In this paper a zeroth-order shear deformation theory has been derived for static and dynamic analysis of laminated composite plates. The responses obtained by the theory for symmetric and antisymmetric laminates are compared with the existing solutions. The comparison firmly establishes that this new shear deformation theory can be used for both thick and thin laminated composite plates with high accuracy.
机构:
Vietnamese German Univ, Dept Computat Engn, Binh Duong New City, Vietnam
Sejong Univ, Dept Architectural Engn, Seoul, South KoreaTon Duc Thang Univ, Div Computat Mech, Ho Chi Minh City, Vietnam
Nguyen-Xuan, H.
Bordas, S. P. A.
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Cardiff Univ, Coll Phys Sci, Sch Engn, Inst Mech & Adv Mat, Cardiff CF10 3AX, S Glam, WalesTon Duc Thang Univ, Div Computat Mech, Ho Chi Minh City, Vietnam
Bordas, S. P. A.
Nguyen-Thanh, N.
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Bauhaus Univ Weimar, Inst Struct Mech, D-99423 Weimar, GermanyTon Duc Thang Univ, Div Computat Mech, Ho Chi Minh City, Vietnam
Nguyen-Thanh, N.
Rabczuk, T.
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Bauhaus Univ Weimar, Inst Struct Mech, D-99423 Weimar, GermanyTon Duc Thang Univ, Div Computat Mech, Ho Chi Minh City, Vietnam
机构:
Univ New S Wales, Sch Civil & Environm Engn, Sydney, NSW 2052, Australia
Hanyang Univ, Dept Civil & Environm Engn, Seoul 133791, South KoreaUniv New S Wales, Sch Civil & Environm Engn, Sydney, NSW 2052, Australia
Thai, Huu-Tai
Choi, Dong-Ho
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Hanyang Univ, Dept Civil & Environm Engn, Seoul 133791, South KoreaUniv New S Wales, Sch Civil & Environm Engn, Sydney, NSW 2052, Australia