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Aeroacoustic Characterization of Single- and Multiscale Porous Fences

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Title: Aeroacoustic Characterization of Single- and Multiscale Porous Fences
Authors: Rodríguez-López, E
Brizzi, LE
Valeau, V
Bruce, PJK
Buxton, ORH
Item Type: Journal Article
Abstract: An experimental characterization of the acoustic behavior and the flowfield past several wall-mounted porous fences is presented. Particle image velocimetry is conducted in the near field of the fences. It shows a spanwise periodicity (associated with the periodic geometry of the grid) of regions where well-defined wakes appear as opposed to regions with a lower mass flow rate influenced by strong recirculations. The acoustic behavior is characterized using a microphone array enabling the spatial locationof noise sourcesto bedetermined. Broadband noise is observed for all grids except for the fractal square grid, where a clear peak appears. The intensity of noise spectra displays scalabilitywith Machnumber M 6 (dipoles), and the preferentialfrequencyfor the fractal square case is shown to scale with thefreestreamvelocity(suggestingasheddingmechanism).For certaingrids, themeanandinstantaneous spatial locations of the noise sources also present a spanwise preferential arrangement coincident with regions where the flow presents well-defined wakes. Regarding the intermittency of the unsteady sources, they present smaller temporal width, separation, and spatial extent for increasing freestream velocity. However, the ratio between these quantities seems to be constant to within 6% for different Mach numbers.
Issue Date: 28-Aug-2017
Date of Acceptance: 13-Jul-2017
URI: http://hdl.handle.net/10044/1/54426
DOI: https://dx.doi.org/10.2514/1.J056057
ISSN: 0001-1452
Publisher: American Institute of Aeronautics and Astronautics
Start Page: 264
End Page: 278
Journal / Book Title: AIAA Journal
Volume: 56
Issue: 1
Copyright Statement: © 2017 by Eduardo Rodríguez-López. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the ISSN 0001-1452 (print) or 1533-385X (online) to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp.
Sponsor/Funder: Commission of the European Communities
Funder's Grant Number: FP7 - 317269
Keywords: Science & Technology
Technology
Engineering, Aerospace
Engineering
NAVIER-STOKES EQUATIONS
AERODYNAMIC DESIGN OPTIMIZATION
DRAG MINIMIZATION
GEOMETRY PARAMETERIZATION
UNSTRUCTURED MESHES
SHAPE OPTIMIZATION
OPTIMUM DESIGN
LINEAR-SYSTEMS
FREE-FORM
ALGORITHM
0901 Aerospace Engineering
0913 Mechanical Engineering
Aerospace & Aeronautics
Publication Status: Published
Appears in Collections:Aeronautics
Faculty of Engineering