NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Tailoring of composite links for optimal damped elasto-dynamic performanceA method is developed for the optimal design of composite links based on dynamic performance criteria directly related to structural modal damping and dynamic stiffness. An integrated mechanics theory correlates structural composite damping to the parameters of basic composite material systems, laminate parameters, link shape, and modal deformations. The inclusion of modal properties allows the selective minimization of vibrations associated with specific modes. Ply angles and fiber volumes are tailored to obtain optimal combinations of damping and stiffness. Applications to simple composite links indicate wide margins for trade-offs and illustrate the importance of various design variables to the optimal design.
Document ID
19890017541
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
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 1.15:102094
NASA-TM-102094
E-4875
Report Number: NAS 1.15:102094
Report Number: NASA-TM-102094
Report Number: E-4875
Meeting Information
Meeting: Design Automation Conference
Location: Montreal, Quebec
Country: Canada
Start Date: September 17, 1989
End Date: September 20, 1989
Sponsors: ASME
Accession Number
89N26912
Funding Number(s)
PROJECT: RTOP 505-63-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available