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  • Nhan đề: Spectral dynamic stiffness formulation for inplane modal analysis of composite plate assemblies and prismatic solids with arbitrary classical/nonclassical boundary conditions /X. Liu a,b, ⇑
Tác giả CN Liu,X.
Nhan đề Spectral dynamic stiffness formulation for inplane modal analysis of composite plate assemblies and prismatic solids with arbitrary classical/nonclassical boundary conditions /X. Liu a,b, ⇑
Từ khóa tự do Inplane modal analysis
Từ khóa tự do Spectral dynamic stiffness method (SDSM)
Từ khóa tự do Symmetric cross-ply laminated plates
Nguồn trích Composite structures2016-12 Số: 1 Tập: 158
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039|y20170907090437|zcuonglv
100 |aLiu,X.
245 |aSpectral dynamic stiffness formulation for inplane modal analysis of composite plate assemblies and prismatic solids with arbitrary classical/nonclassical boundary conditions /X. Liu a,b, ⇑
653 |aInplane modal analysis
653 |aSpectral dynamic stiffness method (SDSM)
653 |aSymmetric cross-ply laminated plates
773 |tComposite structures|v158|i1|d2016-12
890|c1|a0|b0|d5
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