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    Nonlinear Buckling of Composite Shells of Revolution

    Source: Journal of Aerospace Engineering:;2002:;Volume ( 015 ):;issue: 002
    Author:
    Jinsong Huang
    DOI: 10.1061/(ASCE)0893-1321(2002)15:2(64)
    Publisher: American Society of Civil Engineers
    Abstract: By adopting the energy method, a method of calculating the stability of the rotational composite shell is presented that takes into account the influence of nonlinear prebuckling deformations and stresses on the buckling of the shell. The relationships between the prebuckling deformations and strains are calculated by nonlinear Karman equations. The numerical method is used to calculate the energy of the whole system. The nonlinear equation is solved by combining the gradient method and the amended Newton iterative method. A computer program is also developed. Examples are given to demonstrate the accuracy of the method presented in this paper.
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      Nonlinear Buckling of Composite Shells of Revolution

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    contributor authorJinsong Huang
    date accessioned2017-05-08T21:16:06Z
    date available2017-05-08T21:16:06Z
    date copyrightApril 2002
    date issued2002
    identifier other%28asce%290893-1321%282002%2915%3A2%2864%29.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/44962
    description abstractBy adopting the energy method, a method of calculating the stability of the rotational composite shell is presented that takes into account the influence of nonlinear prebuckling deformations and stresses on the buckling of the shell. The relationships between the prebuckling deformations and strains are calculated by nonlinear Karman equations. The numerical method is used to calculate the energy of the whole system. The nonlinear equation is solved by combining the gradient method and the amended Newton iterative method. A computer program is also developed. Examples are given to demonstrate the accuracy of the method presented in this paper.
    publisherAmerican Society of Civil Engineers
    titleNonlinear Buckling of Composite Shells of Revolution
    typeJournal Paper
    journal volume15
    journal issue2
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)0893-1321(2002)15:2(64)
    treeJournal of Aerospace Engineering:;2002:;Volume ( 015 ):;issue: 002
    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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