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Integrated damping mechanics for thick composite laminates and platesA method for predicting the damped dynamic characteristics of thick composite laminates and plates is presented. Unified damping mechanics relate the damping of composite plates to constituent properties, fiber volume ratio, fiber orientation, laminate configuration, plate geometry, temperature, and moisture. Discrete layer damping mechanics for thick laminates, entailing piecewise continuous displacement fields and including the effects of interlaminar shear damping, are described. A semi-analytical method for predicting the modal damping and natural frequencies of thick simply-supported specialty composite plates is included. Applications demonstrate the validity, merit, and ranges of applicability of the new theory. The applications further illustrate the significance of interlaminar shear damping, and investigate the effects of lamination, thickness aspect ratio, fiber content, and temperature.
Document ID
19950028443
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Saravanos, D. A.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 16, 2013
Publication Date
June 1, 1994
Publication Information
Publication: Journal of Applied Mechanics
ISSN: 0021-8936
Subject Category
Composite Materials
Report/Patent Number
ISSN: 0021-8936
Accession Number
95A60042
Funding Number(s)
CONTRACT_GRANT: NCC3-208/4
Distribution Limits
Public
Copyright
Other

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