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    On the Dynamics of Flexible Beams Under Large Overall Motions—The Plane Case: Part I

    Source: Journal of Applied Mechanics:;1986:;volume( 053 ):;issue: 004::page 849
    Author:
    J. C. Simo
    ,
    L. Vu-Quoc
    DOI: 10.1115/1.3171870
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The dynamic response of a flexible beam subject to large overall motions is traditionally formulated relative to a floating frame, sometimes referred to as the shadow beam . This type of formulation leads to equations of motion of the form g̃(ẏ, y, t) = 0 , that are implicit, nonlinear and highly coupled in the inertia terms. An alternative approach is proposed whereby all quantities are referred to the inertial frame. As a result, the inertia term enters linearly in the formulation simply as mass times acceleration. Crucial to this formulation is the use of finite strain rod theories capable of treating finite rotations. Numerical examples that involve finite vibrations coupled with large overall motions are presented in Part II of this paper.
    keyword(s): Dynamics (Mechanics) , Motion , Structural frames , Inertia (Mechanics) , Equations of motion , Shades and shadows , Vibration AND Dynamic response ,
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      On the Dynamics of Flexible Beams Under Large Overall Motions—The Plane Case: Part I

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    http://yetl.yabesh.ir/yetl1/handle/yetl/100681
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    contributor authorJ. C. Simo
    contributor authorL. Vu-Quoc
    date accessioned2017-05-08T23:21:42Z
    date available2017-05-08T23:21:42Z
    date copyrightDecember, 1986
    date issued1986
    identifier issn0021-8936
    identifier otherJAMCAV-26274#849_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/100681
    description abstractThe dynamic response of a flexible beam subject to large overall motions is traditionally formulated relative to a floating frame, sometimes referred to as the shadow beam . This type of formulation leads to equations of motion of the form g̃(ẏ, y, t) = 0 , that are implicit, nonlinear and highly coupled in the inertia terms. An alternative approach is proposed whereby all quantities are referred to the inertial frame. As a result, the inertia term enters linearly in the formulation simply as mass times acceleration. Crucial to this formulation is the use of finite strain rod theories capable of treating finite rotations. Numerical examples that involve finite vibrations coupled with large overall motions are presented in Part II of this paper.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleOn the Dynamics of Flexible Beams Under Large Overall Motions—The Plane Case: Part I
    typeJournal Paper
    journal volume53
    journal issue4
    journal titleJournal of Applied Mechanics
    identifier doi10.1115/1.3171870
    journal fristpage849
    journal lastpage854
    identifier eissn1528-9036
    keywordsDynamics (Mechanics)
    keywordsMotion
    keywordsStructural frames
    keywordsInertia (Mechanics)
    keywordsEquations of motion
    keywordsShades and shadows
    keywordsVibration AND Dynamic response
    treeJournal of Applied Mechanics:;1986:;volume( 053 ):;issue: 004
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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