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Statements

Subject Item
n2:RIV%2F00010669%3A_____%2F13%3A%230001723%21RIV15-MSM-00010669
rdf:type
skos:Concept n17:Vysledek
rdfs:seeAlso
http://www.vzlu.cz/cz/transfer-vysledku/clanky-ve-sbornicich-d/
dcterms:description
This paper describes the airliner wing flutter sensitivity analysis. The sensitivity coefficients defines the influence of the structural parameters changes to the structure eigenvalue and flutter stability characteristics. Evaluated structural parameters represent the possible changes of the structure due to the installation of the smart high-lift devices at the leading and trailing edge region. In general, we can suppose the increasing of the mass and mass moment of inertia around the elastic axis and decreasing of the stiffness. Described effects are ordinarily considered destabilizing regarding the flutter. The main aim of the presented work is to evaluate the impact of components to the stability and to define the most critical regions or parameters. This paper describes the airliner wing flutter sensitivity analysis. The sensitivity coefficients defines the influence of the structural parameters changes to the structure eigenvalue and flutter stability characteristics. Evaluated structural parameters represent the possible changes of the structure due to the installation of the smart high-lift devices at the leading and trailing edge region. In general, we can suppose the increasing of the mass and mass moment of inertia around the elastic axis and decreasing of the stiffness. Described effects are ordinarily considered destabilizing regarding the flutter. The main aim of the presented work is to evaluate the impact of components to the stability and to define the most critical regions or parameters.
dcterms:title
Eigenvalue and Flutter Sensitivity Analysis of Airliner Wing Eigenvalue and Flutter Sensitivity Analysis of Airliner Wing
skos:prefLabel
Eigenvalue and Flutter Sensitivity Analysis of Airliner Wing Eigenvalue and Flutter Sensitivity Analysis of Airliner Wing
skos:notation
RIV/00010669:_____/13:#0001723!RIV15-MSM-00010669
n5:aktivita
n16:P
n5:aktivity
P(7E09012)
n5:dodaniDat
n12:2015
n5:domaciTvurceVysledku
n13:1541765 n13:7615159
n5:druhVysledku
n19:D
n5:duvernostUdaju
n14:S
n5:entitaPredkladatele
n11:predkladatel
n5:idSjednocenehoVysledku
72118
n5:idVysledku
RIV/00010669:_____/13:#0001723
n5:jazykVysledku
n18:eng
n5:klicovaSlova
aeroelasticity; flutter; eigenvalue; sensitivity
n5:klicoveSlovo
n9:aeroelasticity n9:sensitivity n9:flutter n9:eigenvalue
n5:kontrolniKodProRIV
[215FA07DA6DA]
n5:mistoKonaniAkce
Svratka, ČR
n5:mistoVydani
ČR
n5:nazevZdroje
: Engineering Mechanics 2013, 19th International Conference
n5:obor
n21:JU
n5:pocetDomacichTvurcuVysledku
2
n5:pocetTvurcuVysledku
2
n5:projekt
n20:7E09012
n5:rokUplatneniVysledku
n12:2013
n5:tvurceVysledku
Vích, Ondřej Čečrdle, Jiří
n5:typAkce
n8:EUR
n5:zahajeniAkce
2013-01-01+01:00
s:numberOfPages
12
n6:hasPublisher
Czech Society for Mechanics
n10:isbn
9788087012475