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Statements

Subject Item
n2:RIV%2F00010669%3A_____%2F09%3A%230000929%21RIV10-MSM-00010669
rdf:type
n6:Vysledek skos:Concept
dcterms:description
This article discusses simulationof the impact behaviour of a rigid projectile immediately after the impact on an aluminium plate. The result was verified on the real aircraft structure damage. 3D digitizing system was used for comparison between FE calculation and real structure damage. This article discusses simulationof the impact behaviour of a rigid projectile immediately after the impact on an aluminium plate. The result was verified on the real aircraft structure damage. 3D digitizing system was used for comparison between FE calculation and real structure damage.
dcterms:title
SIMULATION OF RIGID PROJECTILE IMPACT ON THE REAL AIRCRAFT STRUCTURE SIMULATION OF RIGID PROJECTILE IMPACT ON THE REAL AIRCRAFT STRUCTURE
skos:prefLabel
SIMULATION OF RIGID PROJECTILE IMPACT ON THE REAL AIRCRAFT STRUCTURE SIMULATION OF RIGID PROJECTILE IMPACT ON THE REAL AIRCRAFT STRUCTURE
skos:notation
RIV/00010669:_____/09:#0000929!RIV10-MSM-00010669
n4:aktivita
n5:Z
n4:aktivity
Z(MSM0001066903)
n4:cisloPeriodika
2
n4:dodaniDat
n12:2010
n4:domaciTvurceVysledku
n14:4780272
n4:druhVysledku
n17:J
n4:duvernostUdaju
n16:S
n4:entitaPredkladatele
n15:predkladatel
n4:idSjednocenehoVysledku
341337
n4:idVysledku
RIV/00010669:_____/09:#0000929
n4:jazykVysledku
n11:eng
n4:klicovaSlova
projectile; finite element method
n4:klicoveSlovo
n10:finite%20element%20method n10:projectile
n4:kodStatuVydavatele
CZ - Česká republika
n4:kontrolniKodProRIV
[7F787C59F8C7]
n4:nazevZdroje
Czech Aerospace Proceedings / Letecký zpravodaj
n4:obor
n9:JY
n4:pocetDomacichTvurcuVysledku
1
n4:pocetTvurcuVysledku
1
n4:rokUplatneniVysledku
n12:2009
n4:svazekPeriodika
2/2009
n4:tvurceVysledku
Doubrava, Radek
n4:zamer
n13:MSM0001066903
s:issn
1211-877X
s:numberOfPages
4