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Application of an Aircraft Design-To-Noise Simulation Process

Bertsch, Lothar and Heinze, Wolfgang and Lummer, Markus (2014) Application of an Aircraft Design-To-Noise Simulation Process. American Institute of Aeronautics and Astronautics. 20th AIAA/CEAS Aeroacoustics Conference, 16. - 20. June 2014, Atlanta, Georgia, USA. doi: 10.2514/6.2014-2169.

Full text not available from this repository.

Official URL: http://arc.aiaa.org | DOI: 10.2514/6.2014-2169


System noise has been integrated as an additional design objective within conceptual aircraft design. The DLR system noise prediction tool PANAM accounts for individual noise sources depending on their geometry and operating conditions. PANAM is integrated into the existing aircraft design framework PrADO from the Technical University of Braunschweig in order to realize a design-to-noise simulation process. In addition, a ray-tracing tool from DLR, SHADOW, is incorporated into the simulation framework in order to account for structural engine noise shielding. The overall simulation process is then applied to identify promising low-noise aircraft concepts. The presented application aims at fan noise reduction through shielding. For the selected reference aircraft, the fan is a major noise source during both landing and takeoff. It is demonstrated, that the aircraft designers influence on the environmental vehicle characteristics is significant at the conceptual design phase. Usually, a trade-off between extensive engine noise shielding and economical flight performance is inevitable. The new design-to-noise process is well suitable to assess all four measures of ICAOs balanced approach.

Item URL in elib:https://elib.dlr.de/85455/
Document Type:Conference or Workshop Item (Speech)
Additional Information:AIAA 2014-2169, 14th AIAA Aviation Technology, Integration, and Operations Conference, DOI: 10.2514/6.2014-2169
Title:Application of an Aircraft Design-To-Noise Simulation Process
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Bertsch, LotharUNSPECIFIEDhttps://orcid.org/0000-0003-2780-2858UNSPECIFIED
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In ISI Web of Science:No
Page Range:pp. 1-17
Publisher:American Institute of Aeronautics and Astronautics
Series Name:Conference Proceedings online
Keywords:Aircraft noise prediction, aircraft design, design-to-noise
Event Title:20th AIAA/CEAS Aeroacoustics Conference
Event Location:Atlanta, Georgia, USA
Event Type:international Conference
Event Dates:16. - 20. June 2014
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 (old)
Location: Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Helicopters
Deposited By: Micknaus, Ilka
Deposited On:18 Jul 2014 10:25
Last Modified:11 Jul 2023 15:06

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