About: Conceptual Design of Aeroelastic Demonstrator for Whirl Flutter Simulation

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An Entity of Type : http://linked.opendata.cz/ontology/domain/vavai/Vysledek, within Data Space : linked.opendata.cz associated with source document(s)

Attributes	Values
rdf:type	skos:Concept http://linked.opendata.cz/ontology/domain/vavai/Vysledek
rdfs:seeAlso	http://www.waset.org/journals/waset/v68.php
Description	This paper deals with the conceptual design of the new aeroelastic demonstrator for the whirl flutter simulation. The paper gives a theoretical background of the whirl flutter phenomenon and describes the events of the whirl flutter occurrence in the aerospace practice. The second part is focused on the experimental research of the whirl flutter on aeroelastic similar models. Finally the concept of the new aeroelastic demonstrator is described. The demonstrator represents the wing and engine of the twin turboprop commuter aircraft including a driven propeller. It allows the changes of the main structural parameters influencing the whirl flutter stability characteristics. It is intended for the experimental investigation of the whirl flutter in the wind tunnel. The results will be utilized for validation of analytical methods and software tools. This paper deals with the conceptual design of the new aeroelastic demonstrator for the whirl flutter simulation. The paper gives a theoretical background of the whirl flutter phenomenon and describes the events of the whirl flutter occurrence in the aerospace practice. The second part is focused on the experimental research of the whirl flutter on aeroelastic similar models. Finally the concept of the new aeroelastic demonstrator is described. The demonstrator represents the wing and engine of the twin turboprop commuter aircraft including a driven propeller. It allows the changes of the main structural parameters influencing the whirl flutter stability characteristics. It is intended for the experimental investigation of the whirl flutter in the wind tunnel. The results will be utilized for validation of analytical methods and software tools. (en)
Title	Conceptual Design of Aeroelastic Demonstrator for Whirl Flutter Simulation Conceptual Design of Aeroelastic Demonstrator for Whirl Flutter Simulation (en)
skos:prefLabel	Conceptual Design of Aeroelastic Demonstrator for Whirl Flutter Simulation Conceptual Design of Aeroelastic Demonstrator for Whirl Flutter Simulation (en)
skos:notation	RIV/00010669:_____/12:#0001517!RIV13-MPO-00010669
http://linked.open...avai/predkladatel	Výzkumný a zkušební letecký ústav, a.s.
http://linked.open...avai/riv/aktivita	I
http://linked.open...avai/riv/aktivity	I
http://linked.open...iv/cisloPeriodika	68
http://linked.open...vai/riv/dodaniDat	2013
http://linked.open...aciTvurceVysledku	Maleček, Jaromír Čečrdle, Jiří
http://linked.open.../riv/druhVysledku	J - Článek v odborném periodiku
http://linked.open...iv/duvernostUdaju	S - Úplné a pravdivé údaje nepodléhající ochraně podle zvláštních právních předpisů
http://linked.open...titaPredkladatele	Výzkumný a zkušební letecký ústav, a.s.
http://linked.open...dnocenehoVysledku	128392
http://linked.open...ai/riv/idVysledku	RIV/00010669:_____/12:#0001517
http://linked.open...riv/jazykVysledku	eng - angličtina
http://linked.open.../riv/klicovaSlova	aeroelasticity; flutter; whirl flutter; W WING demonstrator (en)
http://linked.open.../riv/klicoveSlovo	aeroelasticity flutter W WING demonstrator whirl flutter
http://linked.open...odStatuVydavatele	FR - Francouzská republika
http://linked.open...ontrolniKodProRIV	[3432FFD95818]
http://linked.open...i/riv/nazevZdroje	World Academy of Science, Engineering and Technology
http://linked.open...in/vavai/riv/obor	JU
http://linked.open...ichTvurcuVysledku	2 (xsd:int)
http://linked.open...cetTvurcuVysledku	2 (xsd:int)
http://linked.open...UplatneniVysledku	2012
http://linked.open...iv/tvurceVysledku	Maleček, Jaromír Čečrdle, Jiří
issn	2010-3778
number of pages	5 (xsd:int)
is http://linked.open...avai/riv/vysledek of	Conceptual Design of Aeroelastic Demonstrator for Whirl Flutter Simulation

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