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The Parametric Aircraft Noise Analysis Module - status overview and recent applications

Bertsch, Lothar und Guerin, Sebastien und Looye, Gertjan und Pott-Polenske, Michael (2011) The Parametric Aircraft Noise Analysis Module - status overview and recent applications. 17th AIAA/CEAS Aeroacoustics Conference (32nd AIAA Aeroacoustics Conference), 5.-8. June 2011, Portland, Oregon, USA.

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The German Aerospace Center (DLR) is investigating aircraft noise prediction and noise reduction capabilities. The Parametric Aircraft Noise Analysis Module (PANAM) is a fast prediction tool by the DLR Institute of Aerodynamics and Flow Technology to address overall aircraft noise. It was initially developed to (1) enable comparative design studies with respect to overall aircraft ground noise and to (2) indentify promising low-noise technologies at early aircraft design stages. A brief survey of available and established fast noise prediction codes is provided in order to rank and classify PANAM among existing tools. PANAM predicts aircraft noise generated during arbitrary 3D approach and take-off flight procedures. Noise generation of an operating aircraft is determined by its design, the relative observer position, configuration settings, and operating condition along the flight path. Feasible noise analysis requires a detailed simulation of all these dominating effects. Major aircraft noise components are simulated with individual models and interactions are neglected. Each component is simulated with a separate semi-empirical and parametric noise source model. These models capture major physical effects and correlations yet allow for fast and accurate noise prediction. Sound propagation and convection effects are applied to the emitting noise source in order to transfer static emission into aircraft ground noise impact with respect to the actual flight operating conditions. Recent developments and process interfaces are presented and prediction results are compared with experimental data recorded during DLR flyover noise campaigns with an Airbus A319 (2006), a VFW-614 (2009), and a Boeing B737-700 (2010). Overall, dominating airframe and engine noise sources are adequately modeled and overall aircraft ground noise levels can sufficiently be predicted. The paper concludes with a brief overview on current code applications towards selected noise reduction technologies.

Dokumentart:Konferenzbeitrag (Paper)
Titel:The Parametric Aircraft Noise Analysis Module - status overview and recent applications
AutorenInstitution oder E-Mail-AdresseAutoren-ORCID-iD
Bertsch, Lotharlothar.bertsch@dlr.deNICHT SPEZIFIZIERT
Guerin, Sebastiensebastien.guerin@dlr.deNICHT SPEZIFIZIERT
Looye, Gertjangertjan.looye@dlr.deNICHT SPEZIFIZIERT
Pott-Polenske, Michaelmichael.pott-polenske@dlr.deNICHT SPEZIFIZIERT
Datum:8 Juni 2011
Referierte Publikation:Nein
In Open Access:Nein
In ISI Web of Science:Nein
Stichwörter:aircraft noise prediction, aircraft acoustics, low-noise technology, noise abatement procedures, low-noise aircraft design, noise source modeling
Veranstaltungstitel:17th AIAA/CEAS Aeroacoustics Conference (32nd AIAA Aeroacoustics Conference)
Veranstaltungsort:Portland, Oregon, USA
Veranstaltungsart:internationale Konferenz
Veranstaltungsdatum:5.-8. June 2011
Veranstalter :American Institute of Aeronautics and Astronautics (AIAA)
HGF - Forschungsbereich:Luftfahrt, Raumfahrt und Verkehr
HGF - Programm:keine Zuordnung
HGF - Programmthema:keine Zuordnung
DLR - Schwerpunkt:Luftfahrt
DLR - Forschungsgebiet:L - keine Zuordnung
DLR - Teilgebiet (Projekt, Vorhaben):L - keine Zuordnung (alt)
Standort: Braunschweig
Institute & Einrichtungen:Institut für Aerodynamik und Strömungstechnik
Hinterlegt von: Bertsch, Dr.-Ing. Lothar
Hinterlegt am:14 Jun 2011 08:46
Letzte Änderung:12 Dez 2013 21:18

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