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An integrated methodology for optimizing structural composite dampingA method is presented for tailoring plate and shell composite structures for optimal forced damped dynamic response. The damping of specific vibration modes is optimized with respect to dynamic performance criteria including placement of natural frequencies and minimization of resonance amplitudes. The structural composite damping is synthesized from the properties of the constituent materials, laminate parameters, and structural geometry based on a specialty finite element. Application studies include the optimization of laminated composite beams and composite shells with fiber volume ratios and ply angles as design variables. The results illustrate the significance of damping tailoring to the dynamic performance of composite structures, and the effectiveness of the method in optimizing the structural dynamic response.
Document ID
19900002492
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Saravanos, D. A.
(NASA Lewis Research Center Cleveland, OH, United States)
Chamis, C. C.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1989
Subject Category
Composite Materials
Report/Patent Number
NAS 1.15:102343
NASA-TM-102343
E-5051
Report Number: NAS 1.15:102343
Report Number: NASA-TM-102343
Report Number: E-5051
Meeting Information
Meeting: 1989 Winter Annual Meeting of the ASME
Location: San Francisco, CA
Country: United States
Start Date: December 10, 1989
End Date: December 15, 1989
Accession Number
90N11808
Funding Number(s)
PROJECT: RTOP 505-63-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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