A C0 element for the free vibration analysis of laminated composite plates

Journal of Sound and Vibration

Volumn 191, Issue 5, 1996, Pages 721-738

  Shankara, C A ^a,b   Iyengar, N G R ^a  

^a INDIAN INSTITUTE OF TECHNOLOGY KANPUR   (India)

^b AERONAUTICAL DEVELOPMENT AGENCY   (India)

Author keywords

[No Author keywords available]

Indexed keywords

ASPECT RATIO; CALCULATIONS; DYNAMICS; ELASTICITY; FINITE ELEMENT METHOD; LAMINATED COMPOSITES; MATHEMATICAL MODELS; PLATES (STRUCTURAL COMPONENTS); SHEAR DEFORMATION; SHEAR STRESS; THREE DIMENSIONAL;

CONTINUOUS FINITE ELEMENT MODEL; DISPLACEMENT FIELD MODEL; FIRST ORDER SHEAR DEFORMATION THEORY; HIGHER ORDER SHEAR DEFORMATION THEORY; SIDE TO THICKNESS RATIO; TRANSVERSE SHEAR STRESS;

VIBRATIONS (MECHANICAL);

EID: 0030126897     PISSN: 0022460X     EISSN: None     Source Type: Journal    
DOI: 10.1006/jsvi.1996.0152     Document Type: Article

References (29)

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