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    Vortex Induced Vibration and Frequency Lock In of an Airfoil at High Angles of Attack

    Source: Journal of Fluids Engineering:;2016:;volume( 138 ):;issue: 001::page 11204
    Author:
    Besem, Fanny M.
    ,
    Kamrass, Joshua D.
    ,
    Thomas, Jeffrey P.
    ,
    Tang, Deman
    ,
    Kielb, Robert E.
    DOI: 10.1115/1.4031134
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Vortexinduced vibration is a fluid instability where vortices due to secondary flows exert a periodic unsteady force on the elastic structure. Under certain circumstances, the shedding frequency can lock into the structure natural frequency and lead to limit cycle oscillations. These vibrations may cause material fatigue and are a common source of structural failure. This work uses a frequency domain, harmonic balance (HB) computational fluid dynamics (CFD) code to predict the natural shedding frequency and lockin region of an airfoil at very high angles of attack. The numerical results are then successfully compared to experimental data from wind tunnel testings.
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      Vortex Induced Vibration and Frequency Lock In of an Airfoil at High Angles of Attack

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    http://yetl.yabesh.ir/yetl1/handle/yetl/161303
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    contributor authorBesem, Fanny M.
    contributor authorKamrass, Joshua D.
    contributor authorThomas, Jeffrey P.
    contributor authorTang, Deman
    contributor authorKielb, Robert E.
    date accessioned2017-05-09T01:29:16Z
    date available2017-05-09T01:29:16Z
    date issued2016
    identifier issn0098-2202
    identifier otherfe_138_01_011204.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/161303
    description abstractVortexinduced vibration is a fluid instability where vortices due to secondary flows exert a periodic unsteady force on the elastic structure. Under certain circumstances, the shedding frequency can lock into the structure natural frequency and lead to limit cycle oscillations. These vibrations may cause material fatigue and are a common source of structural failure. This work uses a frequency domain, harmonic balance (HB) computational fluid dynamics (CFD) code to predict the natural shedding frequency and lockin region of an airfoil at very high angles of attack. The numerical results are then successfully compared to experimental data from wind tunnel testings.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleVortex Induced Vibration and Frequency Lock In of an Airfoil at High Angles of Attack
    typeJournal Paper
    journal volume138
    journal issue1
    journal titleJournal of Fluids Engineering
    identifier doi10.1115/1.4031134
    journal fristpage11204
    journal lastpage11204
    identifier eissn1528-901X
    treeJournal of Fluids Engineering:;2016:;volume( 138 ):;issue: 001
    contenttypeFulltext
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