TY - GEN
T1 - OPTIMAL DESIGN OF CONSTRAINED PLATE DAMPING LAYERS USING CONTINUUM FINITE ELEMENTS
AU - Lumsdaine, Arnold
AU - Scott, Richard A.
N1 - Publisher Copyright:
© 1996 American Society of Mechanical Engineers (ASME). All rights reserved.
PY - 1996
Y1 - 1996
N2 - The aim of this paper is to determine the optimal shape of a viscoelastic damping layer within a constrained layer plate that is undergoing harmonic excitation at its midpoint. The optimization objective is to minimize the peak displacement of the plate at the first resonant frequency. The material loss factor is monitored as well to determine the improvement in performance between an initial, uniform layer shape and the optimized shape. A fine mesh validation model is also created to verify the optimized shape. As manufacturing costs would be reduced for a uniform shape, the optimized shape is used as a guide to create a new, uniform damping layer, which is compared with the previous results. Several geometries and boundary conditions are examined. The ABAQUS finite element code is used to model the structures. Elasticity theory based continuum elements are used so that all stress effects are taken into account in the models. The optimization code uses a Sequential Quadratic Programming algorithm. Results show significant improvement in the loss factor for optimized shapes. For most models, the optimal shape tends towards being a thin, uniform damping layer, which indicates shearing effects dominate in producing the optimal shape. In one case, however, it appears that some normal stress effects also have some influence.
AB - The aim of this paper is to determine the optimal shape of a viscoelastic damping layer within a constrained layer plate that is undergoing harmonic excitation at its midpoint. The optimization objective is to minimize the peak displacement of the plate at the first resonant frequency. The material loss factor is monitored as well to determine the improvement in performance between an initial, uniform layer shape and the optimized shape. A fine mesh validation model is also created to verify the optimized shape. As manufacturing costs would be reduced for a uniform shape, the optimized shape is used as a guide to create a new, uniform damping layer, which is compared with the previous results. Several geometries and boundary conditions are examined. The ABAQUS finite element code is used to model the structures. Elasticity theory based continuum elements are used so that all stress effects are taken into account in the models. The optimization code uses a Sequential Quadratic Programming algorithm. Results show significant improvement in the loss factor for optimized shapes. For most models, the optimal shape tends towards being a thin, uniform damping layer, which indicates shearing effects dominate in producing the optimal shape. In one case, however, it appears that some normal stress effects also have some influence.
UR - http://www.scopus.com/inward/record.url?scp=85169411819&partnerID=8YFLogxK
U2 - 10.1115/IMECE1996-0217
DO - 10.1115/IMECE1996-0217
M3 - Conference contribution
AN - SCOPUS:85169411819
T3 - ASME International Mechanical Engineering Congress and Exposition, Proceedings (IMECE)
SP - 159
EP - 168
BT - Noise Control and Acoustics
PB - American Society of Mechanical Engineers (ASME)
T2 - ASME 1996 International Mechanical Engineering Congress and Exposition, IMECE 1996
Y2 - 17 November 1996 through 22 November 1996
ER -