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Dynamic characteristics of specialty composite structures with embedded damping layersDamping mechanics for simulating the damped dynamic characteristics in specialty composite structures with compliant interlaminar damping layers are presented. Finite-element based mechanics incorporating a discrete layer (or layer-wise) laminate damping theory are utilized to represent general laminate configurations in terms of lay-up and fiber orientation angles, cross-sectional thickness, shape, and boundary conditions. Evaluations of the method with exact solutions and experimental data illustrate the accuracy of the method. Additional applications investigate the potential for significant damping enhancement in angle-ply composite laminates with cocured interlaminar damping layers.
Document ID
19930017516
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Saravanos, D. A.
(Ohio Aerospace Inst. Brook Park., United States)
Chamis, C. C.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1993
Subject Category
Composite Materials
Report/Patent Number
NASA-TM-106165
NAS 1.15:106165
E-7863
Report Number: NASA-TM-106165
Report Number: NAS 1.15:106165
Report Number: E-7863
Meeting Information
Meeting: Symposium on Vibroacoustic Characterization of Materials and Structures
Location: Anaheim, CA
Country: United States
Start Date: November 8, 1992
End Date: November 12, 1992
Sponsors: ASME
Accession Number
93N26705
Funding Number(s)
CONTRACT_GRANT: NCC3-208/4
PROJECT: RTOP 510-02-12
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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