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    Quasi-Static and Dynamic Buckling of Thin Cylindrical Shape-Memory Shells

    Source: Journal of Applied Mechanics:;2006:;volume( 073 ):;issue: 005::page 825
    Author:
    Sia Nemat-Nasser
    ,
    Jeom Yong Choi
    ,
    Jon B. Isaacs
    ,
    David W. Lischer
    DOI: 10.1115/1.2165241
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: To investigate the buckling behavior of thin and relatively thick cylindrical shape-memory shells, uniaxial compression tests are performed at a 295K initial temperature, using the CEAM/UCSD’s modified split Hopkinson bar systems and an Instron hydraulic testing machine. The quasi-static buckling response of the shells is directly observed and recorded using a digital camera with a close-up lens and two back mirrors. To document the dynamic buckling modes, a high-speed Imacon 200 framing camera is used. The shape-memory shells with an austenite-finish temperature of Af=281K, buckle gradually and gracefully in quasi-static loading, and fully recover upon unloading, showing a superelastic property, whereas when suitably annealed, the shells do not recover spontaneously upon unloading, but they do so once heated, showing a shape-memory effect. The thin shells had a common thickness of 0.125mm a common outer radius of 2.25mm (i.e., a common radius, R, to thickness, t, ratio, R∕t, of 18). A shell with the ratio of length, L, to diameter, D(L∕D) of 1.5 buckled under a quasi-static load by forming a nonsymmetric chessboard pattern, while with a L∕D of 1.95 the buckling started with the formation of symmetrical rings which then changed into a nonsymmetric chessboard pattern. A similar buckling mode is also observed under a dynamic loading condition for a shell with L∕D of 2. However, thicker shells, with 0.5mm thickness and radius 4mm(R∕t=8), buckled under a dynamic loading condition by the formation of a symmetrical ring pattern. For comparison, we have also tested shells of similar geometry but made of steel and aluminum. In the case of the steel shells with constrained end conditions, the buckling, which consists of nonsymmetric (no rings) folds (chessboard patterns), is sudden and catastrophic, and involves no recovery upon unloading. The gradual buckling of the shape-memory shells is associated with the stress-induced martensite formation and seems to have a profound effect on the unstable deformations of thin structures made from shape-memory alloys.
    keyword(s): Stress , Buckling , Shells , Displacement , Nickel titanium alloys , Shapes AND Temperature ,
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      Quasi-Static and Dynamic Buckling of Thin Cylindrical Shape-Memory Shells

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    http://yetl.yabesh.ir/yetl1/handle/yetl/133004
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    • Journal of Applied Mechanics

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    contributor authorSia Nemat-Nasser
    contributor authorJeom Yong Choi
    contributor authorJon B. Isaacs
    contributor authorDavid W. Lischer
    date accessioned2017-05-09T00:18:34Z
    date available2017-05-09T00:18:34Z
    date copyrightSeptember, 2006
    date issued2006
    identifier issn0021-8936
    identifier otherJAMCAV-26602#825_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/133004
    description abstractTo investigate the buckling behavior of thin and relatively thick cylindrical shape-memory shells, uniaxial compression tests are performed at a 295K initial temperature, using the CEAM/UCSD’s modified split Hopkinson bar systems and an Instron hydraulic testing machine. The quasi-static buckling response of the shells is directly observed and recorded using a digital camera with a close-up lens and two back mirrors. To document the dynamic buckling modes, a high-speed Imacon 200 framing camera is used. The shape-memory shells with an austenite-finish temperature of Af=281K, buckle gradually and gracefully in quasi-static loading, and fully recover upon unloading, showing a superelastic property, whereas when suitably annealed, the shells do not recover spontaneously upon unloading, but they do so once heated, showing a shape-memory effect. The thin shells had a common thickness of 0.125mm a common outer radius of 2.25mm (i.e., a common radius, R, to thickness, t, ratio, R∕t, of 18). A shell with the ratio of length, L, to diameter, D(L∕D) of 1.5 buckled under a quasi-static load by forming a nonsymmetric chessboard pattern, while with a L∕D of 1.95 the buckling started with the formation of symmetrical rings which then changed into a nonsymmetric chessboard pattern. A similar buckling mode is also observed under a dynamic loading condition for a shell with L∕D of 2. However, thicker shells, with 0.5mm thickness and radius 4mm(R∕t=8), buckled under a dynamic loading condition by the formation of a symmetrical ring pattern. For comparison, we have also tested shells of similar geometry but made of steel and aluminum. In the case of the steel shells with constrained end conditions, the buckling, which consists of nonsymmetric (no rings) folds (chessboard patterns), is sudden and catastrophic, and involves no recovery upon unloading. The gradual buckling of the shape-memory shells is associated with the stress-induced martensite formation and seems to have a profound effect on the unstable deformations of thin structures made from shape-memory alloys.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleQuasi-Static and Dynamic Buckling of Thin Cylindrical Shape-Memory Shells
    typeJournal Paper
    journal volume73
    journal issue5
    journal titleJournal of Applied Mechanics
    identifier doi10.1115/1.2165241
    journal fristpage825
    journal lastpage833
    identifier eissn1528-9036
    keywordsStress
    keywordsBuckling
    keywordsShells
    keywordsDisplacement
    keywordsNickel titanium alloys
    keywordsShapes AND Temperature
    treeJournal of Applied Mechanics:;2006:;volume( 073 ):;issue: 005
    contenttypeFulltext
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