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The Acoustic Analogy: A Powerful Tool in Aeroacoustics with Emphasis on Jet Noise PredictionThe acoustic analogy introduced by Lighthill to study jet noise is now over 50 years old. In the present paper, Lighthill s Acoustic Analogy is revisited together with a brief evaluation of the state-of-the-art of the subject and an exploration of the possibility of further improvements in jet noise prediction from analytical methods, computational fluid dynamics (CFD) predictions, and measurement techniques. Experimental Particle Image Velocimetry (PIV) data is used both to evaluate turbulent statistics from Reynolds-averaged Navier-Stokes (RANS) CFD and to propose correlation models for the Lighthill stress tensor. The NASA Langley Jet3D code is used to study the effect of these models on jet noise prediction. From the analytical investigation, a retarded time correction is shown that improves, by approximately 8 dB, the over-prediction of aft-arc jet noise by Jet3D. In experimental investigation, the PIV data agree well with the CFD mean flow predictions, with room for improvement in Reynolds stress predictions. Initial modifications, suggested by the PIV data, to the form of the Jet3D correlation model showed no noticeable improvements in jet noise prediction.
Document ID
20040075530
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Farassat, F.
(NASA Langley Research Center Hampton, VA, United States)
Doty, Michael J.
(National Academy of Sciences - National Research Council Hampton, VA, United States)
Hunter, Craig A.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 7, 2013
Publication Date
May 7, 2004
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
AIAA Paper 2004-2872
Meeting Information
Meeting: 10th AIAA/CEAS Aeroacoustics Conference
Location: Manchester
Country: United Kingdom
Start Date: May 10, 2004
End Date: May 12, 2004
Sponsors: American Inst. of Aeronautics and Astronautics, National Oceanic and Atmospheric Administration
Funding Number(s)
OTHER: 23-781-10-12-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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