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Nonlinear three-port measurements for the determination of high-level excitation effects on the acoustic properties of perforates
KTH, School of Engineering Sciences (SCI), Engineering Mechanics, Fluid Mechanics and Engineering Acoustics. (The Marcus Wallenberg Laboratory of Sound and Vibration Research)ORCID iD: 0000-0003-2194-082x
KTH, School of Engineering Sciences (SCI), Engineering Mechanics, Fluid Mechanics and Engineering Acoustics. (The Marcus Wallenberg Laboratory of Sound and Vibration Research)ORCID iD: 0000-0002-8474-8563
KTH, School of Engineering Sciences (SCI), Engineering Mechanics, Fluid Mechanics and Engineering Acoustics.ORCID iD: 0000-0003-4103-0129
2022 (English)In: Proceeding of the 28th AIAA/CEAS Aeroacoustics 2022 Conference / [ed] AIAA/CEAS, American Institute of Aeronautics and Astronautics (AIAA) , 2022Conference paper, Published paper (Refereed)
Abstract [en]

The effect of high-level excitation on the acoustic properties of perforates, and formulation of the non-linear part of the impedance is under scientific discussion. Analytical models including the non-linear properties, as well as various experimental studies give varying results for the acoustic impedance. This paper aims to provide detailed results obtained under high-level excitation with different acoustic wave incidence and flow configurations. Contrary to the well-established two-port configuration, here, a three-port measurement technique is used to observe the acoustic impedance of the perforated plate using excitation from the three different directions. Plane wave propagation is considered and physical quantities such as in-hole particle velocity, which is calculated at the perforate sample, are used as the controlling parameters. This paper is an attempt to study the effect of high-level excitation on the acoustic behavior of the perforates with grazing and normal acoustic incidence. Moreover, the non-linear behavior of the perforate determined in presence of an external grazing flow is also discussed.

Place, publisher, year, edition, pages
American Institute of Aeronautics and Astronautics (AIAA) , 2022.
Keywords [en]
Acoustic Properties, Strouhal Numbers, Vena Contracta, Flow Velocity, Mach Number
National Category
Fluid Mechanics and Acoustics
Research subject
Aerospace Engineering
Identifiers
URN: urn:nbn:se:kth:diva-319645DOI: 10.2514/6.2022-2928Scopus ID: 2-s2.0-85135086193OAI: oai:DiVA.org:kth-319645DiVA, id: diva2:1701119
Conference
28th AIAA/CEAS Aeroacoustics 2022 Conference
Note

QC 20221005

Available from: 2022-10-04 Created: 2022-10-04 Last updated: 2022-10-06Bibliographically 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, S. A.Bodén, HansBoij, Susann

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