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Fan noise due to boundary layer ingestion in novel aircraft architectures (activities within DLR project AGATA3S)

Tapken, Ulf (2018) Fan noise due to boundary layer ingestion in novel aircraft architectures (activities within DLR project AGATA3S). CEAS-ASC Workshop ‘Future Aircraft Design and Noise Impact’, 6.-7. Sep. 2018, Amsterdam, Niederlande.

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Item URL in elib:https://elib.dlr.de/126215/
Document Type:Conference or Workshop Item (Speech)
Title:Fan noise due to boundary layer ingestion in novel aircraft architectures (activities within DLR project AGATA3S)
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Tapken, Ulfulf.tapken (at) dlr.deUNSPECIFIED
Date:September 2018
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:Fan, Triebwerk, Einbettung, Flugzeug, Grenzschichteinsaugung, Akustik
Event Title:CEAS-ASC Workshop ‘Future Aircraft Design and Noise Impact’
Event Location:Amsterdam, Niederlande
Event Type:Workshop
Event Dates:6.-7. Sep. 2018
Organizer:CEAS-ASC, NLR
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 - Fan and Compressor Technologies
Location: Berlin-Charlottenburg
Institutes and Institutions:Institute of Propulsion Technology > Engine Acoustic
Institute of Propulsion Technology > Fan and Compressor
Institute of Propulsion Technology > Engine
Institute of Propulsion Technology > Engine Measurement Systems
Institute for Aerodynamics and Flow Technology > Transport Aircraft
Institute for Aerodynamics and Flow Technology > Technical Acoustics
Institute of Aeroelasticity > Aeroelastic Experiments
Institute of Structures and Design > Design and Manufacture Technologies
Deposited By: Tapken, Ulf
Deposited On:28 Jan 2019 10:25
Last Modified:31 Jul 2019 20:24

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