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Effects of Cavity Diameter on Acoustic Impedance in a Complex Acoustic EnvironmentThis paper investigates the effects of cavity diameter on the acoustic performance of conventional perforate-over-honeycomb liners. This investigation is a follow up to a previous study where it was demonstrated that the cavity diameter has a relatively small effect on the acoustic impedance for core cavity diameters up to 2.0 inches. In the current study, liner concepts are exposed to a complex acoustic environment, where higher-order modes are present. Four liner configurations are explored in this investigation, which include two cavity cores of different cavity diameters combined with two facesheets. These configurations are tested in the Grazing Flow Impedance Tube (GFIT) at Mach 0.0, 0.3, and 0.5 at a source sound pressure level of 150 dB. A comparison of the acoustic performance of these samples suggests that the cavity diameter has a relatively small effect on the acoustic impedance for core cavity diameters up to 2.0 inches at these conditions. These configurations are exposed to a more complex acoustic environment (e.g., higher-order modes) in the Curved Duct Test Rig (CDTR) at Mach 0.0 and 0.3.
Document ID
20190027208
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Brown, M. C.
(NASA Langley Research Center Hampton, VA, United States)
Jones, M. G.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
July 11, 2019
Publication Date
June 18, 2018
Subject Category
Aircraft Design, Testing And Performance
Aircraft Propulsion And Power
Report/Patent Number
NF1676L-28604
Meeting Information
Meeting: AIAA/CEAS Aeroacoustics Conference (2018 AIAA Aviation)
Location: Atlanta, GA
Country: United States
Start Date: June 25, 2018
End Date: June 29, 2018
Sponsors: American Institute of Aeronautics and Astronautics (AIAA)
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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