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Statements

Subject Item
n2:RIV%2F00216305%3A26210%2F14%3APU111370%21RIV15-MSM-26210___
rdf:type
n6:Vysledek skos:Concept
dcterms:description
The motivation for this work is a desire for deep understanding of the structural failures in a composite glider wing, which has been tested in the laboratories of the Institute of Aerospace Engineering, Faculty of Mechanical Engineering, University of Technology in Brno. To understand the causes of the encountered failures, one has to consider the effects of all the stages in design, manufacturing and testing of the wing. This paper focuses on the design stage only. Presented facts are obtained from finite element analysis. The geometry used for the analysis is that of tested specimens. This allows validating the results by comparison of deformation and strains measured during the laboratory tests. Analysis starts with simple I-beam loaded by three-point-bending. In the next step a cantilever is added. Several more modifications follow, changing the I-beam to the wing. Case evaluation considers the interaction between normal (material direction 1) and inter-laminar shear stresses in the upper flange. The motivation for this work is a desire for deep understanding of the structural failures in a composite glider wing, which has been tested in the laboratories of the Institute of Aerospace Engineering, Faculty of Mechanical Engineering, University of Technology in Brno. To understand the causes of the encountered failures, one has to consider the effects of all the stages in design, manufacturing and testing of the wing. This paper focuses on the design stage only. Presented facts are obtained from finite element analysis. The geometry used for the analysis is that of tested specimens. This allows validating the results by comparison of deformation and strains measured during the laboratory tests. Analysis starts with simple I-beam loaded by three-point-bending. In the next step a cantilever is added. Several more modifications follow, changing the I-beam to the wing. Case evaluation considers the interaction between normal (material direction 1) and inter-laminar shear stresses in the upper flange.
dcterms:title
MODIFICATIONS OF A SIMPLE I-BEAM AND ITS EFFECTS ON THE STRESS STATE MODIFICATIONS OF A SIMPLE I-BEAM AND ITS EFFECTS ON THE STRESS STATE
skos:prefLabel
MODIFICATIONS OF A SIMPLE I-BEAM AND ITS EFFECTS ON THE STRESS STATE MODIFICATIONS OF A SIMPLE I-BEAM AND ITS EFFECTS ON THE STRESS STATE
skos:notation
RIV/00216305:26210/14:PU111370!RIV15-MSM-26210___
n3:aktivita
n16:P
n3:aktivity
P(ED0002/01/01)
n3:dodaniDat
n4:2015
n3:domaciTvurceVysledku
n12:8587698 n12:2891131
n3:druhVysledku
n11:D
n3:duvernostUdaju
n19:S
n3:entitaPredkladatele
n18:predkladatel
n3:idSjednocenehoVysledku
30130
n3:idVysledku
RIV/00216305:26210/14:PU111370
n3:jazykVysledku
n10:eng
n3:klicovaSlova
beam, normal stress, shear stress, classical laminate theory, wing, composite
n3:klicoveSlovo
n9:classical%20laminate%20theory n9:wing n9:beam n9:shear%20stress n9:normal%20stress n9:composite
n3:kontrolniKodProRIV
[B79F1D747339]
n3:mistoKonaniAkce
Hradec Králové
n3:mistoVydani
Hradec Králové, Česká republika
n3:nazevZdroje
Sborník příspěvků Mezinárodní Masarykovy konference pro doktorandy a mladé vědecké pracovníky 2014
n3:obor
n7:JU
n3:pocetDomacichTvurcuVysledku
2
n3:pocetTvurcuVysledku
2
n3:projekt
n17:ED0002%2F01%2F01
n3:rokUplatneniVysledku
n4:2014
n3:tvurceVysledku
Cejpek, Jakub Juračka, Jaroslav
n3:typAkce
n5:WRD
n3:zahajeniAkce
2014-12-15+01:00
s:numberOfPages
5
n15:hasPublisher
MAGNANIMITAS
n21:isbn
978-80-87952-07-8
n14:organizacniJednotka
26210