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    Calculation of the Response of a Composite Plate to Localized Dynamic Surface Loads Using a New Wave Number Integral Method

    Source: Journal of Applied Mechanics:;2005:;volume( 072 ):;issue: 001::page 18
    Author:
    Sauvik Banerjee
    ,
    Ph.D. Student
    ,
    Assoc. Mem. ASME
    ,
    William Prosser
    ,
    Ajit Mal
    DOI: 10.1115/1.1828064
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This study is motivated by the need for an efficient and accurate tool to analyze the wave field produced by localized dynamic sources on the surface or the interior of isotropic plates and anisotropic composite laminates. A semi-analytical method based on the wave number integral representation of the elastodynamic field is described that reduces the overall computational effort significantly over other available methods. This method is used to calculate the guided wave field produced in a thin unidirectional graphite/epoxy composite laminate by a dynamic surface point load. The results are compared with those obtained from a finite element analysis, showing excellent agreement, except for minor differences at higher frequencies. A recently discovered feature of the calculated surface motion, namely, a spatially periodic “phase reversal” of the main pulse with propagation distance, is observed in both cases. The present work is expected to be helpful in developing impact damage monitoring systems in defect-critical structural components through real time analysis of acoustic emission wave forms.
    keyword(s): Composite materials , Stress , Waves , Frequency , Plates (structures) AND Laminates ,
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      Calculation of the Response of a Composite Plate to Localized Dynamic Surface Loads Using a New Wave Number Integral Method

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    http://yetl.yabesh.ir/yetl1/handle/yetl/131263
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    contributor authorSauvik Banerjee
    contributor authorPh.D. Student
    contributor authorAssoc. Mem. ASME
    contributor authorWilliam Prosser
    contributor authorAjit Mal
    date accessioned2017-05-09T00:15:07Z
    date available2017-05-09T00:15:07Z
    date copyrightJanuary, 2005
    date issued2005
    identifier issn0021-8936
    identifier otherJAMCAV-26588#18_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/131263
    description abstractThis study is motivated by the need for an efficient and accurate tool to analyze the wave field produced by localized dynamic sources on the surface or the interior of isotropic plates and anisotropic composite laminates. A semi-analytical method based on the wave number integral representation of the elastodynamic field is described that reduces the overall computational effort significantly over other available methods. This method is used to calculate the guided wave field produced in a thin unidirectional graphite/epoxy composite laminate by a dynamic surface point load. The results are compared with those obtained from a finite element analysis, showing excellent agreement, except for minor differences at higher frequencies. A recently discovered feature of the calculated surface motion, namely, a spatially periodic “phase reversal” of the main pulse with propagation distance, is observed in both cases. The present work is expected to be helpful in developing impact damage monitoring systems in defect-critical structural components through real time analysis of acoustic emission wave forms.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleCalculation of the Response of a Composite Plate to Localized Dynamic Surface Loads Using a New Wave Number Integral Method
    typeJournal Paper
    journal volume72
    journal issue1
    journal titleJournal of Applied Mechanics
    identifier doi10.1115/1.1828064
    journal fristpage18
    journal lastpage24
    identifier eissn1528-9036
    keywordsComposite materials
    keywordsStress
    keywordsWaves
    keywordsFrequency
    keywordsPlates (structures) AND Laminates
    treeJournal of Applied Mechanics:;2005:;volume( 072 ):;issue: 001
    contenttypeFulltext
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