Coupled modification of natural frequencies and buckling loads of composite cylindrical panels

International Journal of Mechanical Sciences

Volumn 51, Issue 9-10, 2009, Pages 708-717

  Shahab, S ^a   Mirzaeifar, R ^b   Bahai, H ^a  

^a BRUNEL UNIVERSITY   (United Kingdom)

^b Georgia Institute of Technology   (United States)

Author keywords

Buckling load; Composite cylindrical panel; Eigenvalue; Eigenvector; Natural frequency

Indexed keywords

ALGEBRAIC SYSTEM; ARBITRARY ANGLES; BUCKLING LOAD; BUCKLING LOADS; COMPOSITE CYLINDRICAL PANEL; CYLINDRICAL PANELS; EIGENVALUE; EIGENVALUES; EIGENVECTOR; INVERSE EIGENVALUE PROBLEMS; LAYERED COMPOSITES; OBJECTIVE FUNCTIONS; SECOND ORDER DERIVATIVES; SIMULTANEOUS EQUATIONS; STACKING SEQUENCE; TAYLOR EXPANSIONS;

EIGENVALUES AND EIGENFUNCTIONS; NATURAL FREQUENCIES;

BUCKLING;

EID: 70349462805     PISSN: 00207403     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.ijmecsci.2009.08.002     Document Type: Article

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