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Shock and Vibration
Volume 19, Issue 4, Pages 693-705

Prediction of Turbulent Boundary Layer Induced Noise in the Cabin of a BWB Aircraft

Joana Rocha,1 Afzal Suleman,1 and Fernando Lau2

1Department of Mechanical Engineering, University of Victoria, Victoria, BC, Canada
2Departamento de Engenharia Mecânica (Aeroespacial), Instituto Superior Técnico, Lisboa, Portugal

Received 3 April 2011; Revised 30 October 2011

Copyright © 2012 Hindawi Publishing Corporation. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.

Citations to this Article [4 citations]

The following is the list of published articles that have cited the current article.

  • Joana Rocha, “Sound Radiation and Vibration of Composite Panels Excited by Turbulent Flow: Analytical Prediction and Analysis,” Shock and Vibration, vol. 2014, pp. 1–18, 2014. View at Publisher · View at Google Scholar
  • A Caiazzo, N Alujević, B Pluymers, and W Desmet, “Active control of turbulent boundary layer sound transmission into a vehicle interior,” Journal of Physics: Conference Series, vol. 744, pp. 012026, 2016. View at Publisher · View at Google Scholar
  • Pengbo Li, Yunju Yan, and Huagang Lin, “Numerical simulation and experimental researches on the vibration–acoustic coupled property of an aircraft model under strong reverberation noise,” Journal of Vibration and Control, vol. 23, no. 17, pp. 2757–2766, 2016. View at Publisher · View at Google Scholar
  • A. Caiazzo, N. Alujević, B. Pluymers, and W. Desmet, “Active control of turbulent boundary layer-induced sound transmission through the cavity-backed double panels,” Journal of Sound and Vibration, vol. 422, pp. 161–188, 2018. View at Publisher · View at Google Scholar