A wind tunnel analysis of flutter vibrations of a U-beam
Identifikátory výsledku
Kód výsledku v IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68378297%3A_____%2F14%3A00429315" target="_blank" >RIV/68378297:_____/14:00429315 - isvavai.cz</a>
Výsledek na webu
<a href="http://paginas.fe.up.pt/eurodyn2014/CD/papers/435_MS20_ABS_1318.pdf" target="_blank" >http://paginas.fe.up.pt/eurodyn2014/CD/papers/435_MS20_ABS_1318.pdf</a>
DOI - Digital Object Identifier
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Alternativní jazyky
Jazyk výsledku
angličtina
Název v původním jazyce
A wind tunnel analysis of flutter vibrations of a U-beam
Popis výsledku v původním jazyce
Motivated by assessing the aeroelastic stability of a conveyor solution, the aeroelastic stability of a U-beam with an aspect ratio (width B over frontal height H) of B/H = 4.62 is investigated. Wind-tunnel experiments involving a special test stand forsectional models and complementary CFD simulations were carried out. We find that the U-beam can perform self-excited two-degree of freedom (flutter) vibrations. This is also reflected in the simulation results. Vortex-induced vibrations were observed experimentally, but the amplitudes were small in respect to the frontal height. Numerically, it was found that there exist two different patterns of the flow around the U-profile: One pattern that is very similar to the flow around a rectangular prism ( ?R-flow pattern) and another pattern were the flow ?reaches into the pocket of the profile (?U-flow pattern). The amplitude of vortex induced vibrations depends strongly on the flow pattern. When the R-flow pattern is realized, the amplitud
Název v anglickém jazyce
A wind tunnel analysis of flutter vibrations of a U-beam
Popis výsledku anglicky
Motivated by assessing the aeroelastic stability of a conveyor solution, the aeroelastic stability of a U-beam with an aspect ratio (width B over frontal height H) of B/H = 4.62 is investigated. Wind-tunnel experiments involving a special test stand forsectional models and complementary CFD simulations were carried out. We find that the U-beam can perform self-excited two-degree of freedom (flutter) vibrations. This is also reflected in the simulation results. Vortex-induced vibrations were observed experimentally, but the amplitudes were small in respect to the frontal height. Numerically, it was found that there exist two different patterns of the flow around the U-profile: One pattern that is very similar to the flow around a rectangular prism ( ?R-flow pattern) and another pattern were the flow ?reaches into the pocket of the profile (?U-flow pattern). The amplitude of vortex induced vibrations depends strongly on the flow pattern. When the R-flow pattern is realized, the amplitud
Klasifikace
Druh
D - Stať ve sborníku
CEP obor
JM - Inženýrské stavitelství
OECD FORD obor
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Návaznosti výsledku
Projekt
Výsledek vznikl pri realizaci vícero projektů. Více informací v záložce Projekty.
Návaznosti
I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace
Ostatní
Rok uplatnění
2014
Kód důvěrnosti údajů
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Údaje specifické pro druh výsledku
Název statě ve sborníku
Proceedings of the 9th International Conference on Structural Dynamics. EURODYN 2014
ISBN
978-972-752-165-4
ISSN
2311-9020
e-ISSN
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Počet stran výsledku
8
Strana od-do
3113-3120
Název nakladatele
European Association for Structural Dynamics (EASD)
Místo vydání
Porto
Místo konání akce
Porto
Datum konání akce
30. 6. 2014
Typ akce podle státní příslušnosti
WRD - Celosvětová akce
Kód UT WoS článku
000354786604020