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High Intensity Modal Impedance Tube Development at NASA LangleyA High Intensity Modal Impedance Tube (HIMIT) was developed for evaluation of acoustic liners in a normal incidence, high sound pressure level (SPL), and high frequency environment. Capabilities of the HIMIT are demonstrated here by testing three classes of acoustic liners: a narrow chamber liner, conventional single degree of freedom liners, and over-the-rotor liners. The experimental results are compared to results in NASA Langley's Normal Incidence Tube (NIT) for validation. The Zwikker and Kosten Transmission Line (ZKTL) model is also compared to the HIMIT results for selected configurations to study its applicability at high SPLs and frequencies. The HIMIT and NIT impedance spectra compare favorably up to 3.0 kHz, which is the upper frequency limit of the NIT analysis. The ZKTL model was used at frequencies up to 6.0 kHz and showed great comparison for the entire frequency range tested, indicating that the model may be used at high frequencies when the plane wave mode is dominant.
Document ID
20230000292
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Chelsea Solano
(Langley Research Center Hampton, Virginia, United States)
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)
Date Acquired
January 10, 2023
Publication Date
February 1, 2023
Subject Category
Acoustics
Report/Patent Number
NASA/TM-20230000292
Funding Number(s)
WBS: 081876.02.07.50.10.02.03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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