4.5 Article

Acoustic and vibration response of a structure with added noise control treatment under various excitations

Journal

JOURNAL OF THE ACOUSTICAL SOCIETY OF AMERICA
Volume 135, Issue 2, Pages 693-704

Publisher

ACOUSTICAL SOC AMER AMER INST PHYSICS
DOI: 10.1121/1.4861361

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Funding

  1. Fonds Quebecois de la Recherche sur la Nature et les Technologies as part of NSERC Chair in Aviation Acoustics
  2. Bombardier aerospace as part of NSERC Chair in Aviation Acoustics

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The evaluation of the acoustic performance of noise control treatments is of great importance in many engineering applications, e. g., aircraft, automotive, and building acoustics applications. Numerical methods such as finite-and boundary elements allow for the study of complex structures with added noise control treatment. However, these methods are computationally expensive when used for complex structures. At an early stage of the acoustic trim design process, many industries look for simple and easy to use tools that provide sufficient physical insight that can help to formulate design criteria. The paper presents a simple and tractable approach for the acoustic design of noise control treatments. It presents and compares two transfer matrix-based methods to investigate the vibroacoustic behavior of noise control treatments. The first is based on a modal approach, while the second is based on wave-number space decomposition. In addition to the classical rain-on-the-roof and diffuse acoustic field excitations, the paper also addresses turbulent boundary layer and point source (monopole) excitations. Various examples are presented and compared to a finite element calculation to validate the methodology and to confirm its relevance along with its limitations. (C) 2014 Acoustical Society of America.

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