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    On the Stability of the Equilibrium of Nonconservative Continuous Systems With Slight Damping

    Source: Journal of Applied Mechanics:;1967:;volume( 034 ):;issue: 002::page 344
    Author:
    S. Nemat-Nasser
    DOI: 10.1115/1.3607688
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The stability of the equilibrium configuration of a linearly elastic solid (with or without internal damping) subjected to partial follower surface tractions (nonconservative loading) is studied. Proportional loading is considered and it is proved that the flutter (oscillations with increasing amplitude) load parameter of the undamped system is an upper bound for that of the system with slight damping. The necessary and sufficient condition for stability of the equilibrium state with respect to flutter-type motions, and sufficiency conditions for stability with respect to both divergence (or buckling) and flutter, are established. Based on energy considerations, an approximate method of stability analysis is suggested which reduces to the usual energy criterion for the cases of conservative loading.
    keyword(s): Stability , Equilibrium (Physics) , Damping , Flutter (Aerodynamics) , Motion , Stress , Buckling AND Oscillations ,
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      On the Stability of the Equilibrium of Nonconservative Continuous Systems With Slight Damping

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    http://yetl.yabesh.ir/yetl1/handle/yetl/116767
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    contributor authorS. Nemat-Nasser
    date accessioned2017-05-08T23:49:48Z
    date available2017-05-08T23:49:48Z
    date copyrightJune, 1967
    date issued1967
    identifier issn0021-8936
    identifier otherJAMCAV-25850#344_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/116767
    description abstractThe stability of the equilibrium configuration of a linearly elastic solid (with or without internal damping) subjected to partial follower surface tractions (nonconservative loading) is studied. Proportional loading is considered and it is proved that the flutter (oscillations with increasing amplitude) load parameter of the undamped system is an upper bound for that of the system with slight damping. The necessary and sufficient condition for stability of the equilibrium state with respect to flutter-type motions, and sufficiency conditions for stability with respect to both divergence (or buckling) and flutter, are established. Based on energy considerations, an approximate method of stability analysis is suggested which reduces to the usual energy criterion for the cases of conservative loading.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleOn the Stability of the Equilibrium of Nonconservative Continuous Systems With Slight Damping
    typeJournal Paper
    journal volume34
    journal issue2
    journal titleJournal of Applied Mechanics
    identifier doi10.1115/1.3607688
    journal fristpage344
    journal lastpage348
    identifier eissn1528-9036
    keywordsStability
    keywordsEquilibrium (Physics)
    keywordsDamping
    keywordsFlutter (Aerodynamics)
    keywordsMotion
    keywordsStress
    keywordsBuckling AND Oscillations
    treeJournal of Applied Mechanics:;1967:;volume( 034 ):;issue: 002
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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