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Acoustic performance of bias flow liners in gas turbine combustors

Lahiri, Claus (2014) Acoustic performance of bias flow liners in gas turbine combustors. DLR-Forschungsbericht. DLR-FB 2014-39, 364 S. Deutsches Zentrum für Luft- und Raumfahrt.

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Item URL in elib:https://elib.dlr.de/93931/
Document Type:Monograph (DLR-Forschungsbericht)
Additional Information:Zugl.: Berlin, Technische Universität, Diss., 2014 (urn:nbn:de:kobv:83-opus4-59486)
Title:Acoustic performance of bias flow liners in gas turbine combustors
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Lahiri, ClausAT-TRAUNSPECIFIED
Date:December 2014
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Number of Pages:364
Publisher:Deutsches Zentrum für Luft- und Raumfahrt
Series Name:DLR Forschungsbericht
ISSN:1434-8454
Status:Published
Keywords:Thermoakustik, Strömungsakustik, durchströmte Liner, Schalldämpfung, Impedanz, thermoacoustics, aeroacoustics, bias flow liner, sound absorption, impedance
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 - Combusion Chamber Technologies (old), E - Gas Turbine (old)
Location: other
Institutes and Institutions:Institute of Propulsion Technology > Engine Acoustic
Deposited By: Lahiri, Claus
Deposited On:07 Jan 2015 14:47
Last Modified:07 Jan 2015 14:47

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