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Unsteady flow, turbulence and acoustic measurements on the counterrotating DLR turbo fan stage CIRSPMULTI, with and witout inlet distuortions

Meyer, Robert and Tapken, Ulf and Klähn, Lukas and Behn, Maximilian and Lengyel-Kampmann, Timea (2024) Unsteady flow, turbulence and acoustic measurements on the counterrotating DLR turbo fan stage CIRSPMULTI, with and witout inlet distuortions. In: 69th ASME Turbo Expo 2024: Turbomachinery Technical Conference and Exposition, GT 2024, GT2024 (124839). ASME Turbo Expo 2024. ASME Turbo Expo 2024, 2024-06-24 - 2024-06-28, London, UK. doi: 10.1115/GT2024-124839. ISBN 978-079188807-0.

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Official URL: https://asme-turboexpo.secure-platform.com/a/solicitations/223/sessiongallery/15256/application/124839

Abstract

Extensive aerodynamic and acoustic measurements were carried out on a counter-rotating turbofan (CRISP) stage under the influence of inlet distortions that are representative of the boundary layer ingestion of an engine embedded in the aircraft fuselage. The unsteady flow field was measured and analyzed using hot-wire anemometry upstream, between and downstream of the rotors, both with and without inlet distortions. Acoustic measurements were carried out using extensive microphone arrays on the intake and exhaust sides of the fan. This article presents exemplary measurement results, which show the significant effect of inlet distortions on turbulence and fan sound excitation.

Item URL in elib:https://elib.dlr.de/205605/
Document Type:Conference or Workshop Item (Speech)
Title:Unsteady flow, turbulence and acoustic measurements on the counterrotating DLR turbo fan stage CIRSPMULTI, with and witout inlet distuortions
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Meyer, RobertUNSPECIFIEDhttps://orcid.org/0009-0005-5241-1818165329955
Tapken, UlfUNSPECIFIEDhttps://orcid.org/0000-0002-0870-1253165329957
Klähn, LukasUNSPECIFIEDhttps://orcid.org/0000-0002-1425-4453165329958
Behn, MaximilianUNSPECIFIEDhttps://orcid.org/0000-0001-8478-8269UNSPECIFIED
Lengyel-Kampmann, TimeaUNSPECIFIEDhttps://orcid.org/0009-0002-3320-7019UNSPECIFIED
Date:24 June 2024
Journal or Publication Title:69th ASME Turbo Expo 2024: Turbomachinery Technical Conference and Exposition, GT 2024
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:Yes
Volume:GT2024
DOI:10.1115/GT2024-124839
Publisher:ASME Turbo Expo 2024
Series Name:GT2024-124839;
ISBN:978-079188807-0
Status:Published
Keywords:Engine acoustics; inlet distortion; boundary layer ingestion, broadband noise, turbulence measurement, unsteady flow, fan noise, tonal noise
Event Title:ASME Turbo Expo 2024
Event Location:London, UK
Event Type:international Conference
Event Start Date:24 June 2024
Event End Date:28 June 2024
Organizer:ASME Turbo EXPO 2024
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Clean Propulsion
DLR - Research area:Aeronautics
DLR - Program:L CP - Clean Propulsion
DLR - Research theme (Project):L - Future Engines and Engine Integration
Location: Berlin-Charlottenburg
Institutes and Institutions:Institute of Propulsion Technology > Engine Acoustic
Deposited By: Meyer, Dr.-Ing. Robert
Deposited On:12 Aug 2024 10:51
Last Modified:14 Nov 2024 13:53

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