Dynamic analysis and design of laminated composite beams with multiple damping layers
- 1 April 1993
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 31 (4) , 736-745
- https://doi.org/10.2514/3.11611
Abstract
No abstract availableThis publication has 9 references indexed in Scilit:
- Analysis of natural frequencies and modal loss factors of simply supported beams with adhesively bonded double-strap jointsThe Journal of the Acoustical Society of America, 1992
- Vibration analysis of adhesively bonded lap joint, part II: Numerical solutionJournal of Sound and Vibration, 1992
- Vibration analysis of adhesively bonded lap joint, part I: TheoryJournal of Sound and Vibration, 1992
- An Analytical Model for the Vibration of Laminated Beams Including the Effects of Both Shear and Thickness Deformation in the Adhesive LayerJournal of Vibration and Acoustics, 1986
- The prediction of the damping effectiveness of multiple constrained layer damping treatmentsThe Journal of the Acoustical Society of America, 1979
- Frequency and Loss Factors of Sandwich Beams under Various Boundary ConditionsJournal of Mechanical Engineering Science, 1978
- On the dynamic response of a rectangular sandwich plate with viscoelastic core and generally orthotropic facingsJournal of Sound and Vibration, 1976
- The forced vibration of a three-layer, damped sandwich beam with arbitrary boundary conditionsJournal of Sound and Vibration, 1969
- Theory of Vibratory Bending for Elastic and Viscoelastic Layered Finite-Length BeamsJournal of Applied Mechanics, 1965