Analytical Solutions to Vibration of Generally Layered Composite Beams
Abstract
Dynamic equations governing the free vibration of laminated composite beams are developed using Hamilton's principle. The effects of transverse shear and rotary inertia are included in the energy formulation. Analytical solutions are obtained by the method of Lagrange multipliers wherein the free vibration problem is posed as a constrained variational problem, the constraints being imposed through Lagrange multipliers. Natural frequencies and mode shapes of clamped-clamped and clamped-supported composite beams are presented to demonstrate the efficiency of the methodology.
Recommended Citation
S. Krishnaswamy et al., "Analytical Solutions to Vibration of Generally Layered Composite Beams," Journal of Sound and Vibration, Elsevier, Jan 1992.
The definitive version is available at https://doi.org/10.1016/0022-460X(92)90452-4
Department(s)
Mechanical and Aerospace Engineering
International Standard Serial Number (ISSN)
0022-460X
Document Type
Article - Journal
Document Version
Citation
File Type
text
Language(s)
English
Rights
© 1992 Elsevier, All rights reserved.
Publication Date
01 Jan 1992