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Multi-objective shape and material optimization of composite structures including dampingA multi-objective optimal design methodology is developed for light-weight, low cost composite structures of improved dynamic performance. The design objectives include minimization of resonance amplitudes (or maximization of modal damping), weight, and material cost. The design vector includes micromechanics, laminate, and structural shape parameters. Performance constraints are imposed on static displacements, dynamic amplitudes, and natural frequencies. The effects of damping on the dynamics of composite structures are incorporated. Preliminary applications on a cantilever composite beam illustrated that only the proposed multi-objective optimization, as opposed to single objective functions, simultaneously improved all objectives. The significance of composite damping in the design of advanced composite structures was also demonstrated, indicating the design methods based on undamped dynamics may fail to improve the dynamic performance near resonances.
Document ID
19900011816
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Saravanos, D. A.
(Case Western Reserve Univ. Cleveland, OH., United States)
Chamis, Christos C.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1990
Subject Category
Composite Materials
Report/Patent Number
NAS 1.15:102579
E-5410
NASA-TM-102579
Report Number: NAS 1.15:102579
Report Number: E-5410
Report Number: NASA-TM-102579
Meeting Information
Meeting: Structures, Structural Dynamics, and Materials Conference
Location: Long Beach, CA
Country: United States
Start Date: April 2, 1990
End Date: April 4, 1990
Sponsors: AHS, ASME, AIAA, ASCE, ASC
Accession Number
90N21132
Funding Number(s)
PROJECT: RTOP 505-63-1B
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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