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Some Analytic Results for the Study of Broadband Noise Radiation from Wings, Propellers and Jets in Uniform MotionAlan Powell has made significant contributions to the understanding of many aeroacoustic problems, in particular, the problems of broadband noise from jets and boundary layers. In this paper, some analytic results are presented for the calculation of the correlation function of the broadband noise radiated from a wing, a propeller, and a jet in uniform forward motion. It is shown that, when the observer (or microphone) motion is suitably chosen, the geometric terms of the radiation formula become time independent. The time independence of these terms leads to a significant simplification of the statistical analysis of the radiated noise, even when the near field terms are included. For a wing in forward motion, if the observer is in the moving reference frame, then the correlation function of the near and far field noise can be related to a space-time cross-correlation function of the pressure on the wing surface. A similar result holds for a propeller in forward flight if the observer is in a reference frame that is attached to the propeller and rotates at the shaft speed. For a jet in motion, it is shown that the correlation function of the radiated noise can be related to the space-time crosscorrelation of the Lighthill stress tensor in the jet. Exact analytical results are derived for all three cases. For the cases under present consideration, the inclusion of the near field terms does not introduce additional complexity, as compared to existing formulations that are limited to the far field.
Document ID
20040040195
Acquisition Source
Langley Research Center
Document Type
Reprint (Version printed in journal)
Authors
Farassat, F.
(NASA Langley Research Center Hampton, VA, United States)
Casper, J.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2003
Publication Information
Publication: International Journal of Aeroacoustics
Publisher: Multi-Science Publishing Co. Ltd.
Volume: 2
Issue: 4-Mar
Subject Category
Aircraft Design, Testing And Performance
Funding Number(s)
OTHER: 23-781-10-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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