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    Thermal Stresses in Spherical Shells

    Source: Journal of Aerospace Engineering:;1993:;Volume ( 006 ):;issue: 001
    Author:
    Pei Jianping
    ,
    Issam E. Harik
    DOI: 10.1061/(ASCE)0893-1321(1993)6:1(106)
    Publisher: American Society of Civil Engineers
    Abstract: This paper presents an iterative finite-difference technique for the analysis of axisymmetric spherical shells with variable wall thickness. The formulation is based on thin elastic shell theory. One-dimensional finite-difference points are used to discretize the shell into strips along the meridian, and an iterative technique is employed to determine the normal and meridional displacements. The stress resultants and bending stresses are then evaluated. Unlike existing analytical and finite-difference techniques, the proposed method is applicable with ease to any variation in rigidity along the meridian, to general loading conditions, and to steep and shallow shells. Results are presented and compared with those of the finite-element method.
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      Thermal Stresses in Spherical Shells

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    http://yetl.yabesh.ir/yetl1/handle/yetl/44756
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    contributor authorPei Jianping
    contributor authorIssam E. Harik
    date accessioned2017-05-08T21:15:45Z
    date available2017-05-08T21:15:45Z
    date copyrightJanuary 1993
    date issued1993
    identifier other%28asce%290893-1321%281993%296%3A1%28106%29.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/44756
    description abstractThis paper presents an iterative finite-difference technique for the analysis of axisymmetric spherical shells with variable wall thickness. The formulation is based on thin elastic shell theory. One-dimensional finite-difference points are used to discretize the shell into strips along the meridian, and an iterative technique is employed to determine the normal and meridional displacements. The stress resultants and bending stresses are then evaluated. Unlike existing analytical and finite-difference techniques, the proposed method is applicable with ease to any variation in rigidity along the meridian, to general loading conditions, and to steep and shallow shells. Results are presented and compared with those of the finite-element method.
    publisherAmerican Society of Civil Engineers
    titleThermal Stresses in Spherical Shells
    typeJournal Paper
    journal volume6
    journal issue1
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)0893-1321(1993)6:1(106)
    treeJournal of Aerospace Engineering:;1993:;Volume ( 006 ):;issue: 001
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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