A Finite Element Analysis Based on Higher-order Zig-zag Shell Theory for Laminated Composites with Multiple Delaminations
45th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conference
01.01.2004
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Efficient Higher Order Shell Theory for Laminated Composites with Multiple Delaminations
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|Postbuckling of laminated composites with delaminations
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