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    Mixed Experimental‐Structural Model for Interlaminar Shear Fracture Toughness

    Source: Journal of Aerospace Engineering:;1991:;Volume ( 004 ):;issue: 001
    Author:
    William E. Bachrach
    ,
    Thomas R. Hicks
    ,
    Zbigniew S. Habas
    ,
    Dianne M. Granata
    DOI: 10.1061/(ASCE)0893-1321(1991)4:1(108)
    Publisher: American Society of Civil Engineers
    Abstract: For brittle composite materials, a mixed experimental and structural model is developed to determine a consistent interlaminar shear fracture toughness
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      Mixed Experimental‐Structural Model for Interlaminar Shear Fracture Toughness

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/44692
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    • Journal of Aerospace Engineering

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    contributor authorWilliam E. Bachrach
    contributor authorThomas R. Hicks
    contributor authorZbigniew S. Habas
    contributor authorDianne M. Granata
    date accessioned2017-05-08T21:15:37Z
    date available2017-05-08T21:15:37Z
    date copyrightJanuary 1991
    date issued1991
    identifier other%28asce%290893-1321%281991%294%3A1%28108%29.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/44692
    description abstractFor brittle composite materials, a mixed experimental and structural model is developed to determine a consistent interlaminar shear fracture toughness
    publisherAmerican Society of Civil Engineers
    titleMixed Experimental‐Structural Model for Interlaminar Shear Fracture Toughness
    typeJournal Paper
    journal volume4
    journal issue1
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)0893-1321(1991)4:1(108)
    treeJournal of Aerospace Engineering:;1991:;Volume ( 004 ):;issue: 001
    contenttypeFulltext
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