Variable-kinematics approach for linearized buckling analysis of laminated plates and shells

AIAA Journal

Volumn 48, Issue 9, 2010, Pages 1987-1996

  D'Ottavio, M ^a,c   Carrera, E ^b  

^a UNIVERSITÉ PARIS OUEST NANTERRE LA DÉFENSE   (France)

^b POLITECNICO DI TORINO   (Italy)

^c Department of Aerospace Engineering   (France)

Author keywords

[No Author keywords available]

Indexed keywords

BUCKLING ANALYSIS; BUCKLING LOADS; CARRERA'S UNIFIED FORMULATION; CLOSED FORM SOLUTIONS; CONSTANT STRESS; DOUBLY CURVED SHELLS; EIGENVALUE PROBLEM; INTERLAMINAR; LAMINATED PLATE; LAYER-WISE; MULTI-LAYERED; MULTILAYERED PLATES; NORMAL STRESS; ORTHOTROPIC LAYERS; REISSNER'S MIXED VARIATIONAL THEOREMS; SIMPLY SUPPORTED; SINGLE LAYER; STABILITY EQUATIONS; TRANSVERSE SHEAR;

BUCKLING; CRACK INITIATION; EIGENVALUES AND EIGENFUNCTIONS; ELASTICITY; KINEMATICS; LAMINATING; LINEARIZATION; STRUCTURAL DESIGN;

SHELLS (STRUCTURES);

EID: 77957104807     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/1.J050203     Document Type: Article

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