Aeroelastická analýza a experiment polokřídla velkého dopravního letounu

Kód výsledku v IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00010669%3A_____%2F07%3A%230000635" target="_blank" >RIV/00010669:_____/07:#0000635 - isvavai.cz</a>

Výsledek na webu

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DOI - Digital Object Identifier

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Jazyk výsledku

angličtina

Název v původním jazyce

Aeroelastic Analysis and Experiment of an Airliner Half-Wing Model

Popis výsledku v původním jazyce

The paper deals with aeroelastic analysis and experiments of the isolated half?wing of the research wind tunnel model EuRAM (European Research Aeroelastic Model) performed at VZLU in the frame of the projects ?Active Aeroelastic Aircraft Structures? and?Research on Strength of Low-weight Structures with Special Regard to Airplane Structures?. The half-wing model is a part of the complete four jet engine airliner wind tunnel model. The model stiffness and modal characteristics were analytically and experimentally verified. The main interest was focused on the evaluation of the model aeroelastic characteristics, especially flutter, static and dynamic effectiveness of unconventional control surfaces, and aeroelastic response to the dynamic loads. Analytical and experimental results were compared to verify and update the analytical models. The results were also used for efficient planning and organization of the more expensive experiments on the complete aircraft wind tunnel model

Název v anglickém jazyce

Aeroelastic Analysis and Experiment of an Airliner Half-Wing Model

Popis výsledku anglicky

The paper deals with aeroelastic analysis and experiments of the isolated half?wing of the research wind tunnel model EuRAM (European Research Aeroelastic Model) performed at VZLU in the frame of the projects ?Active Aeroelastic Aircraft Structures? and?Research on Strength of Low-weight Structures with Special Regard to Airplane Structures?. The half-wing model is a part of the complete four jet engine airliner wind tunnel model. The model stiffness and modal characteristics were analytically and experimentally verified. The main interest was focused on the evaluation of the model aeroelastic characteristics, especially flutter, static and dynamic effectiveness of unconventional control surfaces, and aeroelastic response to the dynamic loads. Analytical and experimental results were compared to verify and update the analytical models. The results were also used for efficient planning and organization of the more expensive experiments on the complete aircraft wind tunnel model

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

Z - Vyzkumny zamer (s odkazem do CEZ)<br>R - Projekt Ramcoveho programu EK

Rok uplatnění

2007

Kód důvěrnosti údajů

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

Název periodika

Czech Aerospace Proceedings / Letecký zpravodaj

ISSN

1211-877X

e-ISSN

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Svazek periodika

1-2007

Číslo periodika v rámci svazku

březen

Stát vydavatele periodika

CZ - Česká republika

Počet stran výsledku

9

Strana od-do

22-30

Kód UT WoS článku

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EID výsledku v databázi Scopus

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