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Statements

Subject Item
n2:RIV%2F60162694%3AG43__%2F08%3A00424138%21RIV11-MO0-G43_____
rdf:type
n15:Vysledek skos:Concept
dcterms:description
The aim of the work is to create a FEM model of bonded composite patch. The tension is put on analysing the adhesive shear stress that is crucial for the load capacity of the bonded joint. Included are influencing factors like adhesive fillet, thickness of the patch, the length of damage, symmetry of the joint and a chamfer of damaged plate. The goals of the work help to battle aircraft repairing in the field conditions. The aim of the work is to create a FEM model of bonded composite patch. The tension is put on analysing the adhesive shear stress that is crucial for the load capacity of the bonded joint. Included are influencing factors like adhesive fillet, thickness of the patch, the length of damage, symmetry of the joint and a chamfer of damaged plate. The goals of the work help to battle aircraft repairing in the field conditions.
dcterms:title
Analysis of Bonded Composite Patch Using FEM Analysis of Bonded Composite Patch Using FEM
skos:prefLabel
Analysis of Bonded Composite Patch Using FEM Analysis of Bonded Composite Patch Using FEM
skos:notation
RIV/60162694:G43__/08:00424138!RIV11-MO0-G43_____
n4:aktivita
n17:S
n4:aktivity
S
n4:cisloPeriodika
16
n4:dodaniDat
n6:2011
n4:domaciTvurceVysledku
n16:3956326
n4:druhVysledku
n5:J
n4:duvernostUdaju
n12:S
n4:entitaPredkladatele
n8:predkladatel
n4:idSjednocenehoVysledku
355777
n4:idVysledku
RIV/60162694:G43__/08:00424138
n4:jazykVysledku
n14:eng
n4:klicovaSlova
FEM; composite patch; shear stress; bonding
n4:klicoveSlovo
n9:shear%20stress n9:bonding n9:composite%20patch n9:FEM
n4:kodStatuVydavatele
CZ - Česká republika
n4:kontrolniKodProRIV
[14EDE5991E6F]
n4:nazevZdroje
Acta Avionica
n4:obor
n7:KA
n4:pocetDomacichTvurcuVysledku
1
n4:pocetTvurcuVysledku
1
n4:rokUplatneniVysledku
n6:2008
n4:svazekPeriodika
10
n4:tvurceVysledku
Hub, Juraj
s:issn
1335-9479
s:numberOfPages
4
n13:organizacniJednotka
G43