Ballistic Impact Behavior of Novel Coextruded Polycarbonate/Polymethyl Methacrylate Multilayers
Ballistic impact behavior of coextruded polycarbonate (PC)/polymethyl methacrylate (PMMA) composites consisting of 256, 1024, 2048, and 4096 layers with various composition has been evaluated. The individual layer thickness of PMMA was determined to be critical for the impact response of these multi...
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creator | Hsieh, Alex J DeSchepper, Daniel C Song, John W |
description | Ballistic impact behavior of coextruded polycarbonate (PC)/polymethyl methacrylate (PMMA) composites consisting of 256, 1024, 2048, and 4096 layers with various composition has been evaluated. The individual layer thickness of PMMA was determined to be critical for the impact response of these multilayers. A brittle/ductile transition occurred as evidenced by a significant increase in the damage zone size when the PMMA layer thickness was reduced to approximately 0.3 to 0.4 microns; a mixed mode of failure resulted in these composites. With the PMMA layer thickness further reduced to approximately 0.15 microns, ductile deformation, which was predominant in the PC control, occurred in the PC/PMMA multilayers, and the resulted damage zone was limited to the immediate vicinity of impact A brittle mode of failure, however, was encountered in all the PC/PMMA composites as the thickness of PMMA layers reached 0.5 microns or higher, regardless of their composition and layer configuration. Results of the ballistic impact energy measurements also revealed that the PMMA layer thickness was the critical parameter, and the determined impact energy values were consistently higher for the multilayers with PMMA layer thickness being 0.15 microns or thinner. In addition, microcracking in PMMA appeared to be the dominant mode of failure. Stress concentration associated with these microcracks in PMMA appeared to be insignificant to promote crack propagation across the ductile PC layers when the layer thickness of PMMA is below its critical value. |
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fullrecord | <record><control><sourceid>dtic_1RU</sourceid><recordid>TN_cdi_dtic_stinet_ADA358417</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>ADA358417</sourcerecordid><originalsourceid>FETCH-dtic_stinet_ADA3584173</originalsourceid><addsrcrecordid>eNrjZIh3SszJySwuyUxW8MwtSEwuUXBKzUgsy8wvUshPU_DLL0vNUXDOT60oKSpNSU1RCMjPqUxOLErKz0ssSdUH8XJTSzIqcxR8gVRiclFlDlBcwbc0pyQzJ7EytaiYh4E1LTGnOJUXSnMzyLi5hjh76KYArYwH2puXWhLv6OJobGphYmhuTEAaAFJ0OsY</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>report</recordtype></control><display><type>report</type><title>Ballistic Impact Behavior of Novel Coextruded Polycarbonate/Polymethyl Methacrylate Multilayers</title><source>DTIC Technical Reports</source><creator>Hsieh, Alex J ; DeSchepper, Daniel C ; Song, John W</creator><creatorcontrib>Hsieh, Alex J ; DeSchepper, Daniel C ; Song, John W ; ARMY RESEARCH LAB ABERDEEN PROVING GROUND MD</creatorcontrib><description>Ballistic impact behavior of coextruded polycarbonate (PC)/polymethyl methacrylate (PMMA) composites consisting of 256, 1024, 2048, and 4096 layers with various composition has been evaluated. The individual layer thickness of PMMA was determined to be critical for the impact response of these multilayers. A brittle/ductile transition occurred as evidenced by a significant increase in the damage zone size when the PMMA layer thickness was reduced to approximately 0.3 to 0.4 microns; a mixed mode of failure resulted in these composites. With the PMMA layer thickness further reduced to approximately 0.15 microns, ductile deformation, which was predominant in the PC control, occurred in the PC/PMMA multilayers, and the resulted damage zone was limited to the immediate vicinity of impact A brittle mode of failure, however, was encountered in all the PC/PMMA composites as the thickness of PMMA layers reached 0.5 microns or higher, regardless of their composition and layer configuration. Results of the ballistic impact energy measurements also revealed that the PMMA layer thickness was the critical parameter, and the determined impact energy values were consistently higher for the multilayers with PMMA layer thickness being 0.15 microns or thinner. In addition, microcracking in PMMA appeared to be the dominant mode of failure. Stress concentration associated with these microcracks in PMMA appeared to be insignificant to promote crack propagation across the ductile PC layers when the layer thickness of PMMA is below its critical value.</description><language>eng</language><subject>Armor ; ARMY RESEARCH ; BALLISTICS ; COEXTRUSION ; COMPOSITE MATERIALS ; CRACK PROPAGATION ; DAMAGE ; DEFORMATION ; DUCTILE BRITTLE TRANSITION ; ENERGY ; EXTRUSION ; FAILURE(MECHANICS) ; IMPACT ; LAYERS ; LIGHTWEIGHT ; Logistics, Military Facilities and Supplies ; MEASUREMENT ; MICROCRACKING ; MULTILAYERS ; MULTIMODE ; PE62618A ; POLYCARBONATES ; Polymer Chemistry ; POLYMERS ; POLYMETHYL METHACRYLATE ; STRESS CONCENTRATION ; THICKNESS</subject><creationdate>1998</creationdate><rights>APPROVED FOR PUBLIC RELEASE</rights><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>230,780,885,27567,27568</link.rule.ids><linktorsrc>$$Uhttps://apps.dtic.mil/sti/citations/ADA358417$$EView_record_in_DTIC$$FView_record_in_$$GDTIC$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Hsieh, Alex J</creatorcontrib><creatorcontrib>DeSchepper, Daniel C</creatorcontrib><creatorcontrib>Song, John W</creatorcontrib><creatorcontrib>ARMY RESEARCH LAB ABERDEEN PROVING GROUND MD</creatorcontrib><title>Ballistic Impact Behavior of Novel Coextruded Polycarbonate/Polymethyl Methacrylate Multilayers</title><description>Ballistic impact behavior of coextruded polycarbonate (PC)/polymethyl methacrylate (PMMA) composites consisting of 256, 1024, 2048, and 4096 layers with various composition has been evaluated. The individual layer thickness of PMMA was determined to be critical for the impact response of these multilayers. A brittle/ductile transition occurred as evidenced by a significant increase in the damage zone size when the PMMA layer thickness was reduced to approximately 0.3 to 0.4 microns; a mixed mode of failure resulted in these composites. With the PMMA layer thickness further reduced to approximately 0.15 microns, ductile deformation, which was predominant in the PC control, occurred in the PC/PMMA multilayers, and the resulted damage zone was limited to the immediate vicinity of impact A brittle mode of failure, however, was encountered in all the PC/PMMA composites as the thickness of PMMA layers reached 0.5 microns or higher, regardless of their composition and layer configuration. Results of the ballistic impact energy measurements also revealed that the PMMA layer thickness was the critical parameter, and the determined impact energy values were consistently higher for the multilayers with PMMA layer thickness being 0.15 microns or thinner. In addition, microcracking in PMMA appeared to be the dominant mode of failure. Stress concentration associated with these microcracks in PMMA appeared to be insignificant to promote crack propagation across the ductile PC layers when the layer thickness of PMMA is below its critical value.</description><subject>Armor</subject><subject>ARMY RESEARCH</subject><subject>BALLISTICS</subject><subject>COEXTRUSION</subject><subject>COMPOSITE MATERIALS</subject><subject>CRACK PROPAGATION</subject><subject>DAMAGE</subject><subject>DEFORMATION</subject><subject>DUCTILE BRITTLE TRANSITION</subject><subject>ENERGY</subject><subject>EXTRUSION</subject><subject>FAILURE(MECHANICS)</subject><subject>IMPACT</subject><subject>LAYERS</subject><subject>LIGHTWEIGHT</subject><subject>Logistics, Military Facilities and Supplies</subject><subject>MEASUREMENT</subject><subject>MICROCRACKING</subject><subject>MULTILAYERS</subject><subject>MULTIMODE</subject><subject>PE62618A</subject><subject>POLYCARBONATES</subject><subject>Polymer Chemistry</subject><subject>POLYMERS</subject><subject>POLYMETHYL METHACRYLATE</subject><subject>STRESS CONCENTRATION</subject><subject>THICKNESS</subject><fulltext>true</fulltext><rsrctype>report</rsrctype><creationdate>1998</creationdate><recordtype>report</recordtype><sourceid>1RU</sourceid><recordid>eNrjZIh3SszJySwuyUxW8MwtSEwuUXBKzUgsy8wvUshPU_DLL0vNUXDOT60oKSpNSU1RCMjPqUxOLErKz0ssSdUH8XJTSzIqcxR8gVRiclFlDlBcwbc0pyQzJ7EytaiYh4E1LTGnOJUXSnMzyLi5hjh76KYArYwH2puXWhLv6OJobGphYmhuTEAaAFJ0OsY</recordid><startdate>199810</startdate><enddate>199810</enddate><creator>Hsieh, Alex J</creator><creator>DeSchepper, Daniel C</creator><creator>Song, John W</creator><scope>1RU</scope><scope>BHM</scope></search><sort><creationdate>199810</creationdate><title>Ballistic Impact Behavior of Novel Coextruded Polycarbonate/Polymethyl Methacrylate Multilayers</title><author>Hsieh, Alex J ; DeSchepper, Daniel C ; Song, John W</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-dtic_stinet_ADA3584173</frbrgroupid><rsrctype>reports</rsrctype><prefilter>reports</prefilter><language>eng</language><creationdate>1998</creationdate><topic>Armor</topic><topic>ARMY RESEARCH</topic><topic>BALLISTICS</topic><topic>COEXTRUSION</topic><topic>COMPOSITE MATERIALS</topic><topic>CRACK PROPAGATION</topic><topic>DAMAGE</topic><topic>DEFORMATION</topic><topic>DUCTILE BRITTLE TRANSITION</topic><topic>ENERGY</topic><topic>EXTRUSION</topic><topic>FAILURE(MECHANICS)</topic><topic>IMPACT</topic><topic>LAYERS</topic><topic>LIGHTWEIGHT</topic><topic>Logistics, Military Facilities and Supplies</topic><topic>MEASUREMENT</topic><topic>MICROCRACKING</topic><topic>MULTILAYERS</topic><topic>MULTIMODE</topic><topic>PE62618A</topic><topic>POLYCARBONATES</topic><topic>Polymer Chemistry</topic><topic>POLYMERS</topic><topic>POLYMETHYL METHACRYLATE</topic><topic>STRESS CONCENTRATION</topic><topic>THICKNESS</topic><toplevel>online_resources</toplevel><creatorcontrib>Hsieh, Alex J</creatorcontrib><creatorcontrib>DeSchepper, Daniel C</creatorcontrib><creatorcontrib>Song, John W</creatorcontrib><creatorcontrib>ARMY RESEARCH LAB ABERDEEN PROVING GROUND MD</creatorcontrib><collection>DTIC Technical Reports</collection><collection>DTIC STINET</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Hsieh, Alex J</au><au>DeSchepper, Daniel C</au><au>Song, John W</au><aucorp>ARMY RESEARCH LAB ABERDEEN PROVING GROUND MD</aucorp><format>book</format><genre>unknown</genre><ristype>RPRT</ristype><btitle>Ballistic Impact Behavior of Novel Coextruded Polycarbonate/Polymethyl Methacrylate Multilayers</btitle><date>1998-10</date><risdate>1998</risdate><abstract>Ballistic impact behavior of coextruded polycarbonate (PC)/polymethyl methacrylate (PMMA) composites consisting of 256, 1024, 2048, and 4096 layers with various composition has been evaluated. The individual layer thickness of PMMA was determined to be critical for the impact response of these multilayers. A brittle/ductile transition occurred as evidenced by a significant increase in the damage zone size when the PMMA layer thickness was reduced to approximately 0.3 to 0.4 microns; a mixed mode of failure resulted in these composites. With the PMMA layer thickness further reduced to approximately 0.15 microns, ductile deformation, which was predominant in the PC control, occurred in the PC/PMMA multilayers, and the resulted damage zone was limited to the immediate vicinity of impact A brittle mode of failure, however, was encountered in all the PC/PMMA composites as the thickness of PMMA layers reached 0.5 microns or higher, regardless of their composition and layer configuration. Results of the ballistic impact energy measurements also revealed that the PMMA layer thickness was the critical parameter, and the determined impact energy values were consistently higher for the multilayers with PMMA layer thickness being 0.15 microns or thinner. In addition, microcracking in PMMA appeared to be the dominant mode of failure. Stress concentration associated with these microcracks in PMMA appeared to be insignificant to promote crack propagation across the ductile PC layers when the layer thickness of PMMA is below its critical value.</abstract><oa>free_for_read</oa></addata></record> |
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source | DTIC Technical Reports |
subjects | Armor ARMY RESEARCH BALLISTICS COEXTRUSION COMPOSITE MATERIALS CRACK PROPAGATION DAMAGE DEFORMATION DUCTILE BRITTLE TRANSITION ENERGY EXTRUSION FAILURE(MECHANICS) IMPACT LAYERS LIGHTWEIGHT Logistics, Military Facilities and Supplies MEASUREMENT MICROCRACKING MULTILAYERS MULTIMODE PE62618A POLYCARBONATES Polymer Chemistry POLYMERS POLYMETHYL METHACRYLATE STRESS CONCENTRATION THICKNESS |
title | Ballistic Impact Behavior of Novel Coextruded Polycarbonate/Polymethyl Methacrylate Multilayers |
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