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Implementation of the NASA High Intensity Modal Impedance TubeThis paper provides a description of the High Intensity Modal Impedance Tube (HIMIT) and its use for the evaluation of acoustic liners. Tests conducted with two liners, one linear and one nonlinear, are used to evaluate the suitability of the HIMIT for evaluation at frequencies up to 6 kHz and sound pressure levels up to 155 dB. Two impedance eduction methods are used, one suitable for plane wave frequencies and the other applicable over the full frequency range. These educed impedances are compared against those computed with an impedance prediction method and against those educed with another zero-flow test rig. These results confirm that the HIMIT can be used with confidence for the evaluation of acoustic liners over these frequency and sound pressure level ranges.
Document ID
20220017773
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Michael G Jones
(Langley Research Center Hampton, Virginia, United States)
Alexander N Carr
(Langley Research Center Hampton, Virginia, United States)
Douglas M Nark
(Langley Research Center Hampton, Virginia, United States)
Lawrence E Becker
(Analytical Services & Materials (United States) Hampton, Virginia, United States)
Date Acquired
November 24, 2022
Publication Date
December 1, 2022
Subject Category
Acoustics
Report/Patent Number
NASA/TM-20220017773
Funding Number(s)
WBS: 081876.02.07.50.10.02.03
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
impedance
modal decomposition
HIMIT
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