Free vibration of laminated composite plates with a central circular hole

Composite Structures

Volumn 35, Issue 4, 1996, Pages 357-368

  Chai, Gin Boay ^a  

^a NANYANG TECHNOLOGICAL UNIVERSITY   (Singapore)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; ASPECT RATIO; BOUNDARY CONDITIONS; COMPOSITE STRUCTURES; COMPUTER SIMULATION; FINITE ELEMENT METHOD; LAMINATED COMPOSITES; NUMERICAL ANALYSIS; STACKING FAULTS; VIBRATIONS (MECHANICAL);

COUPLING RESPONSE; FREE VIBRATION; HOLE SIZE; LAMINATED COMPOSITE PLATE; STACKING SEQUENCE;

PLATES (STRUCTURAL COMPONENTS);

EID: 0030204253     PISSN: 02638223     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0263-8223(96)00037-2     Document Type: Article

References (16)

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