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Statements

Subject Item
n2:RIV%2F00010669%3A_____%2F14%3A%230001724%21RIV15-MSM-00010669
rdf:type
n3:Vysledek skos:Concept
dcterms:description
This report deals with FNG 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 report deals with FNG 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
FNG Impact of Components on Stability, Stiffness Targets for Components FNG Impact of Components on Stability, Stiffness Targets for Components
skos:prefLabel
FNG Impact of Components on Stability, Stiffness Targets for Components FNG Impact of Components on Stability, Stiffness Targets for Components
skos:notation
RIV/00010669:_____/14:#0001724!RIV15-MSM-00010669
n5:aktivita
n15:P
n5:aktivity
P(7E09012)
n5:dodaniDat
n11:2015
n5:domaciTvurceVysledku
n16:1541765 n16:7615159
n5:druhVysledku
n7:O
n5:duvernostUdaju
n12:S
n5:entitaPredkladatele
n9:predkladatel
n5:idSjednocenehoVysledku
17129
n5:idVysledku
RIV/00010669:_____/14:#0001724
n5:jazykVysledku
n6:eng
n5:klicovaSlova
aeroelasticity; flutter; eigenvalue; sensitivity
n5:klicoveSlovo
n8:flutter n8:sensitivity n8:eigenvalue n8:aeroelasticity
n5:kontrolniKodProRIV
[7420F251E456]
n5:obor
n13:JU
n5:pocetDomacichTvurcuVysledku
2
n5:pocetTvurcuVysledku
2
n5:projekt
n14:7E09012
n5:rokUplatneniVysledku
n11:2014
n5:tvurceVysledku
Čečrdle, Jiří Vích, Ondřej