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    Elasticity Solutions for Hertzian Loaded Composite Sandwich Plates

    Source: Journal of Aerospace Engineering:;1997:;Volume ( 010 ):;issue: 001
    Author:
    Eric J. Herup
    ,
    Anthony N. Palazotto
    DOI: 10.1061/(ASCE)0893-1321(1997)10:1(27)
    Publisher: American Society of Civil Engineers
    Abstract: The elasticity solutions for composite laminates in bending originally developed by Pagano are extended for Hertzian contact-type loading in this paper. Two solutions are obtained, corresponding to cylindrical bending and three-dimensional bending of a rectangular plate. Loads simulating contact with a spherical indentor are obtained by superposition of the elasticity solutions for individual terms of truncated Fourier sine series representations of Hertzian contact stresses. In this way, a benchmark for models of impact loaded plates is provided in which the loading is more representative of contact than the solutions often used for that purpose. The solutions provide insight into the interpretation of experimental data from low-velocity impact tests and are used to judge the performance of finite-element–based low-velocity impact algorithms in predicting stress under the impactor.
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      Elasticity Solutions for Hertzian Loaded Composite Sandwich Plates

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    contributor authorEric J. Herup
    contributor authorAnthony N. Palazotto
    date accessioned2017-05-08T21:15:53Z
    date available2017-05-08T21:15:53Z
    date copyrightJanuary 1997
    date issued1997
    identifier other%28asce%290893-1321%281997%2910%3A1%2827%29.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/44841
    description abstractThe elasticity solutions for composite laminates in bending originally developed by Pagano are extended for Hertzian contact-type loading in this paper. Two solutions are obtained, corresponding to cylindrical bending and three-dimensional bending of a rectangular plate. Loads simulating contact with a spherical indentor are obtained by superposition of the elasticity solutions for individual terms of truncated Fourier sine series representations of Hertzian contact stresses. In this way, a benchmark for models of impact loaded plates is provided in which the loading is more representative of contact than the solutions often used for that purpose. The solutions provide insight into the interpretation of experimental data from low-velocity impact tests and are used to judge the performance of finite-element–based low-velocity impact algorithms in predicting stress under the impactor.
    publisherAmerican Society of Civil Engineers
    titleElasticity Solutions for Hertzian Loaded Composite Sandwich Plates
    typeJournal Paper
    journal volume10
    journal issue1
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)0893-1321(1997)10:1(27)
    treeJournal of Aerospace Engineering:;1997:;Volume ( 010 ):;issue: 001
    contenttypeFulltext
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