elib
DLR-Header
DLR-Logo -> http://www.dlr.de
DLR Portal Home | Imprint | Privacy Policy | Contact | Deutsch
Fontsize: [-] Text [+]

Future Applications for Scientific Aircraft Noise Simulation Tools

Bertsch, Lothar (2015) Future Applications for Scientific Aircraft Noise Simulation Tools. 3. Workshop „Strömungsschall in Luftfahrt, Fahrzeug- und Anlagentechnik“, 12.- 13. Nov. 2015, Braunschweig, Deutschland.

Full text not available from this repository.

Official URL: http://www.dglr.de/fileadmin/inhalte/dglr/fb/q2/workshop-q23-braunschweig-2015/Agenda.pd

Abstract

Aircraft noise is probably the most dominating contribution to community noise annoyance. The most effective way to reduce aircraft noise is 1) the reduction at the source and 2) the optimization of the actual flight operation of the aircraft. In order to identify promising concepts for such a noise reduction and to evaluate the impact on a system level, so-called scientific noise prediction tools have been developed. The overall aircraft noise is hereby described in a componential and parametric way, i.e. the major noise contributors are modelled individually under consideration of relevant parameters. The selected parameters reflect the influence of geometrical details and operational conditions on each modeled noise source and ultimately on the overall vehicle noise. The underlying models yield one-third-octave band SPL spectra for each emission angle. For typical applications this data is translated into time-level-histories on the ground and noise footprints. Obviously, much more information can be derived from the standard output, i.e. the spectral and directional SPL data. Access to this output data is very promising for new and unconventional application of the scientific aircraft noise simulation tools. Three exemplary applications are presented and discussed here. First example: noise-to-design activities. Parametric noise sources models of the scientific tools translate geometrical and operational input into noise levels. It seems promising to reverse this process, i.e. starting with some selected noise goals and then tracing it back to a required modification to the underlying geometry or flight operation.

Item URL in elib:https://elib.dlr.de/98535/
Document Type:Conference or Workshop Item (Speech)
Additional Information:„Q2.3 Strömungsakustik und Fluglärm“ der Deutschen Gesellschaft für Luft- und Raumfahrt DGLR und „Strömungsakustik“ der Deutschen Gesellschaft für Akustik DEGA, unterstützt durch das Fluglärmnetzwerk „X-Noise EV“
Title:Future Applications for Scientific Aircraft Noise Simulation Tools
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Bertsch, Lotharlothar.bertsch (at) dlr.deUNSPECIFIED
Date:2015
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Series Name:Beiträge online
Status:Published
Keywords:Noise Prediction, Aircraft Design, Auralization, PANAM
Event Title:3. Workshop „Strömungsschall in Luftfahrt, Fahrzeug- und Anlagentechnik“
Event Location:Braunschweig, Deutschland
Event Type:Workshop
Event Dates:12.- 13. Nov. 2015
Organizer:Deutschen Gesellschaft für Luft- und Raumfahrt (DGLR) und Deutschen Gesellschaft für Akustik (DEGA)
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:rotorcraft
DLR - Research area:Aeronautics
DLR - Program:L RR - Rotorcraft Research
DLR - Research theme (Project):L - The Virtual Aerodynamic Rotorcraft
Location: Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Helicopters
Deposited By: Micknaus, Ilka
Deposited On:27 Nov 2015 16:09
Last Modified:10 May 2016 23:32

Repository Staff Only: item control page

Browse
Search
Help & Contact
Information
electronic library is running on EPrints 3.3.12
Copyright © 2008-2017 German Aerospace Center (DLR). All rights reserved.