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    Effects of Bonding Stiffness on Thermal Stresses in Sandwich Panels

    Source: Journal of Aerospace Engineering:;1992:;Volume ( 005 ):;issue: 004
    Author:
    R. Hussein
    ,
    P. Fazio
    ,
    K. Ha
    DOI: 10.1061/(ASCE)0893-1321(1992)5:4(480)
    Publisher: American Society of Civil Engineers
    Abstract: Sandwich panels made of thin skins and a lightweight core expand and/or bow when subjected to temperature changes. The significance of induced thermal stresses in the panels depends on material properties. The effects of bonding layers on these stresses were not investigated in available works on the structural analysis of sandwich panels. This paper presents elasticity solutions for thermal stresses in sandwich panels with interlayer slip. The effects of finite bonding stiffnesses on the structural behavior of the panels are investigated. The numerical results show that the bonding stiffness, up to a certain level, has a strong effect on panel structural response. The answer to what constitutes perfect bonding is best answered in terms of the ratio of the core stiffness to the bonding stiffness. A heat chamber is designed and used to test sandwich specimens under different temperature changes. The experimental values for normal stresses in the skins are in good agreement with the present theory.
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      Effects of Bonding Stiffness on Thermal Stresses in Sandwich Panels

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    contributor authorR. Hussein
    contributor authorP. Fazio
    contributor authorK. Ha
    date accessioned2017-05-08T21:15:44Z
    date available2017-05-08T21:15:44Z
    date copyrightOctober 1992
    date issued1992
    identifier other%28asce%290893-1321%281992%295%3A4%28480%29.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/44752
    description abstractSandwich panels made of thin skins and a lightweight core expand and/or bow when subjected to temperature changes. The significance of induced thermal stresses in the panels depends on material properties. The effects of bonding layers on these stresses were not investigated in available works on the structural analysis of sandwich panels. This paper presents elasticity solutions for thermal stresses in sandwich panels with interlayer slip. The effects of finite bonding stiffnesses on the structural behavior of the panels are investigated. The numerical results show that the bonding stiffness, up to a certain level, has a strong effect on panel structural response. The answer to what constitutes perfect bonding is best answered in terms of the ratio of the core stiffness to the bonding stiffness. A heat chamber is designed and used to test sandwich specimens under different temperature changes. The experimental values for normal stresses in the skins are in good agreement with the present theory.
    publisherAmerican Society of Civil Engineers
    titleEffects of Bonding Stiffness on Thermal Stresses in Sandwich Panels
    typeJournal Paper
    journal volume5
    journal issue4
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)0893-1321(1992)5:4(480)
    treeJournal of Aerospace Engineering:;1992:;Volume ( 005 ):;issue: 004
    contenttypeFulltext
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