elib
DLR-Header
DLR-Logo -> http://www.dlr.de
DLR Portal Home | Impressum | Datenschutz | Kontakt | English
Schriftgröße: [-] Text [+]

Hydrodynamic/acoustic splitting approach with flow-acoustic feedback for universal subsonic noise computation

Ewert, Roland und Kreuzinger, Johannes (2021) Hydrodynamic/acoustic splitting approach with flow-acoustic feedback for universal subsonic noise computation. Journal of Computational Physics (444). Elsevier. doi: 10.1016/j.jcp.2021.110548. ISSN 0021-9991.

[img] PDF - Preprintversion (eingereichte Entwurfsversion)
4MB

Offizielle URL: https://www.sciencedirect.com/science/article/pii/S0021999121004435

Kurzfassung

A generalized approach to decompose the compressible Navier-Stokes equations into an equivalent set of coupled equations for flow and acoustics is introduced. As a significant extension to standard hydrodynamic/acoustic splitting methods, the approach provides the essential coupling terms, which account for the feedback from the acoustics to the flow. A unique simplified version of the split equation system with feedback is derived that conforms to the compressible Navier-Stokes equations in the subsonic flow regime, where the feedback reduces to one additional term in the flow momentum equation. Subsonic simulations are conducted for flow-acoustic feedback cases using a scale-resolving runtime coupled hierarchical Cartesian mesh solver, which operates with different explicit time step sizes for incompressible flow and acoustics. The first simulation case focuses on the tone of a generic flute. With the flow-acoustic feedback term included, the simulation produces the tone characteristics similar to those obtained by Kühnelt with a LatticeBoltzmann method. In a contrasting manner, the simulation lacks the proper tone without the feedback term included. As the second simulation case, a thick plate in a duct is studied at various low Mach numbers around the Parker-beta-mode resonance. The simulations reveal the flow-acoustic feedback characteristics in very good agreement with results from experiment of Welsh et al. Simulations and theoretical considerations reveal that the feedback term does not reduce the stable convective flow based time step size of the flow equations.

elib-URL des Eintrags:https://elib.dlr.de/147924/
Dokumentart:Zeitschriftenbeitrag
Titel:Hydrodynamic/acoustic splitting approach with flow-acoustic feedback for universal subsonic noise computation
Autoren:
AutorenInstitution oder E-Mail-AdresseAutoren-ORCID-iDORCID Put Code
Ewert, RolandRoland.Ewert (at) dlr.deNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Kreuzinger, Johannesj.kreuzinger (at) km-turbulenz.deNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Datum:15 Juli 2021
Erschienen in:Journal of Computational Physics
Referierte Publikation:Ja
Open Access:Ja
Gold Open Access:Nein
In SCOPUS:Ja
In ISI Web of Science:Ja
DOI:10.1016/j.jcp.2021.110548
Verlag:Elsevier
ISSN:0021-9991
Status:veröffentlicht
Stichwörter:Hydrodynamic-acoustic splitting approach, Acoustic perturbation equations, Computational aeroacoustics, Incompressible Navier-Stokes equations
HGF - Forschungsbereich:Luftfahrt, Raumfahrt und Verkehr
HGF - Programm:Luftfahrt
HGF - Programmthema:Effizientes Luftfahrzeug
DLR - Schwerpunkt:Luftfahrt
DLR - Forschungsgebiet:L EV - Effizientes Luftfahrzeug
DLR - Teilgebiet (Projekt, Vorhaben):L - Digitale Technologien, L - Klima, Wetter und Umwelt, E - Windenergie
Standort: Braunschweig
Institute & Einrichtungen:Institut für Aerodynamik und Strömungstechnik > Technische Akustik
Hinterlegt von: Ewert, Dr.-Ing. Roland
Hinterlegt am:04 Jan 2022 11:45
Letzte Änderung:04 Jan 2022 11:45

Nur für Mitarbeiter des Archivs: Kontrollseite des Eintrags

Blättern
Suchen
Hilfe & Kontakt
Informationen
electronic library verwendet EPrints 3.3.12
Gestaltung Webseite und Datenbank: Copyright © Deutsches Zentrum für Luft- und Raumfahrt (DLR). Alle Rechte vorbehalten.