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Shock and Vibration
Volume 19 (2012), Issue 4, Pages 693-705
http://dx.doi.org/10.3233/SAV-2011-0660

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.

How to Cite this Article

Joana Rocha, Afzal Suleman, and Fernando Lau, “Prediction of Turbulent Boundary Layer Induced Noise in the Cabin of a BWB Aircraft,” Shock and Vibration, vol. 19, no. 4, pp. 693-705, 2012. doi:10.3233/SAV-2011-0660