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dc.contributor.authorGrasso, Marzio
dc.contributor.authorPenta, Francesco
dc.contributor.authorPucillo, Giovanni Pio
dc.contributor.authorRicci, Fabrizio
dc.contributor.authorRosiello, Vincenzo
dc.contributor.editorAo, S.I.
dc.contributor.editorGelman, Len
dc.contributor.editorHukins, David W.L.
dc.contributor.editorHunter, Andrew
dc.contributor.editorKorsunsky, A.M.
dc.date.accessioned2016-04-04T11:47:27Z
dc.date.available2016-04-04T11:47:27Z
dc.date.issued2015
dc.identifier.citationGrasso , M , Penta , F , Pucillo , G P , Ricci , F & Rosiello , V 2015 , Low Velocity Impact Response of Composite Panels for Aeronautical Applications . in S I Ao , L Gelman , D W L Hukins , A Hunter & A M Korsunsky (eds) , Proceedings of The World Congress on Engineering 2015 . vol. 2 , Newswood Limited , pp. 1138-1143 , World Congress on Engineering 2015 , London , United Kingdom , 1/07/15 . < http://www.iaeng.org/publication/WCE2015/WCE2015_pp1138-1143.pdf >
dc.identifier.citationconference
dc.identifier.isbn978-988-14047-0-1
dc.identifier.otherPURE: 9874601
dc.identifier.otherPURE UUID: 5eab34ac-70b2-4ad5-9978-ebb419049ff8
dc.identifier.otherScopus: 84991250767
dc.identifier.urihttp://hdl.handle.net/2299/16922
dc.description.abstractThe present experimental work analyses the impact behaviour of thermosetting composite materials for aeronautic applications. The main goal of the experimental activity was to identify the energy level in correspondence of which penetration occurs. The initial values of the impact energy were estimated according to analytical correlations found in literature. Tests were performed on three types of composite panels: carbon fibre laminated panels, fibreglass laminated panels and hybrid panels. The technology of lamina is that of prepeg fabric with twill sequence and fibres weaving at 0°-90° and ± 45°. The fixture used for tests is a Charpy impact test machine, which was conveniently equipped to evaluate the angular variation and the acceleration of the impacting mass. Preliminarily, non-destructive ultrasonic controls were performed to check that the specimens were not damaged before impacts tests. The interesting results of the tests were identification of the energy absorbed and the impact force for each specimen. Moreover, for each energy and force level, it was possible to associate a different fracture state. Comparisons among the results obtained for specimens made up of just one type of reinforcement (glass or carbon) and the results obtained with hybrid specimens were performed.en
dc.format.extent6
dc.language.isoeng
dc.publisherNewswood Limited
dc.relation.ispartofProceedings of The World Congress on Engineering 2015
dc.titleLow Velocity Impact Response of Composite Panels for Aeronautical Applicationsen
dc.contributor.institutionSchool of Engineering and Technology
dc.identifier.urlhttp://www.iaeng.org/publication/WCE2015/WCE2015_pp1138-1143.pdf
rioxxterms.typeOther
herts.preservation.rarelyaccessedtrue


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