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Acoustic investigation of a specially manufactured non-locally reacting liner for aircraft applications

Busse, St. and Richter, Ch. and Nitsch, S. and Thiele, F. and Bake, F. and Enghardt, L. and Kückens, C. and Müller, U. (2010) Acoustic investigation of a specially manufactured non-locally reacting liner for aircraft applications. In: Proceedings 16th AIAA/CEAS Aeroacoustics Conference, Vol. 15 (Nr. 5). 16th AIAA/CEAS Aeroacoustics Conference (31st AIAA Aeroacoustics Conference), 07.-09. Juni 2010, Stockholm, Schweden. ISBN 978-1-60086-744-6 .

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Document Type:Conference or Workshop Item (Paper)
Title:Acoustic investigation of a specially manufactured non-locally reacting liner for aircraft applications
Authors:
AuthorsInstitution or Email of Authors
Busse, St.Institut für Strömungsmechanik und Technische Akustik
Richter, Ch.Institut für Strömungsmechanik und Technische Akustik, TU Berlin
Nitsch, S.Institut für Strömungsmechanik und Technische Akustik, TU Berlin
Thiele, F.Institut für Strömungsmechanik und Technische Akustik, TU Berlin
Bake, F.UNSPECIFIED
Enghardt, L.UNSPECIFIED
Kückens, C.PFW Aerospace AG, Speyer
Müller, U.Melicon GmbH
Date:2010
Journal or Publication Title:Proceedings 16th AIAA/CEAS Aeroacoustics Conference
Refereed publication:Yes
In ISI Web of Science:No
Volume:Vol. 15
ISBN:978-1-60086-744-6
Status:Published
Keywords:acoustic, aircraft applications
Event Title:16th AIAA/CEAS Aeroacoustics Conference (31st AIAA Aeroacoustics Conference)
Event Location:Stockholm, Schweden
Event Type:international Conference
Event Dates:07.-09. Juni 2010
Organizer:AIAA
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Propulsion Systems
DLR - Research area:Aeronautics
DLR - Program:L ER - Engine Research
DLR - Research theme (Project):L - Combustion Chamber Technologies
Location: Berlin-Adlershof
Institutes and Institutions:Institute of Propulsion Technology > Engine Acoustic
Deposited By: Balbir Kaur
Deposited On:03 Feb 2011 09:34
Last Modified:09 Oct 2012 15:52

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