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Experimental Study of Trailing-Edge Bluntness Noise Reduction by Porous Plates

Kershner, John und Jaworski, Justin und Geyer, Thomas (2024) Experimental Study of Trailing-Edge Bluntness Noise Reduction by Porous Plates. AIAA Journal. American Institute of Aeronautics and Astronautics (AIAA). doi: 10.2514/1.J064045. ISSN 0001-1452.

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Offizielle URL: https://arc.aiaa.org/doi/10.2514/1.J064045

Kurzfassung

The acoustic and aerodynamic fields of blunt porous plates are examined experimentally in an effort to mitigate trailing-edge bluntness noise. The plates are characterized by a single dimensionless porosity parameter identified in previous works that controls the influence of porosity on the sound field. Hot-wire anemometry interrogates the velocity field to connect turbulence details of specific regions to flow noise directivity and beamforming source maps. Porous plates are demonstrated to reduce the bluntness-induced noise by up to 17 dB and progressively suppress broadband low-frequency noise as the value of the porosity parameter increases. However, an increase in this parameter also increases the high-frequency noise created by the pores themselves. The same highly perforated plate characterized by a large value of the porosity parameter reduces the bluntness-induced vortex shedding that is present in the wake of the impermeable plate. Lastly, pore shape and positional alignment are shown to have a complex effect on the acoustic field. Among the porosity designs considered, plates with circular pores are most effective for low-frequency noise reductions but generate high-frequency noise. No meaningful difference is found between the acoustic spectra from plates of the same open-area fraction with pores aligned along or staggered about the flow direction.

elib-URL des Eintrags:https://elib.dlr.de/205681/
Dokumentart:Zeitschriftenbeitrag
Titel:Experimental Study of Trailing-Edge Bluntness Noise Reduction by Porous Plates
Autoren:
AutorenInstitution oder E-Mail-AdresseAutoren-ORCID-iDORCID Put Code
Kershner, JohnLehigh UniversityNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Jaworski, JustinVirginia TechNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Geyer, Thomasthomas.geyer (at) dlr.dehttps://orcid.org/0000-0003-2380-1188166199727
Datum:5 August 2024
Erschienen in:AIAA Journal
Referierte Publikation:Ja
Open Access:Nein
Gold Open Access:Nein
In SCOPUS:Ja
In ISI Web of Science:Ja
DOI:10.2514/1.J064045
Verlag:American Institute of Aeronautics and Astronautics (AIAA)
ISSN:0001-1452
Status:veröffentlicht
Stichwörter:Aircraft Wing Design, Overall Sound Pressure Level, Boundary Layer Thickness, Turbulence Intensity, Free Stream Velocity, Porous Materials, Noise Reduction, Aeroacoustic Noise, Trailing Edge Noise, Vortex Shedding
HGF - Forschungsbereich:Luftfahrt, Raumfahrt und Verkehr
HGF - Programm:Luftfahrt
HGF - Programmthema:Umweltschonender Antrieb
DLR - Schwerpunkt:Luftfahrt
DLR - Forschungsgebiet:L CP - Umweltschonender Antrieb
DLR - Teilgebiet (Projekt, Vorhaben):L - Komponenten und Emissionen
Standort: Cottbus
Institute & Einrichtungen:Institut für Elektrifizierte Luftfahrtantriebe
Hinterlegt von: Geyer, Thomas
Hinterlegt am:26 Aug 2024 14:08
Letzte Änderung:11 Nov 2024 14:48

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