Low-velocity Impact Characterization of Glass, Carbon and Kevlar Composites Using Repeated Drop Tests
Low-velocity (≅ 1.2-2.4 m/s) repeated drop weight impact tests were carried out on advanced composites (glass, carbon, kevlar in epoxy matrix - LY 556, HT 972) using an instrumented impact test machine (DYNATUP 8250). The incident energies ranged from 3.5 to 15 J (constant impactor mass 5.42 kg). Nu...
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Veröffentlicht in: | Journal of reinforced plastics and composites 2004-01, Vol.23 (15), p.1583-1599 |
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creator | Sugun, B. S. Rao, R. M. V. G. K. |
description | Low-velocity (≅ 1.2-2.4 m/s) repeated drop weight impact tests were carried out on advanced composites (glass, carbon, kevlar in epoxy matrix - LY 556, HT 972) using an instrumented impact test machine (DYNATUP 8250). The incident energies ranged from 3.5 to 15 J (constant impactor mass 5.42 kg). Number of drops to failure (Nf) data were obtained for the above with simultaneous recording of the load-time and energy-time traces. The extent of impact damage for glass and kevlar composites was interpreted using final delamination area maps (tracings).
Results for all the three composites showed that with an increase in drop numbers, the peak load (PL) steadily decreased while the total energy (Et) increased, until failure. Also, as the incident energy (Ein) was varied in arithmetic progression, the number of drops to failure (Nf) varied in harmonic progression. Finally it was concluded that repeated drop tests with final delamination area maps assist in understanding the impact damage tolerance of polymer composites. |
doi_str_mv | 10.1177/0731684404039798 |
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Results for all the three composites showed that with an increase in drop numbers, the peak load (PL) steadily decreased while the total energy (Et) increased, until failure. Also, as the incident energy (Ein) was varied in arithmetic progression, the number of drops to failure (Nf) varied in harmonic progression. Finally it was concluded that repeated drop tests with final delamination area maps assist in understanding the impact damage tolerance of polymer composites.</description><identifier>ISSN: 0731-6844</identifier><identifier>EISSN: 1530-7964</identifier><identifier>DOI: 10.1177/0731684404039798</identifier><identifier>CODEN: JRPCDW</identifier><language>eng</language><publisher>Thousand Oaks, CA: SAGE Publications</publisher><subject>Applied sciences ; Composites ; Exact sciences and technology ; Forms of application and semi-finished materials ; Laminates ; Polymer industry, paints, wood ; Technology of polymers</subject><ispartof>Journal of reinforced plastics and composites, 2004-01, Vol.23 (15), p.1583-1599</ispartof><rights>2005 INIST-CNRS</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c340t-488a0737ec3362cf9d09c62f5be8ea6b9c0df911665547be2e7fbc996fb156a3</citedby><cites>FETCH-LOGICAL-c340t-488a0737ec3362cf9d09c62f5be8ea6b9c0df911665547be2e7fbc996fb156a3</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://journals.sagepub.com/doi/pdf/10.1177/0731684404039798$$EPDF$$P50$$Gsage$$H</linktopdf><linktohtml>$$Uhttps://journals.sagepub.com/doi/10.1177/0731684404039798$$EHTML$$P50$$Gsage$$H</linktohtml><link.rule.ids>314,778,782,21802,27907,27908,43604,43605</link.rule.ids><backlink>$$Uhttp://pascal-francis.inist.fr/vibad/index.php?action=getRecordDetail&idt=16178708$$DView record in Pascal Francis$$Hfree_for_read</backlink></links><search><creatorcontrib>Sugun, B. S.</creatorcontrib><creatorcontrib>Rao, R. M. V. G. K.</creatorcontrib><title>Low-velocity Impact Characterization of Glass, Carbon and Kevlar Composites Using Repeated Drop Tests</title><title>Journal of reinforced plastics and composites</title><description>Low-velocity (≅ 1.2-2.4 m/s) repeated drop weight impact tests were carried out on advanced composites (glass, carbon, kevlar in epoxy matrix - LY 556, HT 972) using an instrumented impact test machine (DYNATUP 8250). The incident energies ranged from 3.5 to 15 J (constant impactor mass 5.42 kg). Number of drops to failure (Nf) data were obtained for the above with simultaneous recording of the load-time and energy-time traces. The extent of impact damage for glass and kevlar composites was interpreted using final delamination area maps (tracings).
Results for all the three composites showed that with an increase in drop numbers, the peak load (PL) steadily decreased while the total energy (Et) increased, until failure. Also, as the incident energy (Ein) was varied in arithmetic progression, the number of drops to failure (Nf) varied in harmonic progression. Finally it was concluded that repeated drop tests with final delamination area maps assist in understanding the impact damage tolerance of polymer composites.</description><subject>Applied sciences</subject><subject>Composites</subject><subject>Exact sciences and technology</subject><subject>Forms of application and semi-finished materials</subject><subject>Laminates</subject><subject>Polymer industry, paints, wood</subject><subject>Technology of polymers</subject><issn>0731-6844</issn><issn>1530-7964</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2004</creationdate><recordtype>article</recordtype><recordid>eNp1UEtLxDAQDqLg-rh7zEVPVpM2TZqj1CcuCLKeyzQ7Wbt0m5rpKvrr7bKCIHj6YL7HzHyMnUhxIaUxl8JkUhdKCSUya2yxwyYyz0RirFa7bLKhkw2_zw6IlkKkUik1YTgNH8k7tsE1wyd_WPXgBl6-QhwRY_MFQxM6Hjy_a4HonJcQ63EA3Zw_4nsLkZdh1QdqBiT-Qk234M_YIww459cx9HyGNNAR2_PQEh7_4CGb3d7Myvtk-nT3UF5NE5cpMSSqKGA81KDLMp06b-fCOp36vMYCQdfWibm3Umqd58rUmKLxtbNW-1rmGrJDdraN7WN4W4-Lq1VDDtsWOgxrqtIizYzKi1EotkIXA1FEX_WxWUH8rKSoNnVWf-scLac_2UAOWh-hcw39-rQ0hREbXbLVESywWoZ17MaP_8_9BkhPgjM</recordid><startdate>20040101</startdate><enddate>20040101</enddate><creator>Sugun, B. S.</creator><creator>Rao, R. M. V. G. K.</creator><general>SAGE Publications</general><general>Sage</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>20040101</creationdate><title>Low-velocity Impact Characterization of Glass, Carbon and Kevlar Composites Using Repeated Drop Tests</title><author>Sugun, B. S. ; Rao, R. M. V. G. K.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c340t-488a0737ec3362cf9d09c62f5be8ea6b9c0df911665547be2e7fbc996fb156a3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2004</creationdate><topic>Applied sciences</topic><topic>Composites</topic><topic>Exact sciences and technology</topic><topic>Forms of application and semi-finished materials</topic><topic>Laminates</topic><topic>Polymer industry, paints, wood</topic><topic>Technology of polymers</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Sugun, B. S.</creatorcontrib><creatorcontrib>Rao, R. M. V. G. K.</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 reinforced plastics and composites</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Sugun, B. S.</au><au>Rao, R. M. V. G. K.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Low-velocity Impact Characterization of Glass, Carbon and Kevlar Composites Using Repeated Drop Tests</atitle><jtitle>Journal of reinforced plastics and composites</jtitle><date>2004-01-01</date><risdate>2004</risdate><volume>23</volume><issue>15</issue><spage>1583</spage><epage>1599</epage><pages>1583-1599</pages><issn>0731-6844</issn><eissn>1530-7964</eissn><coden>JRPCDW</coden><abstract>Low-velocity (≅ 1.2-2.4 m/s) repeated drop weight impact tests were carried out on advanced composites (glass, carbon, kevlar in epoxy matrix - LY 556, HT 972) using an instrumented impact test machine (DYNATUP 8250). The incident energies ranged from 3.5 to 15 J (constant impactor mass 5.42 kg). Number of drops to failure (Nf) data were obtained for the above with simultaneous recording of the load-time and energy-time traces. The extent of impact damage for glass and kevlar composites was interpreted using final delamination area maps (tracings).
Results for all the three composites showed that with an increase in drop numbers, the peak load (PL) steadily decreased while the total energy (Et) increased, until failure. Also, as the incident energy (Ein) was varied in arithmetic progression, the number of drops to failure (Nf) varied in harmonic progression. Finally it was concluded that repeated drop tests with final delamination area maps assist in understanding the impact damage tolerance of polymer composites.</abstract><cop>Thousand Oaks, CA</cop><pub>SAGE Publications</pub><doi>10.1177/0731684404039798</doi><tpages>17</tpages></addata></record> |
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subjects | Applied sciences Composites Exact sciences and technology Forms of application and semi-finished materials Laminates Polymer industry, paints, wood Technology of polymers |
title | Low-velocity Impact Characterization of Glass, Carbon and Kevlar Composites Using Repeated Drop Tests |
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