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    Efficient C0 Finite Element Formulation for Thermal Stress Analysis of Laminated Composite and Sandwich Plates

    Source: Journal of Aerospace Engineering:;2015:;Volume ( 028 ):;issue: 004
    Author:
    Wu Zhen
    ,
    Lin Kun
    DOI: 10.1061/(ASCE)AS.1943-5525.0000450
    Publisher: American Society of Civil Engineers
    Abstract: By introducing thermal expansion coefficients in the transverse displacement field, this paper proposes an approach to improve the performance of the global-local higher-order theory for thermal stress analysis of laminated composite plates. Transverse normal deformation has been considered in the proposed model, whereas the additional displacement variables have not increased because thermal loads could be included in the generalized force vector. The proposed model a priori satisfies the continuity conditions of transverse shear stresses at interfaces, and the number of displacement variables involved in the present model is independent of the number of layers. The derivatives of transverse displacement have been eliminated from the displacement field so that the
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      Efficient C0 Finite Element Formulation for Thermal Stress Analysis of Laminated Composite and Sandwich Plates

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    http://yetl.yabesh.ir/yetl1/handle/yetl/71744
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    contributor authorWu Zhen
    contributor authorLin Kun
    date accessioned2017-05-08T22:07:16Z
    date available2017-05-08T22:07:16Z
    date copyrightJuly 2015
    date issued2015
    identifier other29661369.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/71744
    description abstractBy introducing thermal expansion coefficients in the transverse displacement field, this paper proposes an approach to improve the performance of the global-local higher-order theory for thermal stress analysis of laminated composite plates. Transverse normal deformation has been considered in the proposed model, whereas the additional displacement variables have not increased because thermal loads could be included in the generalized force vector. The proposed model a priori satisfies the continuity conditions of transverse shear stresses at interfaces, and the number of displacement variables involved in the present model is independent of the number of layers. The derivatives of transverse displacement have been eliminated from the displacement field so that the
    publisherAmerican Society of Civil Engineers
    titleEfficient C0 Finite Element Formulation for Thermal Stress Analysis of Laminated Composite and Sandwich Plates
    typeJournal Paper
    journal volume28
    journal issue4
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)AS.1943-5525.0000450
    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
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