Buckling and vibration analysis of laminated composite plate/shell structures via a smoothed quadrilateral flat shell element with in-plane rotations

Computers and Structures

Volumn 89, Issue 7-8, 2011, Pages 612-625

  Nguyen Van, H ^a,c   Mai Duy, N ^a   Karunasena, W ^b   Tran Cong, T ^a  

^a UNIVERSITY OF SOUTHERN QUEENSLAND   (Australia)

^b UNIVERSITY OF SOUTHERN QUEENSLAND   (Australia)

^c UNIVERSITY OF ARCHITECTURE HO CHI MINH CITY   (Viet Nam)

Author keywords

Buckling response; Laminated composite plate and shell; Locking free; Natural vibration; Strain smoothing method

Indexed keywords

BUCKLING RESPONSE; FLAT ELEMENTS; FLAT SHELL; FREE-VIBRATION ANALYSIS; GEOMETRIC STIFFNESS; INPLANE ROTATION; LAMINATED COMPOSITE PLATES; LOCKING-FREE; MODULUS RATIO; NATURAL VIBRATION; NUMERICAL EXAMPLE; NUMERICAL SOLUTION; SMOOTHING TECHNIQUES; SPAN-TO-THICKNESS RATIO;

BUCKLING; DELAMINATION; LAMINATED COMPOSITES; LAMINATING; PLATES (STRUCTURAL COMPONENTS); SHELLS (STRUCTURES); STIFFNESS MATRIX;

VIBRATION ANALYSIS;

EID: 79952280151     PISSN: 00457949     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.compstruc.2011.01.005     Document Type: Article

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