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    The Effect of a Normal Shock on the Aeroelastic Stability of a Panel

    Source: Journal of Applied Mechanics:;1983:;volume( 050 ):;issue: 002::page 275
    Author:
    M. H. Williams
    DOI: 10.1115/1.3167032
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The effect of a standing shock wave on the static and dynamic aeroelastic stability of a flexible panel is investigated using a linear structural and aerodynamic theoretical model. It is found that the shock is generally stabilizing. The lowest critical dynamic pressures are associated with shock positions downstream from the panel, where the panel is uninfluenced by the shock.
    keyword(s): Stability , Shock (Mechanics) AND Shock waves ,
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      The Effect of a Normal Shock on the Aeroelastic Stability of a Panel

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    https://yetl.yabesh.ir/yetl1/handle/yetl/96652
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    contributor authorM. H. Williams
    date accessioned2017-05-08T23:14:46Z
    date available2017-05-08T23:14:46Z
    date copyrightJune, 1983
    date issued1983
    identifier issn0021-8936
    identifier otherJAMCAV-26217#275_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/96652
    description abstractThe effect of a standing shock wave on the static and dynamic aeroelastic stability of a flexible panel is investigated using a linear structural and aerodynamic theoretical model. It is found that the shock is generally stabilizing. The lowest critical dynamic pressures are associated with shock positions downstream from the panel, where the panel is uninfluenced by the shock.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleThe Effect of a Normal Shock on the Aeroelastic Stability of a Panel
    typeJournal Paper
    journal volume50
    journal issue2
    journal titleJournal of Applied Mechanics
    identifier doi10.1115/1.3167032
    journal fristpage275
    journal lastpage282
    identifier eissn1528-9036
    keywordsStability
    keywordsShock (Mechanics) AND Shock waves
    treeJournal of Applied Mechanics:;1983:;volume( 050 ):;issue: 002
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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