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    Biaxial Buckling Analysis of Soft-Core Functionally Graded Graphene-Reinforced Sandwich Plates

    Source: Journal of Aerospace Engineering:;2024:;Volume ( 037 ):;issue: 005::page 04024066-1
    Author:
    Ali Basiri
    ,
    Mohammad Mahdi Kheirikhah
    ,
    Seyyed Mohammad Reza Khalili
    DOI: 10.1061/JAEEEZ.ASENG-5589
    Publisher: American Society of Civil Engineers
    Abstract: Graphene platelets (GPLs) exhibit outstanding mechanical and physical properties and therefore are employed as a reinforcement in advanced polymer composite structures. The purpose of this paper is to analyze the biaxial buckling of functionally graded graphene-reinforced sandwich plates with a soft orthotropic core. A new high-order three-layer theory is developed for the accurate modeling and analysis of the sandwich structure. The sandwich plate is divided into three layers including two face sheets and a core and a different third-order kinematic assumption is dedicated to each layer. The transverse flexibility of each layer as well as the displacements continuity at the interfaces are considered. Additionally, the continuity conditions and the conditions of zero transverse stresses in the whole structure are satisfied. The plate is subjected to a biaxial compressive loading and the governing equations are derived using the principle of minimum potential energy. Analytical solutions are presented for simply supported boundary conditions to obtain the critical buckling load. The influences of plate geometry and GPL properties on buckling load are investigated. The results obtained in specific cases are compared with the published results and the validity of the present results is confirmed. It can be drawn that the use of GPL increases the buckling load of graphene-reinforced sandwich plates.
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      Biaxial Buckling Analysis of Soft-Core Functionally Graded Graphene-Reinforced Sandwich Plates

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4298576
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    contributor authorAli Basiri
    contributor authorMohammad Mahdi Kheirikhah
    contributor authorSeyyed Mohammad Reza Khalili
    date accessioned2024-12-24T10:15:15Z
    date available2024-12-24T10:15:15Z
    date copyright9/1/2024 12:00:00 AM
    date issued2024
    identifier otherJAEEEZ.ASENG-5589.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4298576
    description abstractGraphene platelets (GPLs) exhibit outstanding mechanical and physical properties and therefore are employed as a reinforcement in advanced polymer composite structures. The purpose of this paper is to analyze the biaxial buckling of functionally graded graphene-reinforced sandwich plates with a soft orthotropic core. A new high-order three-layer theory is developed for the accurate modeling and analysis of the sandwich structure. The sandwich plate is divided into three layers including two face sheets and a core and a different third-order kinematic assumption is dedicated to each layer. The transverse flexibility of each layer as well as the displacements continuity at the interfaces are considered. Additionally, the continuity conditions and the conditions of zero transverse stresses in the whole structure are satisfied. The plate is subjected to a biaxial compressive loading and the governing equations are derived using the principle of minimum potential energy. Analytical solutions are presented for simply supported boundary conditions to obtain the critical buckling load. The influences of plate geometry and GPL properties on buckling load are investigated. The results obtained in specific cases are compared with the published results and the validity of the present results is confirmed. It can be drawn that the use of GPL increases the buckling load of graphene-reinforced sandwich plates.
    publisherAmerican Society of Civil Engineers
    titleBiaxial Buckling Analysis of Soft-Core Functionally Graded Graphene-Reinforced Sandwich Plates
    typeJournal Article
    journal volume37
    journal issue5
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/JAEEEZ.ASENG-5589
    journal fristpage04024066-1
    journal lastpage04024066-16
    page16
    treeJournal of Aerospace Engineering:;2024:;Volume ( 037 ):;issue: 005
    contenttypeFulltext
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