Modeled and Measured Dynamics of a Composite Beam with Periodically Varying Foam Core

By: Nasa, National Aeronautics and Space Adm

The 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. Cabell, Randolph H. and Cano, Roberto J. and Schiller, Noah H. and Roberts Gary D. Langley Research Center NASA/TM-2012-217565, L-20116, NF1676L-14167

• Format: Paperback
• Language: English
• ISBN: 1794364781
• ISBN13: 9781794364783
• Release Date: January 1
• Publisher: Independently Published
• Length: 32 Pages
• Weight: 0.22 lbs.
• Dimensions: 0.1" x 8.5" x 11.0"