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Advances in Acoustics and Vibration
Volume 2011, Article ID 573209, 9 pages
http://dx.doi.org/10.1155/2011/573209
Research Article

A Theoretical Basis for the Scaling Law of Broadband Shock Noise Intensity in Supersonic Jets

ASRC Aerospace, NASA Kennedy Space Center, Merritt Island, FL 32899, USA

Received 8 September 2010; Accepted 27 January 2011

Academic Editor: Lars Hakansson

Copyright © 2011 Max Kandula. 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

Max Kandula, “A Theoretical Basis for the Scaling Law of Broadband Shock Noise Intensity in Supersonic Jets,” Advances in Acoustics and Vibration, vol. 2011, Article ID 573209, 9 pages, 2011. https://doi.org/10.1155/2011/573209.