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Statements

Subject Item
n2:RIV%2F00010669%3A_____%2F13%3A%230001551%21RIV14-MPO-00010669
rdf:type
n13:Vysledek skos:Concept
rdfs:seeAlso
http://pig.sagepub.com/content/227/6.toc
dcterms:description
This paper deals with the aileron flutter of the light sport aircraft. It gives an assessment of the influence of the retrofitting of the tab with regard to the aircraft aileron flutter characteristics. The necessary actuation system stiffness and the aileron flapping frequency to ensure stability at maximal speed of the aircraft are evaluated. The study was motivated by the M-7 aircraft accident in the western Bohemia in 2006. The finite element (FE) model was prepared by the optimization (gradient based methods) utilizing the geometry and the test results to obtain the unknown structural parameters (stiffness, inertia). The design variables were mass and stiffness characteristics, initial values of design variables were set according geometry. The design responses (constrains and objective functions) were formulated in order to match ground vibration tests and other known This paper deals with the aileron flutter of the light sport aircraft. It gives an assessment of the influence of the retrofitting of the tab with regard to the aircraft aileron flutter characteristics. The necessary actuation system stiffness and the aileron flapping frequency to ensure stability at maximal speed of the aircraft are evaluated. The study was motivated by the M-7 aircraft accident in the western Bohemia in 2006. The finite element (FE) model was prepared by the optimization (gradient based methods) utilizing the geometry and the test results to obtain the unknown structural parameters (stiffness, inertia). The design variables were mass and stiffness characteristics, initial values of design variables were set according geometry. The design responses (constrains and objective functions) were formulated in order to match ground vibration tests and other known
dcterms:title
Assessment of Aileron Tab Installation Influence on Light Sport Aircraft Flutter Characteristics Assessment of Aileron Tab Installation Influence on Light Sport Aircraft Flutter Characteristics
skos:prefLabel
Assessment of Aileron Tab Installation Influence on Light Sport Aircraft Flutter Characteristics Assessment of Aileron Tab Installation Influence on Light Sport Aircraft Flutter Characteristics
skos:notation
RIV/00010669:_____/13:#0001551!RIV14-MPO-00010669
n13:predkladatel
n14:ico%3A00010669
n4:aktivita
n16:I
n4:aktivity
I
n4:cisloPeriodika
6
n4:dodaniDat
n5:2014
n4:domaciTvurceVysledku
n15:7615159
n4:druhVysledku
n17:J
n4:duvernostUdaju
n9:S
n4:entitaPredkladatele
n18:predkladatel
n4:idSjednocenehoVysledku
62249
n4:idVysledku
RIV/00010669:_____/13:#0001551
n4:jazykVysledku
n19:eng
n4:klicovaSlova
aeroelasticity; flutter; eigenvalue; sensitivity
n4:klicoveSlovo
n10:eigenvalue n10:aeroelasticity n10:sensitivity n10:flutter
n4:kodStatuVydavatele
GB - Spojené království Velké Británie a Severního Irska
n4:kontrolniKodProRIV
[A84D1747D6C4]
n4:nazevZdroje
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering
n4:obor
n12:JU
n4:pocetDomacichTvurcuVysledku
1
n4:pocetTvurcuVysledku
1
n4:rokUplatneniVysledku
n5:2013
n4:svazekPeriodika
227
n4:tvurceVysledku
Čečrdle, Jiří
s:issn
0954-4100
s:numberOfPages
9
n11:doi
10.1177/0954410012446396