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Computation of Airframe Noise with the Discontinuous Galerkin Method

Bauer, Marcus (2008) Computation of Airframe Noise with the Discontinuous Galerkin Method. DAGA, Dresden, Deutschland.

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Abstract

Airframe noise is generated through turbulence passing by the edges of (rigid) bodies. Considering the low noise engines of modern airliners, it is an important noise source during the approach phase.

Item URL in elib:https://elib.dlr.de/59941/
Document Type:Conference or Workshop Item (Paper)
Title:Computation of Airframe Noise with the Discontinuous Galerkin Method
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Bauer, Marcusmarcus.bauer (at) dlr.deUNSPECIFIED
Date:March 2008
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:Discontinuous Galerkin Airframe Noise
Event Title:DAGA
Event Location:Dresden, Deutschland
Event Type:Conference
Organizer:DEGA
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:L VU - Air Traffic and Environment (old)
DLR - Research area:Aeronautics
DLR - Program:L VU - Air Traffic and Environment
DLR - Research theme (Project):L - Quiet Air Traffic (old)
Location: Braunschweig
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Technical Acoustics
Deposited By: Bauer, Marcus
Deposited On:16 Sep 2009 16:19
Last Modified:31 Jul 2019 19:25

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