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Comparison of Two Acoustic Waveguide Methods for Determining Liner ImpedanceAcoustic measurements taken in a flow impedance tube are used to assess the relative accuracy of two waveguide methods for impedance eduction in the presence of grazing flow. The aeroacoustic environment is assumed to contain forward and backward-traveling acoustic waves, consisting of multiple modes, and uniform mean flow. Both methods require a measurement of the complex acoustic pressure profile over the length of the test liner. The Single Mode Method assumes that the sound pressure level and phase decay-rates of a single progressive mode can be extracted from this measured complex acoustic pressure profile. No a priori assumptions are made in the Finite Element. Method regarding the modal or reflection content in the measured acoustic pressure profile. The integrity of each method is initially demonstrated by how well their no-flow impedances match those acquired in a normal incidence impedance tube. These tests were conducted using ceramic tubular and conventional perforate liners. Ceramic tubular liners were included because of their impedance insensitivity to mean flow effects. Conversely, the conventional perforate liner was included because its impedance is known to be sensitive to mean flow velocity effects. Excellent comparisons between impedance values educed with the two waveguide methods in the absence of mean flow and the corresponding values educed with the normal incident impedance tube were observed. The two methods are then compared for mean flow Mach numbers up to 0.5, and are shown to give consistent results for both types of test liners. The quality of the results indicates that the Single Mode Method should be used when the measured acoustic pressure profile is clearly dominated by a single progressive mode, and the Finite Element Method should be used for all other cases.
Document ID
20010057034
Acquisition Source
Langley Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Jones, Michael G.
(NASA Langley Research Center Hampton, VA United States)
Watson, Willie R.
(NASA Langley Research Center Hampton, VA United States)
Tracy, Maureen B.
(NASA Langley Research Center Hampton, VA United States)
Parrott, Tony L.
(NASA Langley Research Center Hampton, VA United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2001
Subject Category
Acoustics
Report/Patent Number
AIAA Paper 2001-2266
Report Number: AIAA Paper 2001-2266
Meeting Information
Meeting: 7th AIAA/CEAS Aeroacoustics Conference
Location: Maastricht
Country: Netherlands
Start Date: May 28, 2001
End Date: May 30, 2001
Sponsors: Confederation of European Aerospace Societies, American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Public Use Permitted.
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