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/ | ||||||||||||||||
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Dokumentart: | Zeitschriftenbeitrag | ||||||||||||||||
Titel: | Experimental Study of Trailing-Edge Bluntness Noise Reduction by Porous Plates | ||||||||||||||||
Autoren: |
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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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