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Three-port measurements for determination of the effect of flow on the acoustic properties of perforates
KTH, School of Engineering Sciences (SCI), Engineering Mechanics, Fluid Mechanics and Engineering Acoustics, Marcus Wallenberg Laboratory MWL.ORCID iD: 0000-0003-2194-082X
KTH, School of Engineering Sciences (SCI), Engineering Mechanics, Fluid Mechanics and Engineering Acoustics, Marcus Wallenberg Laboratory MWL.ORCID iD: 0000-0002-8474-8563
KTH, School of Engineering Sciences (SCI), Engineering Mechanics, Fluid Mechanics and Engineering Acoustics, Marcus Wallenberg Laboratory MWL.ORCID iD: 0000-0003-4103-0129
Université du Mans, Le Mans, France.
2021 (English)In: AIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2021, American Institute of Aeronautics and Astronautics Inc, AIAA , 2021Conference paper, Published paper (Refereed)
Abstract [en]

A major discussion in the scientific community is the effect of the acoustic propagation direction being relative to the mean flow direction on the acoustic boundary condition posed by perforated liners. The reason being that the results from liner-impedance-eduction measurements show acoustic propagation upstream or downstream to the flow direction giving different resulting acoustical impedances. This paper contributes to this continuing effort to gain confidence in results obtained under different acoustical excitation and flow configurations. Instead of a traditional two-port configuration, by placing a perforate sample in a T-junction, this paper presents a three-port measurement technique. The transfer impedance of the perforate is determined under grazing as well as under normal incidence. Moreover, to study the effect of acoustic incidence relative to the flow directions, transfer impedance is also determined under the presence of grazing flow. A comparison of the measurement results with existing analytical and semi empirical models is also presented. An attempt to determine the nature of the transfer impedance under normal acoustic incidence is carried out and an analogous behavior between an empty T-junction and the perforated sample is proposed. 

Place, publisher, year, edition, pages
American Institute of Aeronautics and Astronautics Inc, AIAA , 2021.
Keywords [en]
Acoustic impedance measurement, Aeroacoustics, Acoustic propagation, Acoustics property, Community IS, Mean-flow directions, Propagation direction, Scientific community, T junctions, Three-port measurement, Transfer impedance, Acoustic impedance
National Category
Fluid Mechanics and Acoustics
Identifiers
URN: urn:nbn:se:kth:diva-316269DOI: 10.2514/6.2021-2269Scopus ID: 2-s2.0-85126804112OAI: oai:DiVA.org:kth-316269DiVA, id: diva2:1688864
Conference
AIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2021, 2 August 2021 through 6 August 2021
Note

Part of book: 978-1-62410-610-1

QC 20221005

Available from: 2022-08-19 Created: 2022-08-19 Last updated: 2024-01-10Bibliographically approved
In thesis
1. Experimental Investigation of the Acoustic Properties of Perforate using Acoustic Three-Ports
Open this publication in new window or tab >>Experimental Investigation of the Acoustic Properties of Perforate using Acoustic Three-Ports
2022 (English)Licentiate thesis, comprehensive summary (Other academic)
Abstract [en]

This thesis discusses the aero-acoustic characterisation of a perforate sample using a three-port technique. A rectangular T-junction with a flush mounted perforated sample at the intersection form the acoustical three-port. Under acoustic excitation from three different directions a direct method of impedance determination is incorporated to experimentally determine the passive acoustic properties of the perforate. The three-port scattering matrix and the normalised transfer impedance are calculated in the presence of grazing flow and for high-level excitation and the behaviour of these characteristics is studied. Validation of the determined results in the linear range is carried out by comparing it with existing models. Moreover, based on the experimental results for low grazing flow velocities the dependence of the real part of the transfer impedance on the grazing flow parameters as well as dimensionless numbers is described, and a semi-empirical model quantifying the behaviour is proposed.

Furthermore, the thesis explains some experimental errors pertaining to standing wave patterns and operating conditions, and corrections are suggested to reduce the errors.

Place, publisher, year, edition, pages
Stockholm: KTH Royal Institute of Technology, 2022. p. 49
Series
TRITA-SCI-FOU ; 2022:52
Keywords
Duct Acoustics, Acoustical Three-port, Perforated plate, Transfer Impedance, Scattering Matrix, Grazing Flow, High-level Excitation, Non-linear effects, Flow-Acoustic Interaction, Rectangular T-Junction
National Category
Fluid Mechanics and Acoustics
Research subject
Vehicle and Maritime Engineering
Identifiers
urn:nbn:se:kth:diva-319725 (URN)978-91-8040-381-8 (ISBN)
Presentation
2022-10-28, https://kth-se.zoom.us/j/64629745239, D3, Lindstedtsvägen 9, KTH, Stockholm, 10:00 (English)
Opponent
Supervisors
Funder
EU, Horizon 2020, 813367
Note

QC 221007

Available from: 2022-10-07 Created: 2022-10-06 Last updated: 2022-10-26Bibliographically approved

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Shah, ShailBodén, HansBoij, Susann

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