Dynamic crush behaviors of aluminum honeycomb specimens under compression dominant inclined loads
The dynamic crush behaviors of aluminum 5052-H38 honeycomb specimens under compression dominant inclined loads are investigated by experiments. Different types of honeycomb specimens were designed for crush tests under pure compressive and compression dominant inclined loads with respect to the out-...
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Veröffentlicht in: | International Journal of Plasticity, 24(1):89-117 24(1):89-117, 2008, Vol.24 (1), p.89-117 |
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creator | Hong, Sung-Tae Pan, Jwo Tyan, Tau Prasad, Priya |
description | The dynamic crush behaviors of aluminum 5052-H38 honeycomb specimens under compression dominant inclined loads are investigated by experiments. Different types of honeycomb specimens were designed for crush tests under pure compressive and compression dominant inclined loads with respect to the out-of-plane direction. A test fixture was designed for dynamic crush tests under inclined loads. The results of the dynamic crush tests indicate that as the impact velocity increases, the normal crush strength increases and the shear strength remains nearly the same. The trends of the normalized normal crush strengths under inclined loads for specimens with different in-plane orientation angles as functions of the impact velocity are very similar to each other. Based on the experimental results, a macroscopic yield criterion as a function of the impact velocity is proposed. The experimental results suggest that, as the impact velocity increases, the shape of the macroscopic yield surface changes, or more specifically, the curvature of the yield surface increases near the pure compression state. The experimental results also show similar microscopic progressive folding mechanisms in honeycomb specimens under pure compressive and inclined loads. However, honeycomb specimens under inclined loads show inclined stacking patterns of folds due to the asymmetric location of horizontal plastic hinge lines. |
doi_str_mv | 10.1016/j.ijplas.2007.02.003 |
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(PNNL), Richland, WA (United States)</creatorcontrib><description>The dynamic crush behaviors of aluminum 5052-H38 honeycomb specimens under compression dominant inclined loads are investigated by experiments. Different types of honeycomb specimens were designed for crush tests under pure compressive and compression dominant inclined loads with respect to the out-of-plane direction. A test fixture was designed for dynamic crush tests under inclined loads. The results of the dynamic crush tests indicate that as the impact velocity increases, the normal crush strength increases and the shear strength remains nearly the same. The trends of the normalized normal crush strengths under inclined loads for specimens with different in-plane orientation angles as functions of the impact velocity are very similar to each other. Based on the experimental results, a macroscopic yield criterion as a function of the impact velocity is proposed. The experimental results suggest that, as the impact velocity increases, the shape of the macroscopic yield surface changes, or more specifically, the curvature of the yield surface increases near the pure compression state. The experimental results also show similar microscopic progressive folding mechanisms in honeycomb specimens under pure compressive and inclined loads. However, honeycomb specimens under inclined loads show inclined stacking patterns of folds due to the asymmetric location of horizontal plastic hinge lines.</description><identifier>ISSN: 0749-6419</identifier><identifier>EISSN: 1879-2154</identifier><identifier>DOI: 10.1016/j.ijplas.2007.02.003</identifier><identifier>CODEN: IJPLER</identifier><language>eng</language><publisher>Oxford: Elsevier Ltd</publisher><subject>ALUMINIUM ; Aluminum honeycombs ; aluminum honeysombs ; compession ; Compressing ; Compression ; COMPRESSION STRENGTH ; Crush tests ; Crushing ; Dynamic crush ; DYNAMIC LOADS ; Dynamics ; Exact sciences and technology ; Fracture mechanics (crack, fatigue, damage...) ; Fundamental areas of phenomenology (including applications) ; Honeycomb ; Honeycomb construction ; HONEYCOMB STRUCTURES ; Impact velocity ; Inclined stacking pattern ; Inelasticity (thermoplasticity, viscoplasticity...) ; Loads (forces) ; MATERIALS SCIENCE ; MECHANICAL TESTS ; ORIENTATION ; Physics ; Plasticity ; quasi-static crush ; SHEAR PROPERTIES ; Solid mechanics ; STATIC LOADS ; Structural and continuum mechanics ; Yield criterion</subject><ispartof>International Journal of Plasticity, 24(1):89-117, 2008, Vol.24 (1), p.89-117</ispartof><rights>2007 Elsevier Ltd</rights><rights>2007 INIST-CNRS</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c426t-e3c46cd9e6b11217f64cab07632370d3ad1ce55cfda915c711bef0ee3ad5c39e3</citedby></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://dx.doi.org/10.1016/j.ijplas.2007.02.003$$EHTML$$P50$$Gelsevier$$H</linktohtml><link.rule.ids>314,778,782,883,3539,4012,27906,27907,27908,45978</link.rule.ids><backlink>$$Uhttp://pascal-francis.inist.fr/vibad/index.php?action=getRecordDetail&idt=19193701$$DView record in Pascal Francis$$Hfree_for_read</backlink><backlink>$$Uhttps://www.osti.gov/biblio/921555$$D View this record in Osti.gov$$Hfree_for_read</backlink></links><search><creatorcontrib>Hong, Sung-Tae</creatorcontrib><creatorcontrib>Pan, Jwo</creatorcontrib><creatorcontrib>Tyan, Tau</creatorcontrib><creatorcontrib>Prasad, Priya</creatorcontrib><creatorcontrib>Pacific Northwest National Lab. (PNNL), Richland, WA (United States)</creatorcontrib><title>Dynamic crush behaviors of aluminum honeycomb specimens under compression dominant inclined loads</title><title>International Journal of Plasticity, 24(1):89-117</title><description>The dynamic crush behaviors of aluminum 5052-H38 honeycomb specimens under compression dominant inclined loads are investigated by experiments. Different types of honeycomb specimens were designed for crush tests under pure compressive and compression dominant inclined loads with respect to the out-of-plane direction. A test fixture was designed for dynamic crush tests under inclined loads. The results of the dynamic crush tests indicate that as the impact velocity increases, the normal crush strength increases and the shear strength remains nearly the same. The trends of the normalized normal crush strengths under inclined loads for specimens with different in-plane orientation angles as functions of the impact velocity are very similar to each other. Based on the experimental results, a macroscopic yield criterion as a function of the impact velocity is proposed. The experimental results suggest that, as the impact velocity increases, the shape of the macroscopic yield surface changes, or more specifically, the curvature of the yield surface increases near the pure compression state. The experimental results also show similar microscopic progressive folding mechanisms in honeycomb specimens under pure compressive and inclined loads. However, honeycomb specimens under inclined loads show inclined stacking patterns of folds due to the asymmetric location of horizontal plastic hinge lines.</description><subject>ALUMINIUM</subject><subject>Aluminum honeycombs</subject><subject>aluminum honeysombs</subject><subject>compession</subject><subject>Compressing</subject><subject>Compression</subject><subject>COMPRESSION STRENGTH</subject><subject>Crush tests</subject><subject>Crushing</subject><subject>Dynamic crush</subject><subject>DYNAMIC LOADS</subject><subject>Dynamics</subject><subject>Exact sciences and technology</subject><subject>Fracture mechanics (crack, fatigue, damage...)</subject><subject>Fundamental areas of phenomenology (including applications)</subject><subject>Honeycomb</subject><subject>Honeycomb construction</subject><subject>HONEYCOMB STRUCTURES</subject><subject>Impact velocity</subject><subject>Inclined stacking pattern</subject><subject>Inelasticity (thermoplasticity, viscoplasticity...)</subject><subject>Loads (forces)</subject><subject>MATERIALS SCIENCE</subject><subject>MECHANICAL TESTS</subject><subject>ORIENTATION</subject><subject>Physics</subject><subject>Plasticity</subject><subject>quasi-static crush</subject><subject>SHEAR PROPERTIES</subject><subject>Solid mechanics</subject><subject>STATIC LOADS</subject><subject>Structural and continuum mechanics</subject><subject>Yield criterion</subject><issn>0749-6419</issn><issn>1879-2154</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2008</creationdate><recordtype>article</recordtype><recordid>eNp9kU2L3DAMhkNpodNt_0EP7qGll6RW4iTjS6FsP2Ghl_ZsHFlhPCR2aiUL8-_XYRZ625NAevTx6i2KtyArkNB9Olf-vEyWq1rKvpJ1JWXzrDjAsddlDa16Xhxkr3TZKdAvi1fMZylle2zgUNivl2BnjwLTxicx0Mne-5hYxFHYaZt92GZxioEuGOdB8ELoZwostuAoiZxcEjH7GISLmbZhFT7g5AM5MUXr-HXxYrQT05vHeFP8_f7tz-3P8u73j1-3X-5KVHW3ltSg6tBp6gaAGvqxU2gH2XdN3fTSNdYBUtvi6KyGFnuAgUZJlAstNpqam-LddW7k1RtGvxKeMIZAuBqd39C2mflwZZYU_23Eq5k9I02TDRQ3No3Uqj12KoMfnwSh62G_S-mMqiuKKTInGs2S_GzTxYA0uz3mbK72mN0eI2uT7clt7x83WEY7jckG9Py_V4PO8yFzn68c5d_de0q7NApIzqddmYv-6UUPdj2phA</recordid><startdate>2008</startdate><enddate>2008</enddate><creator>Hong, Sung-Tae</creator><creator>Pan, Jwo</creator><creator>Tyan, Tau</creator><creator>Prasad, Priya</creator><general>Elsevier Ltd</general><general>Elsevier Science</general><scope>IQODW</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>7QF</scope><scope>7SR</scope><scope>7TB</scope><scope>8BQ</scope><scope>8FD</scope><scope>FR3</scope><scope>JG9</scope><scope>KR7</scope><scope>OTOTI</scope></search><sort><creationdate>2008</creationdate><title>Dynamic crush behaviors of aluminum honeycomb specimens under compression dominant inclined loads</title><author>Hong, Sung-Tae ; Pan, Jwo ; Tyan, Tau ; Prasad, Priya</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c426t-e3c46cd9e6b11217f64cab07632370d3ad1ce55cfda915c711bef0ee3ad5c39e3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2008</creationdate><topic>ALUMINIUM</topic><topic>Aluminum honeycombs</topic><topic>aluminum honeysombs</topic><topic>compession</topic><topic>Compressing</topic><topic>Compression</topic><topic>COMPRESSION STRENGTH</topic><topic>Crush tests</topic><topic>Crushing</topic><topic>Dynamic crush</topic><topic>DYNAMIC LOADS</topic><topic>Dynamics</topic><topic>Exact sciences and technology</topic><topic>Fracture mechanics (crack, fatigue, damage...)</topic><topic>Fundamental areas of phenomenology (including applications)</topic><topic>Honeycomb</topic><topic>Honeycomb construction</topic><topic>HONEYCOMB STRUCTURES</topic><topic>Impact velocity</topic><topic>Inclined stacking pattern</topic><topic>Inelasticity (thermoplasticity, viscoplasticity...)</topic><topic>Loads (forces)</topic><topic>MATERIALS SCIENCE</topic><topic>MECHANICAL TESTS</topic><topic>ORIENTATION</topic><topic>Physics</topic><topic>Plasticity</topic><topic>quasi-static crush</topic><topic>SHEAR PROPERTIES</topic><topic>Solid mechanics</topic><topic>STATIC LOADS</topic><topic>Structural and continuum mechanics</topic><topic>Yield criterion</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Hong, Sung-Tae</creatorcontrib><creatorcontrib>Pan, Jwo</creatorcontrib><creatorcontrib>Tyan, Tau</creatorcontrib><creatorcontrib>Prasad, Priya</creatorcontrib><creatorcontrib>Pacific Northwest National Lab. (PNNL), Richland, WA (United States)</creatorcontrib><collection>Pascal-Francis</collection><collection>CrossRef</collection><collection>Aluminium Industry Abstracts</collection><collection>Engineered Materials Abstracts</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>METADEX</collection><collection>Technology Research Database</collection><collection>Engineering Research Database</collection><collection>Materials Research Database</collection><collection>Civil Engineering Abstracts</collection><collection>OSTI.GOV</collection><jtitle>International Journal of Plasticity, 24(1):89-117</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Hong, Sung-Tae</au><au>Pan, Jwo</au><au>Tyan, Tau</au><au>Prasad, Priya</au><aucorp>Pacific Northwest National Lab. (PNNL), Richland, WA (United States)</aucorp><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Dynamic crush behaviors of aluminum honeycomb specimens under compression dominant inclined loads</atitle><jtitle>International Journal of Plasticity, 24(1):89-117</jtitle><date>2008</date><risdate>2008</risdate><volume>24</volume><issue>1</issue><spage>89</spage><epage>117</epage><pages>89-117</pages><issn>0749-6419</issn><eissn>1879-2154</eissn><coden>IJPLER</coden><abstract>The dynamic crush behaviors of aluminum 5052-H38 honeycomb specimens under compression dominant inclined loads are investigated by experiments. Different types of honeycomb specimens were designed for crush tests under pure compressive and compression dominant inclined loads with respect to the out-of-plane direction. A test fixture was designed for dynamic crush tests under inclined loads. The results of the dynamic crush tests indicate that as the impact velocity increases, the normal crush strength increases and the shear strength remains nearly the same. The trends of the normalized normal crush strengths under inclined loads for specimens with different in-plane orientation angles as functions of the impact velocity are very similar to each other. Based on the experimental results, a macroscopic yield criterion as a function of the impact velocity is proposed. The experimental results suggest that, as the impact velocity increases, the shape of the macroscopic yield surface changes, or more specifically, the curvature of the yield surface increases near the pure compression state. The experimental results also show similar microscopic progressive folding mechanisms in honeycomb specimens under pure compressive and inclined loads. However, honeycomb specimens under inclined loads show inclined stacking patterns of folds due to the asymmetric location of horizontal plastic hinge lines.</abstract><cop>Oxford</cop><pub>Elsevier Ltd</pub><doi>10.1016/j.ijplas.2007.02.003</doi><tpages>29</tpages></addata></record> |
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subjects | ALUMINIUM Aluminum honeycombs aluminum honeysombs compession Compressing Compression COMPRESSION STRENGTH Crush tests Crushing Dynamic crush DYNAMIC LOADS Dynamics Exact sciences and technology Fracture mechanics (crack, fatigue, damage...) Fundamental areas of phenomenology (including applications) Honeycomb Honeycomb construction HONEYCOMB STRUCTURES Impact velocity Inclined stacking pattern Inelasticity (thermoplasticity, viscoplasticity...) Loads (forces) MATERIALS SCIENCE MECHANICAL TESTS ORIENTATION Physics Plasticity quasi-static crush SHEAR PROPERTIES Solid mechanics STATIC LOADS Structural and continuum mechanics Yield criterion |
title | Dynamic crush behaviors of aluminum honeycomb specimens under compression dominant inclined loads |
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