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    Efficient Failure Analysis of Laminated Composites and Sandwich Cylindrical Shells Based on Higher-Order Zigzag Theory

    Source: Journal of Aerospace Engineering:;2015:;Volume ( 028 ):;issue: 004
    Author:
    Ajay Kumar
    ,
    Anupam Chakrabarti
    ,
    Pradeep Bhargava
    ,
    Vipul Prakash
    DOI: 10.1061/(ASCE)AS.1943-5525.0000433
    Publisher: American Society of Civil Engineers
    Abstract: An efficient failure analysis of laminated composite and sandwich cylindrical shell is done for the first time using an efficient
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      Efficient Failure Analysis of Laminated Composites and Sandwich Cylindrical Shells Based on Higher-Order Zigzag Theory

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/74258
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    contributor authorAjay Kumar
    contributor authorAnupam Chakrabarti
    contributor authorPradeep Bhargava
    contributor authorVipul Prakash
    date accessioned2017-05-08T22:13:34Z
    date available2017-05-08T22:13:34Z
    date copyrightJuly 2015
    date issued2015
    identifier other39904659.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/74258
    description abstractAn efficient failure analysis of laminated composite and sandwich cylindrical shell is done for the first time using an efficient
    publisherAmerican Society of Civil Engineers
    titleEfficient Failure Analysis of Laminated Composites and Sandwich Cylindrical Shells Based on Higher-Order Zigzag Theory
    typeJournal Paper
    journal volume28
    journal issue4
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)AS.1943-5525.0000433
    treeJournal of Aerospace Engineering:;2015:;Volume ( 028 ):;issue: 004
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian