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Measurement Of Trailing Edge Noise using Directional Array and Coherent Output Power MethodsThe use of a directional array of microphones for the measurement of trailing edge (TE) noise is described. The capabilities of this method are evaluated via measurements of TE noise from a NACA 63-215 airfoil model and from a cylindrical rod. This TE noise measurement approach is compared to one that is based on the cross spectral analysis of output signals from a pair of microphones (COP method). Advantages and limitations of both methods are examined. It is shown that the microphone array can accurately measures TE noise and captures its two-dimensional characteristic over a large frequency range for any TE configuration as long as noise contamination from extraneous sources is within bounds. The COP method is shown to also accurately measure TE noise but over a more limited frequency range that narrows for increased TE thickness. Finally, the applicability and generality of an airfoil self-noise prediction method was evaluated via comparison to the experimental data obtained using the COP and array measurement methods. The predicted and experimental results are shown to agree over large frequency ranges.
Document ID
20030063924
Acquisition Source
Headquarters
Document Type
Reprint (Version printed in journal)
Authors
Hutcheson, Florence V.
(NASA Langley Research Center Hampton, VA, United States)
Brooks, Thomas F.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 21, 2013
Publication Date
January 1, 2002
Publication Information
Publication: Aeroacoustics
Volume: 1
Issue: 4
Subject Category
Acoustics
Distribution Limits
Public
Copyright
Public Use Permitted.
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