out-of-plane aluminium honeycomb core are studied for three varieties of the core cell sizes which are 0.01905, 0.0127 and 0.00635 m. The crushing tests were conducted on the Instron machine with a displacement control of 5 mm/min. The initial part in the load-displacement graph shows linear elastic characteristic, followed by a non-linear elastic-plastic regime before it collapses. Based on the observation, the cell sized 0.01905 m shows the global buckling collapse, but the cell sized 0.0127 and 0.00635 m collapse as progressive buckling mode. The cell size 0.00635 m shows highest energy absorption due to it has the highest density and it collapses like the progressive buckling mode compared with the others specimen.</abstract><cop>Zurich</cop><pub>Trans Tech Publications Ltd</pub><doi>10.4028/www.scientific.net/AMM.699.405</doi><tpages>6</tpages></addata></record> |
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subjects | Aluminium Aluminum Buckling Collapse Density Displacement Graphs Honeycomb cores |
title | An Experimental on Honeycomb Core in the Axial Direction under the Quasi-Static Loading |
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