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Fan tone simulation from a UHBR engine with drooped nacelle inlet at Approach condition and an angle of attack of 10°

Holewa, Axel and Guerin, Sebastien (2017) Fan tone simulation from a UHBR engine with drooped nacelle inlet at Approach condition and an angle of attack of 10°. 21st Workshop of the Aeroacoustics Specialists Committee of the CEAS, Dublin, Ireland.

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Item URL in elib:https://elib.dlr.de/117977/
Document Type:Conference or Workshop Item (Speech)
Title:Fan tone simulation from a UHBR engine with drooped nacelle inlet at Approach condition and an angle of attack of 10°
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Holewa, AxelAxel.Holewa (at) dlr.deUNSPECIFIED
Guerin, SebastienSebastien.Guerin (at) dlr.deUNSPECIFIED
Date:September 2017
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:acoustics, inflow distortion, mode scattering
Event Title:21st Workshop of the Aeroacoustics Specialists Committee of the CEAS
Event Location:Dublin, Ireland
Event Type:Workshop
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 - Virtual Engine and Validation methods
Location: Berlin-Charlottenburg
Institutes and Institutions:Institute of Propulsion Technology > Engine Acoustic
Deposited By: Guerin, Sebastien
Deposited On:09 Jan 2018 12:03
Last Modified:09 Jan 2018 12:03

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