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Integrated analysis and design of thick composite structures for optimal passive damping characteristicsThe development of novel composite mechanics for the analysis of damping in composite laminates and structures and the more significant results of this effort are summarized. Laminate mechanics based on piecewise continuous in-plane displacement fields are described that can represent both intralaminar stresses and interlaminar shear stresses and the associated effects on the stiffness and damping characteristics of a composite laminate. Among other features, the mechanics can accurately model the static and damped dynamic response of either thin or thick composite laminates, as well as, specialty laminates with embedded compliant damping layers. The discrete laminate damping theory is further incorporated into structural analysis methods. In this context, an exact semi-analytical method for the simulation of the damped dynamic response of composite plates was developed. A finite element based method and a specialty four-node plate element were also developed for the analysis of composite structures of variable shape and boundary conditions. Numerous evaluations and applications demonstrate the quality and superiority of the mechanics in predicting the damped dynamic characteristics of composite structures. Finally, additional development was focused on the development of optimal tailoring methods for the design of thick composite structures based on the developed analytical capability. Applications on composite plates illustrated the influence of composite mechanics in the optimal design of composites and the potential for significant deviations in the resultant designs when more simplified (classical) laminate theories are used.
Document ID
19930014240
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Saravanos, D. A.
(Ohio Aerospace Inst. Brook Park, OH, United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1993
Subject Category
Composite Materials
Report/Patent Number
NASA-CR-190783
NAS 1.26:190783
E-7676
Report Number: NASA-CR-190783
Report Number: NAS 1.26:190783
Report Number: E-7676
Accession Number
93N23429
Funding Number(s)
PROJECT: RTOP 505-63-5B
CONTRACT_GRANT: NCC3-208/4
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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