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Modeled and Measured Dynamics of a Composite Beam with Periodically Varying Foam CoreThe dynamics of a sandwich beam with carbon fiber composite facesheets and foam core with periodic variations in material properties are studied. The purpose of the study is to compare finite element predictions with experimental measurements on fabricated beam specimens. For the study, three beams were fabricated: one with a compliant foam core, a second with a stiffer core, and a third with the two cores alternating down the length of the beam to create a periodic variation in properties. This periodic variation produces a bandgap in the frequency domain where vibrational energy does not readily propagate down the length of the beam. Mode shapes and natural frequencies are compared, as well as frequency responses from point force input to velocity response at the opposite end of the beam.
Document ID
20120007100
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Cabell, Randolph H.
(NASA Langley Research Center Hampton, VA, United States)
Cano, Roberto J.
(NASA Langley Research Center Hampton, VA, United States)
Schiller, Noah H.
(NASA Langley Research Center Hampton, VA, United States)
Roberts Gary D.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 25, 2013
Publication Date
April 1, 2012
Subject Category
Composite Materials
Report/Patent Number
NASA/TM-2012-217565
L-20116
NF1676L-14167
Report Number: NASA/TM-2012-217565
Report Number: L-20116
Report Number: NF1676L-14167
Funding Number(s)
WBS: WBS 877868.02.07.07.04.01.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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