About: Hail Impact on Composite Plates – Experiments and Numerical Modelling

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rdf:type	skos:Concept http://linked.opendata.cz/ontology/domain/vavai/Vysledek
Description	Aircraft structures may be subjected to various in-service impact threats, such as tool drops, runaway debris, bird strikes etc. With the increasing use of monolithic composite laminates on aircraft primary structures and large external surfaces (i.e. fuselage panels, wing skins, leading edges etc.) hail impact can also be a major threat that could potentially compromise structural integrity and lead to structural failures. For these reasons hail impact has received increasing interest within the research community as well as the latest aircraft composite structures development programmes. This paper describes the experimental approach for measuring the damage caused to monolithic CFRP and GFRP composite plates subjected to impact by an ice-ball (i.e. simulated hailstone) and the several possibilities for predicting this damage by numerical modelling in Simulia Abaqus finite element software. The experimental part of this work is concerned with the development and calibration of air pressure gun, and Aircraft structures may be subjected to various in-service impact threats, such as tool drops, runaway debris, bird strikes etc. With the increasing use of monolithic composite laminates on aircraft primary structures and large external surfaces (i.e. fuselage panels, wing skins, leading edges etc.) hail impact can also be a major threat that could potentially compromise structural integrity and lead to structural failures. For these reasons hail impact has received increasing interest within the research community as well as the latest aircraft composite structures development programmes. This paper describes the experimental approach for measuring the damage caused to monolithic CFRP and GFRP composite plates subjected to impact by an ice-ball (i.e. simulated hailstone) and the several possibilities for predicting this damage by numerical modelling in Simulia Abaqus finite element software. The experimental part of this work is concerned with the development and calibration of air pressure gun, and (en)
Title	Hail Impact on Composite Plates – Experiments and Numerical Modelling Hail Impact on Composite Plates – Experiments and Numerical Modelling (en)
skos:prefLabel	Hail Impact on Composite Plates – Experiments and Numerical Modelling Hail Impact on Composite Plates – Experiments and Numerical Modelling (en)
skos:notation	RIV/00216305:26210/12:PU100221!RIV14-MSM-26210___
http://linked.open...avai/predkladatel	Fakulta strojního inženýrství
http://linked.open...avai/riv/aktivita	P
http://linked.open...avai/riv/aktivity	P(ED0002/01/01)
http://linked.open...iv/cisloPeriodika	22
http://linked.open...vai/riv/dodaniDat	2014
http://linked.open...aciTvurceVysledku	Matěják, Vladimír
http://linked.open.../riv/druhVysledku	J - Článek v odborném periodiku
http://linked.open...iv/duvernostUdaju	S - Úplné a pravdivé údaje nepodléhající ochraně podle zvláštních právních předpisů
http://linked.open...titaPredkladatele	Vysoké učení technické v Brně / Fakulta strojního inženýrství
http://linked.open...dnocenehoVysledku	138580
http://linked.open...ai/riv/idVysledku	RIV/00216305:26210/12:PU100221
http://linked.open...riv/jazykVysledku	eng - angličtina
http://linked.open.../riv/klicovaSlova	Hail impact, Composite, Aircraft, FEM, Abaqus Explicit (en)
http://linked.open.../riv/klicoveSlovo	Composite Aircraft FEM Abaqus Explicit Hail impact
http://linked.open...odStatuVydavatele	PL - Polská republika
http://linked.open...ontrolniKodProRIV	[FEE8ECBEF69C]
http://linked.open...i/riv/nazevZdroje	RESEARCH BULLETIN
http://linked.open...in/vavai/riv/obor	JU
http://linked.open...ichTvurcuVysledku	1 (xsd:int)
http://linked.open...cetTvurcuVysledku	3 (xsd:int)
http://linked.open...vavai/riv/projekt	NETME Centre (New Technologies for Mechanical Engineering)
http://linked.open...UplatneniVysledku	2012
http://linked.open...v/svazekPeriodika	2012
http://linked.open...iv/tvurceVysledku	Matěják, Vladimír
issn	1425-2104
number of pages	10 (xsd:int)
http://localhost/t...ganizacniJednotka	26210

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