{ "ok": true, "doi": "10.46243/jst.2020.v5.i6.pp128-140", "events": [ { "seq": 1, "kind": "register", "at": "2026-09-29 22:00:23", "by": "Administrator (admin)", "by_kind": "user", "note": "registered at Crossref; record read from api.crossref.org", "changes": [ { "path": "abstract.lang", "from": null, "to": "en" }, { "path": "abstract.value", "from": null, "to": "This paper examines the expediency of interface elements in modeling of impact damage analysis for Eglass composite laminate under low velocity impact test. Numerical modelsare built adopting cohesive interface behavior to authenticate the cross-ply damage response; and successively used the strategy to model the impact response of quasi-isotropic composite laminate. Impact test are performed to characterize the induced-damage behavior in quasi-isotropic composite laminate at different impact energy test in terms of impact force, displacement and damage size as well as the stress failure trajectory. Numerical result shows reliability of the model for structural impact analysisin damage initiation and progression in laminated composite plates. The simulation result though reveals large deformation, yet, did not yield in total fracture. This development shows the importance of adopting interface elements in structural impact damage criterion to trigger constraints effect on initiation phase.The study also reveals that the bottom most surface suffers huge deformation compare to the impact surface. It divulges that the extent of damage area in each ply of the composite laminate orients in the fiber direction in ‘star-shaped contour. The main novelty is the capability of using this model for structural impact analysis on both cross-ply and quasi-isotropic composite laminate." }, { "path": "agents.0.name.org", "from": null, "to": "Longman Publishers" }, { "path": "agents.0.role", "from": null, "to": "publisher" }, { "path": "characters.0", "from": null, "to": "Language" }, { "path": "container.identifiers.0.medium", "from": null, "to": "electronic" }, { "path": "container.identifiers.0.type", "from": null, "to": "ISSN" }, { "path": "container.identifiers.0.value", "from": null, "to": "2456-5660" }, { "path": "container.issue", "from": null, "to": "Volume 5" }, { "path": "container.pages.first", "from": null, "to": "128" }, { "path": "container.pages.last", "from": null, "to": "140" }, { "path": "container.titles.0.type", "from": null, "to": "PrincipalTitle" }, { "path": "container.titles.0.value", "from": null, "to": "Journal of Science & Technology" }, { "path": "container.type", "from": null, "to": "Journal" }, { "path": "dates.date_type", "from": null, "to": "PublicationDate" }, { "path": "dates.online", "from": null, "to": "2020-10-25" }, { "path": "dates.published", "from": null, "to": "2020-10-25" }, { "path": "doi", "from": null, "to": "10.46243/jst.2020.v5.i6.pp128-140" }, { "path": "format", "from": null, "to": "smartscholars-doi-metadata/1.0" }, { "path": "identifiers.0.type", "from": null, "to": "DOI" }, { "path": "identifiers.0.value", "from": null, "to": "10.46243/jst.2020.v5.i6.pp128-140" }, { "path": "language", "from": null, "to": "en" }, { "path": "license.applies_to", "from": null, "to": "vor" }, { "path": "license.start", "from": null, "to": "2020-10-25" }, { "path": "license.url", "from": null, "to": "https://creativecommons.org/licenses/by/4.0" }, { "path": "links.0.primary", "from": null, "to": true }, { "path": "links.0.return_type", "from": null, "to": "text/html" }, { "path": "links.0.url", "from": null, "to": "https://www.jst.org.in/index.php/pub/article/view/547" }, { "path": "links.1.purpose", "from": null, "to": "text-mining" }, { "path": "links.1.return_type", "from": null, "to": "application/pdf" }, { "path": "links.1.url", "from": null, "to": "https://www.jst.org.in/index.php/pub/article/download/547/488" }, { "path": "links.2.purpose", "from": null, "to": "text-mining" }, { "path": "links.2.return_type", "from": null, "to": "application/xml" }, { "path": "links.2.url", "from": null, "to": "https://www.jst.org.in/index.php/pub/article/download/547/1517" }, { "path": "modes.0", "from": null, "to": "Visual" }, { "path": "record.issue_number", "from": null, "to": 1 }, { "path": "record.registered", "from": null, "to": "2020-10-29" }, { "path": "record.registrant", "from": null, "to": "Longman Publishers" }, { "path": "record.source", "from": null, "to": "crossref-api" }, { "path": "record.source_agency", "from": null, "to": "Crossref (member 25296)" }, { "path": "record.updated", "from": null, "to": "2026-09-17" }, { "path": "references.0.doi", "from": null, "to": "10.1016/j.compscitech.2010.05.007" }, { "path": "references.0.key", "from": null, "to": "ref1" }, { "path": "references.0.unstructured", "from": null, "to": "Choi I-H, Kim I-G, Ahn S-M, Yeom C-H. 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Composites Science and Technology. 2009;69(7):937-" }, { "path": "references.9.doi", "from": null, "to": "10.1016/j.compscitech.2009.02.009" }, { "path": "references.9.key", "from": null, "to": "ref10" }, { "path": "references.9.unstructured", "from": null, "to": "Lopes C, Seresta O, Coquet Y, Gürdal Z, Camanho P, Thuis B. Low-velocity impact damage on dispersed stacking sequence laminates. Part I: Experiments. Composites Science and Technology. 2009;69(7):926-" }, { "path": "referent", "from": null, "to": "Creation" }, { "path": "structural_type", "from": null, "to": "Digital" }, { "path": "titles.0.lang", "from": null, "to": "en" }, { "path": "titles.0.type", "from": null, "to": "PrincipalTitle" }, { "path": "titles.0.value", "from": null, "to": "Simulation of Quasi-Isotropic E-Glass Composite Laminate at Low\nVelocity Impact with Cohesive Interface Elements" }, { "path": "type", "from": null, "to": "JournalArticle" } ], "record_after": { "format": "smartscholars-doi-metadata/1.0", "doi": "10.46243/jst.2020.v5.i6.pp128-140", "referent": "Creation", "type": "JournalArticle", "structural_type": "Digital", "modes": [ "Visual" ], "characters": [ "Language" ], "titles": [ { "value": "Simulation of Quasi-Isotropic E-Glass Composite Laminate at Low\nVelocity Impact with Cohesive Interface Elements", "type": "PrincipalTitle", "lang": "en" } ], "identifiers": [ { "type": "DOI", "value": "10.46243/jst.2020.v5.i6.pp128-140" } ], "agents": [ { "role": "publisher", "name": { "org": "Longman Publishers" } } ], "dates": { "published": "2020-10-25", "date_type": "PublicationDate", "online": "2020-10-25" }, "language": "en", "container": { "type": "Journal", "titles": [ { "value": "Journal of Science & Technology", "type": "PrincipalTitle" } ], "identifiers": [ { "type": "ISSN", "value": "2456-5660", "medium": "electronic" } ], "issue": "Volume 5", "pages": { "first": "128", "last": "140" } }, "links": [ { "url": "https://www.jst.org.in/index.php/pub/article/view/547", "return_type": "text/html", "primary": true }, { "url": "https://www.jst.org.in/index.php/pub/article/download/547/488", "purpose": "text-mining", "return_type": "application/pdf" }, { "url": "https://www.jst.org.in/index.php/pub/article/download/547/1517", "purpose": "text-mining", "return_type": "application/xml" } ], "abstract": { "value": "This paper examines the expediency of interface elements in modeling of impact damage analysis for Eglass composite laminate under low velocity impact test. Numerical modelsare built adopting cohesive interface behavior to authenticate the cross-ply damage response; and successively used the strategy to model the impact response of quasi-isotropic composite laminate. Impact test are performed to characterize the induced-damage behavior in quasi-isotropic composite laminate at different impact energy test in terms of impact force, displacement and damage size as well as the stress failure trajectory. Numerical result shows reliability of the model for structural impact analysisin damage initiation and progression in laminated composite plates. The simulation result though reveals large deformation, yet, did not yield in total fracture. This development shows the importance of adopting interface elements in structural impact damage criterion to trigger constraints effect on initiation phase.The study also reveals that the bottom most surface suffers huge deformation compare to the impact surface. It divulges that the extent of damage area in each ply of the composite laminate orients in the fiber direction in ‘star-shaped contour. The main novelty is the capability of using this model for structural impact analysis on both cross-ply and quasi-isotropic composite laminate.", "lang": "en" }, "license": { "url": "https://creativecommons.org/licenses/by/4.0", "start": "2020-10-25", "applies_to": "vor" }, "references": [ { "key": "ref1", "doi": "10.1016/j.compscitech.2010.05.007", "unstructured": "Choi I-H, Kim I-G, Ahn S-M, Yeom C-H. Analytical and experimental studies on the low-velocity impact response and damage of composite laminates under in-plane loads with structural damping effects. Composites Science and Technology. 2010;70(10):1513-1522" }, { "key": "ref2", "doi": "10.1016/j.compscitech.2014.04.016", "unstructured": "Xiao S, Chen P, Ye Q. Prediction of damage area in laminated composite plates subjected to low velocity impact. Composites Science and Technology. 2014;98:51-56" }, { "key": "ref3", "doi": "10.1016/s1359-835x(01)00073-2", "unstructured": "Olsson R. Analytical prediction of large mass impact damage in composite laminates. Composites Part A: Applied Science and Manufacturing. 2001;32(9):1207-1215" }, { "key": "ref4", "doi": "10.1016/j.compstruct.2004.07.024", "unstructured": "Hosur MV, Adbullah M, Jeelani S. Studies on the low-velocity impact response of woven hybrid composites. Composite Structures. 2005;67(3):253-262" }, { "key": "ref5", "doi": "10.1016/j.matdes.2013.03.044", "unstructured": "Zhang D, Sun Y, Chen L, Pan N. A comparative study on low-velocity impact response of fabric composite laminates. Materials & Design. 2013;50:750-756" }, { "key": "ref6", "doi": "10.1016/j.matdes.2013.05.016", "unstructured": "Sevkat E, Liaw B, Delale F. Drop-weight impact response of hybrid composites impacted by impactor of various geometries. Materials & Design. 2013;52:67-77" }, { "key": "ref7", "doi": "10.1016/j.ijimpeng.2012.03.002", "unstructured": "Soliman EM, Sheyka MP, Taha MR. Low-velocity impact of thin woven carbon fabric composites incorporating multi-walled carbon nanotubes. International Journal of Impact Engineering. 2012;47:39-47" }, { "key": "ref8", "doi": "10.1016/j.compstruct.2006.06.033", "unstructured": "Mitrevski T, Marshall IH, Thomson RS, Jones R. Low-velocity impacts on preloaded GFRP specimens with various impactor shapes. Composite structures. 2006;76(3):209-217" }, { "key": "ref9", "doi": "10.1016/j.compscitech.2009.02.015", "unstructured": "Lopes C, Camanho P, Gürdal Z, Maimí P, González E. Low-velocity impact damage on dispersed stacking sequence laminates. Part II: Numerical simulations. Composites Science and Technology. 2009;69(7):937-" }, { "key": "ref10", "doi": "10.1016/j.compscitech.2009.02.009", "unstructured": "Lopes C, Seresta O, Coquet Y, Gürdal Z, Camanho P, Thuis B. Low-velocity impact damage on dispersed stacking sequence laminates. Part I: Experiments. Composites Science and Technology. 2009;69(7):926-" }, { "key": "ref11", "doi": "10.1017/s0001924000007685", "unstructured": "Zhang X, Bianchi F, Liu H. Predicting low-velocity impact damage in composites by a quasi-static load model with cohesive interface elements. Aeronautical Journal. 2012;116(1186):1367-1381" }, { "key": "ref12", "doi": "10.1016/j.compstruct.2013.09.004", "unstructured": "Feng D, Aymerich F. Finite element modelling of damage induced by low-velocity impact on composite laminates. Composite Structures. 2014;108:161-171" }, { "key": "ref13", "doi": "10.1007/s13726-018-0633-6", "unstructured": "Ghoushji M, Alebrahim R, Zulkifli R, Sulong A, Abdullah S, Azhari C. Crashworthiness characteristics of natural ramie/bio-epoxy composite tubes for energy absorption application. Iranian Polymer Journal. 2018:1-13" }, { "key": "ref14", "doi": "10.1007/s13726-018-0622-9", "unstructured": "El-baky MAA. Impact performance of hybrid laminated composites with statistical analysis. Iranian Polymer Journal. 2018;27(7):445-459" }, { "key": "ref15", "doi": "10.1007/s13726-017-0590-5", "unstructured": "Zeleniakiene D, Griskevicius P, Norvydas V, Aniskevich A, Zukiene K. Simulation of mechanical behaviour of polychloroprene/versatic acid vinyl ester/methyl methacrylate/2-ethylhexyl acrylate copolymer blend. Iranian Polymer Journal. 2018;27(2):97-103" }, { "key": "ref16", "doi": "10.5755/j02.mech.15966", "unstructured": "Zeleniakienė D, Griškevičius P, Leišis V, Milašienė D. Numerical investigation of impact behaviour of sandwich fiber reinforced plastic composites. Mechanics. 2010;85(5):31-36" }, { "key": "ref17", "doi": "10.1007/s13726-017-0578-1", "unstructured": "Safi S, Zadhoush A, Ahmadi M, Tehrani SPR. 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Applied Composite Materials. 2014;21(1):57-70" }, { "key": "ref21", "doi": "10.1007/s10443-015-9465-0", "unstructured": "Kumar D, Roy R, Kweon J-H, Choi J-h. Numerical Modeling of Combined Matrix Cracking and Delamination in Composite Laminates Using Cohesive Elements. Applied Composite Materials. 2015:1-23" }, { "key": "ref22", "unstructured": "Du J, Tie Y, Li C, Zhou X. Numerical and Experimental Study for Damage Characterization of Composite Laminates Subjected to Low-Velocity Impact.Materials Physics and Mechanics. 2016;27:195-204" }, { "key": "ref23", "doi": "10.1016/j.compstruct.2015.05.037", "unstructured": "Long S, Yao X, Zhang X. Delamination prediction in composite laminates under low-velocity impact. Composite Structures. 2015;132:290-298" }, { "key": "ref24", "doi": "10.1016/j.compstruct.2012.03.039", "unstructured": "Shi Y, Swait T, Soutis C. Modelling damage evolution in composite laminates subjected to low velocity impact. Composite Structures. 2012;94(9):2902-2913" }, { "key": "ref25", "doi": "10.1016/j.paerosci.2015.11.004", "unstructured": "Riccio A, Ricchiuto R, Saputo S, et al. Impact behaviour of omega stiffened composite panels. Progress in Aerospace Sciences. 2016;81:41-48" }, { "key": "ref26", "unstructured": "Version A. 6.11. User’s manual. Dassault Systemes. 2011" }, { "key": "ref27", "unstructured": "Manual AUs. Version 6.11. ABAQUS Inc: Providence, RI, USA. 2011" }, { "key": "ref28", "doi": "10.1016/j.compositesb.2015.04.053", "unstructured": "Wang P, He R, Chen H, Zhu X, Fang D. A novel predictive model for mechanical behavior of single-lap GFRP composite bolted joint under static and dynamic loading. Composites Part B: Engineering. 2015;79:322-330" }, { "key": "ref29", "doi": "10.1016/j.proeng.2016.12.014", "unstructured": "Reddy TS, Reddy PRS, Madhu V. Response of E-glass/Epoxy and Dyneema® Composite Laminates Subjected to low and High Velocity Impact. Procedia Engineering. 2017/01/01 2017;173:278-285" } ], "record": { "registrant": "Longman Publishers", "registered": "2020-10-29", "updated": "2026-09-17", "issue_number": 1, "source": "crossref-api", "source_agency": "Crossref (member 25296)" } }, "url_after": "https://www.jst.org.in/index.php/pub/article/view/547", "sha256_before": null, "sha256_after": "df1d0b397c82a1a076c1381c587923214ebb84182a21178b2230e95b0355bac2" }, { "seq": 2, "kind": "update", "at": "2026-09-29 23:59:41", "by": "Administrator (admin)", "by_kind": "user", "note": "record re-read from api.crossref.org", "changes": [ { "path": "container.titles.0.value", "from": "Journal of Science & Technology", "to": "Journal of Science & Technology" }, { "path": "titles.0.value", "from": "Simulation of Quasi-Isotropic E-Glass Composite Laminate at Low\nVelocity Impact with Cohesive Interface Elements", "to": "Simulation of Quasi-Isotropic E-Glass Composite Laminate at Low Velocity Impact with Cohesive Interface Elements" } ], "record_after": { "format": "smartscholars-doi-metadata/1.0", "doi": "10.46243/jst.2020.v5.i6.pp128-140", "referent": "Creation", "type": "JournalArticle", "structural_type": "Digital", "modes": [ "Visual" ], "characters": [ "Language" ], "titles": [ { "value": "Simulation of Quasi-Isotropic E-Glass Composite Laminate at Low Velocity Impact with Cohesive Interface Elements", "type": "PrincipalTitle", "lang": "en" } ], "identifiers": [ { "type": "DOI", "value": "10.46243/jst.2020.v5.i6.pp128-140" } ], "agents": [ { "role": "publisher", "name": { "org": "Longman Publishers" } } ], "dates": { "published": "2020-10-25", "date_type": "PublicationDate", "online": "2020-10-25" }, "language": "en", "container": { "type": "Journal", "titles": [ { "value": "Journal of Science & Technology", "type": "PrincipalTitle" } ], "identifiers": [ { "type": "ISSN", "value": "2456-5660", "medium": "electronic" } ], "issue": "Volume 5", "pages": { "first": "128", "last": "140" } }, "links": [ { "url": "https://www.jst.org.in/index.php/pub/article/view/547", "return_type": "text/html", "primary": true }, { "url": "https://www.jst.org.in/index.php/pub/article/download/547/488", "purpose": "text-mining", "return_type": "application/pdf" }, { "url": "https://www.jst.org.in/index.php/pub/article/download/547/1517", "purpose": "text-mining", "return_type": "application/xml" } ], "abstract": { "value": "This paper examines the expediency of interface elements in modeling of impact damage analysis for Eglass composite laminate under low velocity impact test. Numerical modelsare built adopting cohesive interface behavior to authenticate the cross-ply damage response; and successively used the strategy to model the impact response of quasi-isotropic composite laminate. Impact test are performed to characterize the induced-damage behavior in quasi-isotropic composite laminate at different impact energy test in terms of impact force, displacement and damage size as well as the stress failure trajectory. Numerical result shows reliability of the model for structural impact analysisin damage initiation and progression in laminated composite plates. The simulation result though reveals large deformation, yet, did not yield in total fracture. This development shows the importance of adopting interface elements in structural impact damage criterion to trigger constraints effect on initiation phase.The study also reveals that the bottom most surface suffers huge deformation compare to the impact surface. It divulges that the extent of damage area in each ply of the composite laminate orients in the fiber direction in ‘star-shaped contour. The main novelty is the capability of using this model for structural impact analysis on both cross-ply and quasi-isotropic composite laminate.", "lang": "en" }, "license": { "url": "https://creativecommons.org/licenses/by/4.0", "start": "2020-10-25", "applies_to": "vor" }, "references": [ { "key": "ref1", "doi": "10.1016/j.compscitech.2010.05.007", "unstructured": "Choi I-H, Kim I-G, Ahn S-M, Yeom C-H. Analytical and experimental studies on the low-velocity impact response and damage of composite laminates under in-plane loads with structural damping effects. Composites Science and Technology. 2010;70(10):1513-1522" }, { "key": "ref2", "doi": "10.1016/j.compscitech.2014.04.016", "unstructured": "Xiao S, Chen P, Ye Q. Prediction of damage area in laminated composite plates subjected to low velocity impact. 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Applied Composite Materials. 2014;21(1):57-70" }, { "key": "ref21", "doi": "10.1007/s10443-015-9465-0", "unstructured": "Kumar D, Roy R, Kweon J-H, Choi J-h. Numerical Modeling of Combined Matrix Cracking and Delamination in Composite Laminates Using Cohesive Elements. Applied Composite Materials. 2015:1-23" }, { "key": "ref22", "unstructured": "Du J, Tie Y, Li C, Zhou X. Numerical and Experimental Study for Damage Characterization of Composite Laminates Subjected to Low-Velocity Impact.Materials Physics and Mechanics. 2016;27:195-204" }, { "key": "ref23", "doi": "10.1016/j.compstruct.2015.05.037", "unstructured": "Long S, Yao X, Zhang X. Delamination prediction in composite laminates under low-velocity impact. Composite Structures. 2015;132:290-298" }, { "key": "ref24", "doi": "10.1016/j.compstruct.2012.03.039", "unstructured": "Shi Y, Swait T, Soutis C. Modelling damage evolution in composite laminates subjected to low velocity impact. Composite Structures. 2012;94(9):2902-2913" }, { "key": "ref25", "doi": "10.1016/j.paerosci.2015.11.004", "unstructured": "Riccio A, Ricchiuto R, Saputo S, et al. Impact behaviour of omega stiffened composite panels. Progress in Aerospace Sciences. 2016;81:41-48" }, { "key": "ref26", "unstructured": "Version A. 6.11. User’s manual. Dassault Systemes. 2011" }, { "key": "ref27", "unstructured": "Manual AUs. Version 6.11. ABAQUS Inc: Providence, RI, USA. 2011" }, { "key": "ref28", "doi": "10.1016/j.compositesb.2015.04.053", "unstructured": "Wang P, He R, Chen H, Zhu X, Fang D. A novel predictive model for mechanical behavior of single-lap GFRP composite bolted joint under static and dynamic loading. Composites Part B: Engineering. 2015;79:322-330" }, { "key": "ref29", "doi": "10.1016/j.proeng.2016.12.014", "unstructured": "Reddy TS, Reddy PRS, Madhu V. Response of E-glass/Epoxy and Dyneema® Composite Laminates Subjected to low and High Velocity Impact. Procedia Engineering. 2017/01/01 2017;173:278-285" } ], "record": { "registrant": "Longman Publishers", "registered": "2020-10-29", "updated": "2026-09-17", "issue_number": 1, "source": "crossref-api", "source_agency": "Crossref (member 25296)" } }, "url_after": "https://www.jst.org.in/index.php/pub/article/view/547", "sha256_before": "df1d0b397c82a1a076c1381c587923214ebb84182a21178b2230e95b0355bac2", "sha256_after": "00de8afac3b5f40326686e1fdbf71bd414a8f874b3f2ef3a07a15780cbcf50df" } ] }