Buckling analysis of a composite shell with multiple delaminations based on a higher order zig-zag theory

Finite Elements in Analysis and Design

Volumn 44, Issue 11, 2008, Pages 675-685

  Oh, Jinho ^a   Cho, Maenghyo ^a   Kim, Jun Sik ^b  

^a Seoul National University   (South Korea)

^b The Pennsylvania State University   (United States)

Author keywords

Buckling analysis; Finite element formulation; General tensor formulation; Multiple delaminations; Zig zag shell theory

Indexed keywords

BENDING (DEFORMATION); BENDING TESTS; BOUNDARY CONDITIONS; BOUNDARY VALUE PROBLEMS; BUCKLING; COMPOSITE STRUCTURES; DELAMINATION; FINITE ELEMENT METHOD; FUNCTION EVALUATION; LAMINATED COMPOSITES; MECHANICS; NUMERICAL ANALYSIS;

(1 1 0) SURFACE; ARBITRARY BOUNDARY CONDITIONS; BUCKLING ANALYSIS; COMPOSITE CYLINDRICAL SHELLS; COMPOSITE SHELLS; CRITICAL BUCKLING LOADS; CURVILINEAR COORDINATE SYSTEMS; DEGREES OF FREEDOM; FINITE ELEMENT (FE); FINITE ELEMENT (FE) FORMULATION; FLAT SURFACES; GENERAL (CO); HIGHER ORDER; LAMINATED COMPOSITE SHELLS; LINEAR BUCKLING; MODE SHAPES; MULTIPLE DELAMINATIONS; NUMERICAL EXAMPLES; OUT OF PLANE; PATCH TESTING; PLATE BENDING ELEMENT; SHAPE FUNCTIONS; SHELL ELEMENTS; SHELL FINITE ELEMENTS; SHELL STRUCTURES; SHELL THEORY; SURFACE REPRESENTATION; TENSOR NOTATION; ZIG ZAG; ZIG ZAG THEORY;

SHELLS (STRUCTURES);

EID: 48949115377     PISSN: 0168874X     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.finel.2008.03.007     Document Type: Article

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