000014261 001__ 14261
000014261 005__ 20161115100146.0
000014261 04107 $$aeng
000014261 046__ $$k2016-08-21
000014261 100__ $$aAbedi, Mehrnoosh
000014261 24500 $$aDamping of laminated plates: boundary condition and lamination sequence effects

000014261 24630 $$n24.$$p24th International Congress of Theoretical and Applied Mechanics - Book of Papers
000014261 260__ $$bInternational Union of Theoretical and Applied Mechanics, 2016
000014261 506__ $$arestricted
000014261 520__ $$2eng$$aThe present study is aimed at determination of an optimal fiber orientation for the maximum modal structural damping of laminates based on in-plane viscoelastic properties obtained for a highly directional out-of-autoclave carbon/epoxy system using the dynamic mechanical analysis. The validation of material loss factors is also provided by conducting experimental modal analysis on unidirectional beam components with preferential ply angles subjected to an impulse excitation. Three different lamination sequences under the combination of clamped and free boundary conditions are taken into account. Under each boundary condition, the effect of fiber orientation on variation of modal loss factor and frequency associated with the first mode of flexural vibration is also studied.

000014261 540__ $$aText je chráněný podle autorského zákona č. 121/2000 Sb.
000014261 653__ $$a

000014261 7112_ $$a24th International Congress of Theoretical and Applied Mechanics$$cMontreal (CA)$$d2016-08-21 / 2016-08-26$$gICTAM2016
000014261 720__ $$aAbedi, Mehrnoosh
000014261 8560_ $$ffischerc@itam.cas.cz
000014261 8564_ $$s176115$$uhttps://invenio.itam.cas.cz/record/14261/files/PO.SM08-1.02.134.pdf$$yOriginal version of the author's contribution as presented on CD,  page 2346, code PO.SM08-1.02.134
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000014261 962__ $$r13812
000014261 980__ $$aPAPER