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    Stability Analysis of an Extrapolated Force Correction Method for Nonlinear Structural Dynamics

    Source: Journal of Applied Mechanics:;1982:;volume( 049 ):;issue: 001::page 203
    Author:
    D. M. Trujillo
    DOI: 10.1115/1.3161969
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In this paper, conditions for the unconditional stability of an extrapolated force correction method have been identified. The analysis assumed a nonlinear elastodynamic system for which energy is conserved. Some numerical examples are included to demonstrate the performance of the method.
    keyword(s): Force , Stability AND Structural dynamics ,
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      Stability Analysis of an Extrapolated Force Correction Method for Nonlinear Structural Dynamics

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    https://yetl.yabesh.ir/yetl1/handle/yetl/95471
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    contributor authorD. M. Trujillo
    date accessioned2017-05-08T23:12:43Z
    date available2017-05-08T23:12:43Z
    date copyrightMarch, 1982
    date issued1982
    identifier issn0021-8936
    identifier otherJAMCAV-26193#203_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/95471
    description abstractIn this paper, conditions for the unconditional stability of an extrapolated force correction method have been identified. The analysis assumed a nonlinear elastodynamic system for which energy is conserved. Some numerical examples are included to demonstrate the performance of the method.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleStability Analysis of an Extrapolated Force Correction Method for Nonlinear Structural Dynamics
    typeJournal Paper
    journal volume49
    journal issue1
    journal titleJournal of Applied Mechanics
    identifier doi10.1115/1.3161969
    journal fristpage203
    journal lastpage205
    identifier eissn1528-9036
    keywordsForce
    keywordsStability AND Structural dynamics
    treeJournal of Applied Mechanics:;1982:;volume( 049 ):;issue: 001
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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