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    Thermomechanical Response Variability of Stiffened Composite Panels

    Source: Journal of Aerospace Engineering:;2002:;Volume ( 015 ):;issue: 004
    Author:
    Ahmed K. Noor
    ,
    James H. Starnes, Jr.
    ,
    Jeanne M. Peters
    DOI: 10.1061/(ASCE)0893-1321(2002)15:4(154)
    Publisher: American Society of Civil Engineers
    Abstract: A study is made of the variability of the response of stiffened composite panels, associated with variations in the major geometric and material parameters of the structures. The major parameters, which have the most effect on the response quantities of interest, are identified by using a hierarchical sensitivity analysis. The range of variation of the response is determined by using a fuzzy set analysis, with the major parameters treated as fuzzy parameters. Numerical results are presented showing the variability of the response of panels with both continuous and terminated stiffeners associated with variations in the micromechanical, effective layer, and geometric parameters. Both flat and curved panels are considered.
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      Thermomechanical Response Variability of Stiffened Composite Panels

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    contributor authorAhmed K. Noor
    contributor authorJames H. Starnes, Jr.
    contributor authorJeanne M. Peters
    date accessioned2017-05-08T22:17:11Z
    date available2017-05-08T22:17:11Z
    date copyrightOctober 2002
    date issued2002
    identifier other40096361.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/76252
    description abstractA study is made of the variability of the response of stiffened composite panels, associated with variations in the major geometric and material parameters of the structures. The major parameters, which have the most effect on the response quantities of interest, are identified by using a hierarchical sensitivity analysis. The range of variation of the response is determined by using a fuzzy set analysis, with the major parameters treated as fuzzy parameters. Numerical results are presented showing the variability of the response of panels with both continuous and terminated stiffeners associated with variations in the micromechanical, effective layer, and geometric parameters. Both flat and curved panels are considered.
    publisherAmerican Society of Civil Engineers
    titleThermomechanical Response Variability of Stiffened Composite Panels
    typeJournal Paper
    journal volume15
    journal issue4
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)0893-1321(2002)15:4(154)
    treeJournal of Aerospace Engineering:;2002:;Volume ( 015 ):;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
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