Vibration behavior of thick composite laminated plates subject to in-plane pre-stress loading

2007 Proceedings of the ASME International Design Engineering Technical Conferences and Computers and Information in Engineering Conference, DETC2007

Volumn 1 PART C, Issue , 2008, Pages 2105-2114

  Fiedler, Lars ^a   Lacarbonara, Walter ^b   Vestroni, Fabrizio ^b  

^a AIRBUS OPERATIONS GMBH   (Germany)

^b SAPIENZA UNIVERSITY OF ROME   (Italy)

Author keywords

[No Author keywords available]

Indexed keywords

ADMISSIBLE FUNCTIONS; ARBITRARY DEGREES; COMPOSITE LAMINATED PLATES; DISPLACEMENT FIELDS; ENERGY FUNCTIONALS; GENERALIZED COORDINATES; GEOMETRIC STIFFNESS MATRICES; HIGHER-ORDER THEORY; IN-PLANE (IP); IN-PLANE LOADING; INDEPENDENT PARAMETERS; INTERNATIONAL DESIGNS; LAMINATED COMPOSITE PLATES; MASS MATRICES; MECHANICAL VIBRATIONS; POLYNOMIAL SERIES; PRE STRESSING; TECHNICAL CONFERENCES; THICKNESS DIRECTION; VARIATIONS OF; VIBRATION BEHAVIORS; VIBRATION PROPERTIES; WIDTH-TO-THICKNESS RATIO;

ARCHITECTURAL DESIGN; COMPUTER NETWORKS; COMPUTERS; ELASTIC MODULI; ENGINEERING; LAMINATED COMPOSITES; LAMINATING; LATTICE VIBRATIONS; LOADING; MATRIX ALGEBRA; MOLECULAR BEAM EPITAXY; PLATES (STRUCTURAL COMPONENTS); STIFFNESS MATRIX; TECHNOLOGY; VIBRATION CONTROL; VIBRATORS;

VIBRATIONS (MECHANICAL);

EID: 44849104819     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/DETC2007-35532     Document Type: Conference Paper

References (12)

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