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Investigation of Physical Mechanisms for Jet Noise Reduction By Plug Nozzle Porosity This paper presents the results of a computational and experimental study on porous plug nozzles and the fluid mechanisms surrounding their observed noise reduction. The study explores a wide range of porous plug geometries, encompassing variations in hole size, plug length and porosity. Computational fluid dynamics (CFD) analyses are employed in concert with an advanced automated mesh refinement (AMR) scheme to investigate porous plug nozzle design strategies that may diminish shock strength, flow separation, and other undesirable characteristics associated with high noise levels. A selected subset of the porous plug nozzles that were analyzed computationally were fabricated at subscale and tested experimentally, obtaining far-field noise spectral data and schlieren flow visualizations. Detailed comparisons between CFD predictions and experimental results were focused on gaining an improved understanding of underlying physical mechanisms responsible for noise reduction associated with the porous plugs.
Document ID
20250006610
Acquisition Source
Glenn Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
John Henry Korth
(Glenn Research Center Cleveland, United States)
Jonathan M Burt
(Glenn Research Center Cleveland, United States)
Khairul B M Q Zaman
(Glenn Research Center Cleveland, United States)
Amy Fagan
(Glenn Research Center Cleveland, United States)
Date Acquired
June 27, 2025
Publication Date
September 30, 2025
Publication Information
Publication: AIAA Journal
Publisher: American Institute of Aeronautics and Astronautics
ISSN: 0001-1452
e-ISSN: 1533-385X
Subject Category
Acoustics
Aerodynamics
Funding Number(s)
WBS: 110076.02.03.04.50
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
Single Expert
Keywords
jets
nozzles
surface porosity
plugs
supersonic flow
shocks
noise
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