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Transfer function modeling of damping mechanisms in distributed parameter modelsThis work formulates a method for the modeling of material damping characteristics in distributed parameter models which may be easily applied to models such as rod, plate, and beam equations. The general linear boundary value vibration equation is modified to incorporate hysteresis effects represented by complex stiffness using the transfer function approach proposed by Golla and Hughes. The governing characteristic equations are decoupled through separation of variables yielding solutions similar to those of undamped classical theory, allowing solution of the steady state as well as transient response. Example problems and solutions are provided demonstrating the similarity of the solutions to those of the classical theories and transient responses of nonviscous systems.
Document ID
19940031388
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Slater, J. C.
(State Univ. of New York Buffalo, NY, United States)
Inman, D. J.
(State Univ. of New York Buffalo, NY, United States)
Date Acquired
September 6, 2013
Publication Date
June 1, 1994
Publication Information
Publication: NASA. Langley Research Center, NASA Workshop on Distributed Parameter Modeling and Control of Flexible Aerospace Systems
Subject Category
Structural Mechanics
Accession Number
94N35895
Funding Number(s)
CONTRACT_GRANT: NGT-50541
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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