Wave propagation in curved laminate composite structures

Authors

  • Sebastian Ghinet Department of Mechanical Engineering, Université de Sherbrooke, 2500 Boulevard Université, Sherbrooke, Que. J1K 2R1, Canada
  • Noureddine Atalla Department of Mechanical Engineering, Université de Sherbrooke, 2500 Boulevard Université, Sherbrooke, Que. J1K 2R1, Canada
  • Haisam Osman Boeing Company, 5301 Bolsa Avenue, Huntington Beach, CA 92647, United States

Keywords:

Acoustic waves, Computer simulation, Data reduction, Eigenvalues and eigenfunctions, Laminated composites, Modal analysis, Shearing, Strain, Vectors, Radiation loss, Ring frequency, Transmission loss, Transversal shearing

Abstract

A model to compute the transmission loss of the sandwich and laminate composite curved panels was developed. The physical behaviour of the panel was represented using a discrete lamina description and each lamina was represented by membrane, bending, transversal shearing and rotational inertial behaviour. The model density, the radiation efficiency and the resononant and non-resonant transmission loss were calculted by using the dispersion relation's solution. It was observed that for the presented problem, the modal energy exchange was dominated by the first wave solution. The result shows that for acoustic trasmission problems, the SEA scheme is accurate.

Additional Files

Published

2004-09-01

How to Cite

1.
Ghinet S, Atalla N, Osman H. Wave propagation in curved laminate composite structures. Canadian Acoustics [Internet]. 2004 Sep. 1 [cited 2024 Sep. 17];32(3):162-3. Available from: https://jcaa.caa-aca.ca/index.php/jcaa/article/view/1678

Issue

Vol. 32 No. 3 (2004)

Section

Proceedings of the Acoustics Week in Canada

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