Počet záznamů: 1  

Flutter derivatives of the Kao-Pin Hsi cable-supported bridge

  1. 1.
    0453617 - ÚTAM 2016 RIV CH eng C - Konferenční příspěvek (zahraniční konf.)
    Buljac, A. - Pospíšil, Stanislav - Kozmar, H. - Kuznetsov, Sergeii - Král, Radomil
    Flutter derivatives of the Kao-Pin Hsi cable-supported bridge.
    Applied Mechanics and Materials. Vol. 821. Zürich: Trans Tech Publications Inc, 2016 - (Fischer, C.), s. 172-179. Engineering Mechanics, 821. ISBN 978-3-03835-700-1. ISSN 1660-9336.
    [Engineering mechanics 2015 /21./. Svratka (CZ), 11.05.2015-14.05.2015]
    Grant CEP: GA ČR(CZ) GA15-01035S; GA MŠMT(CZ) LO1219
    Institucionální podpora: RVO:68378297
    Klíčová slova: bridge-deck section * vibrations * aeroelasticity * flutter derivatives * wind-tunnel experiments
    Kód oboru RIV: JM - Inženýrské stavitelství

    Long-span cable-supported bridges, characterized with low natural frequencies and
    mechanical damping, are very sensitive to wind effects. Therefore, investigation of the aeroelastic
    behaviour of bridges is particularly important when designing these complex engineering structures.
    The focus is on evaluation of dimensionless aeroelastic coefficients, i.e. flutter derivatives, which
    are considered as indicators of the aeroelastic stability of bridges. A comprehensive experimental
    study on dynamic wind-induced behaviour of the Kao-Pin Hsi Bridge in Taiwan is carried out in the
    Climatic Wind Tunnel of the Centre of Excellence Telč (CET), Czech Republic. The bridge-deck
    section is tested at a multipurpose experimental setup originally developed in the CET. Flutter
    derivatives are obtained by the means of the free-vibration technique for the double-degree-offreedom
    (DDOF) system. The results are compared to those of a thin flat plate with large width to
    height ratio, which previously proved to be stable with respect to the flutter phenomenon. While the
    torsional instability is observed for the Kao-Pin Hsi bridge-deck section, the flat plate proves to be
    aeroelastically stable.
    Trvalý link: http://hdl.handle.net/11104/0254379

     
     
Počet záznamů: 1  

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