This HTML5 document contains 40 embedded RDF statements represented using HTML+Microdata notation.

The embedded RDF content will be recognized by any processor of HTML5 Microdata.

Namespace Prefixes

PrefixIRI
n13http://linked.opendata.cz/resource/domain/vavai/vysledek/RIV%2F00216305%3A26210%2F12%3APU100221%21RIV14-MSM-26210___/
dctermshttp://purl.org/dc/terms/
n14http://localhost/temp/predkladatel/
n16http://linked.opendata.cz/resource/domain/vavai/projekt/
n5http://linked.opendata.cz/resource/domain/vavai/riv/tvurce/
n18http://linked.opendata.cz/resource/domain/vavai/subjekt/
n3http://linked.opendata.cz/ontology/domain/vavai/
shttp://schema.org/
skoshttp://www.w3.org/2004/02/skos/core#
n4http://linked.opendata.cz/ontology/domain/vavai/riv/
n2http://linked.opendata.cz/resource/domain/vavai/vysledek/
rdfhttp://www.w3.org/1999/02/22-rdf-syntax-ns#
n10http://linked.opendata.cz/ontology/domain/vavai/riv/klicoveSlovo/
n15http://linked.opendata.cz/ontology/domain/vavai/riv/duvernostUdaju/
xsdhhttp://www.w3.org/2001/XMLSchema#
n19http://linked.opendata.cz/ontology/domain/vavai/riv/jazykVysledku/
n11http://linked.opendata.cz/ontology/domain/vavai/riv/aktivita/
n7http://linked.opendata.cz/ontology/domain/vavai/riv/obor/
n6http://linked.opendata.cz/ontology/domain/vavai/riv/druhVysledku/
n17http://reference.data.gov.uk/id/gregorian-year/

Statements

Subject Item
n2:RIV%2F00216305%3A26210%2F12%3APU100221%21RIV14-MSM-26210___
rdf:type
n3:Vysledek skos:Concept
dcterms: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
dcterms:title
Hail Impact on Composite Plates – Experiments and Numerical Modelling Hail Impact on Composite Plates – Experiments and Numerical Modelling
skos:prefLabel
Hail Impact on Composite Plates – Experiments and Numerical Modelling Hail Impact on Composite Plates – Experiments and Numerical Modelling
skos:notation
RIV/00216305:26210/12:PU100221!RIV14-MSM-26210___
n3:predkladatel
n18:orjk%3A26210
n4:aktivita
n11:P
n4:aktivity
P(ED0002/01/01)
n4:cisloPeriodika
22
n4:dodaniDat
n17:2014
n4:domaciTvurceVysledku
n5:5613760
n4:druhVysledku
n6:J
n4:duvernostUdaju
n15:S
n4:entitaPredkladatele
n13:predkladatel
n4:idSjednocenehoVysledku
138580
n4:idVysledku
RIV/00216305:26210/12:PU100221
n4:jazykVysledku
n19:eng
n4:klicovaSlova
Hail impact, Composite, Aircraft, FEM, Abaqus Explicit
n4:klicoveSlovo
n10:Abaqus%20Explicit n10:Composite n10:FEM n10:Hail%20impact n10:Aircraft
n4:kodStatuVydavatele
PL - Polská republika
n4:kontrolniKodProRIV
[FEE8ECBEF69C]
n4:nazevZdroje
RESEARCH BULLETIN
n4:obor
n7:JU
n4:pocetDomacichTvurcuVysledku
1
n4:pocetTvurcuVysledku
3
n4:projekt
n16:ED0002%2F01%2F01
n4:rokUplatneniVysledku
n17:2012
n4:svazekPeriodika
2012
n4:tvurceVysledku
Matěják, Vladimír
s:issn
1425-2104
s:numberOfPages
10
n14:organizacniJednotka
26210