Conceptual Design of Aeroelastic Demonstrator for Whirl Flutter Simulation

Kód výsledku v IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00010669%3A_____%2F12%3A%230001517" target="_blank" >RIV/00010669:_____/12:#0001517 - isvavai.cz</a>

Výsledek na webu

<a href="http://www.waset.org/journals/waset/v68.php" target="_blank" >http://www.waset.org/journals/waset/v68.php</a>

DOI - Digital Object Identifier

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Jazyk výsledku

angličtina

Název v původním jazyce

Conceptual Design of Aeroelastic Demonstrator for Whirl Flutter Simulation

Popis výsledku v původním jazyce

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 twinturboprop 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 windtunnel. The results will be utilized for validation of analytical methods and software tools.

Název v anglickém jazyce

Conceptual Design of Aeroelastic Demonstrator for Whirl Flutter Simulation

Popis výsledku anglicky

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 twinturboprop 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 windtunnel. The results will be utilized for validation of analytical methods and software tools.

Druh

J_x - Nezařazeno - Článek v odborném periodiku (Jimp, Jsc a Jost)

CEP obor

JU - Aeronautika, aerodynamika, letadla

OECD FORD obor

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Projekt

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Návaznosti

I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace

Rok uplatnění

2012

Kód důvěrnosti údajů

S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Název periodika

World Academy of Science, Engineering and Technology

ISSN

2010-3778

e-ISSN

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Svazek periodika

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Číslo periodika v rámci svazku

68

Stát vydavatele periodika

FR - Francouzská republika

Počet stran výsledku

5

Strana od-do

132-136

Kód UT WoS článku

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EID výsledku v databázi Scopus

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