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Reduction of inertial end correction of perforated plates due to secondary high amplitude stimuli

Burgmayer, Ralf and Bake, Friedrich and Enghardt, Lars (2022) Reduction of inertial end correction of perforated plates due to secondary high amplitude stimuli. JASA Express Letters, 2 (4), 042801. Acoustical Society of America. doi: 10.1121/10.0009920. ISSN 2691-1191.

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Official URL: https://asa.scitation.org/doi/10.1121/10.0009920

Abstract

The decrease in reactance of perforated plates at high sound pressure amplitudes is of interest for the design of Helmholtz resonator liners. It is associated with the loss of end correction due to flow separation at the orifices. In practical applications, complex acoustic signals impinge on perforations. The loss of end correction due to multiple stimuli of unrelated frequency and phase has not been considered yet. This study assesses and presents an empirical approximation for the reduction of end correction of perforated plates at primary frequencies when flow separation is induced by an additional secondary unrelated high amplitude stimulus.

Item URL in elib:https://elib.dlr.de/186979/
Document Type:Article
Title:Reduction of inertial end correction of perforated plates due to secondary high amplitude stimuli
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Burgmayer, RalfUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Bake, FriedrichUNSPECIFIEDhttps://orcid.org/0000-0002-3235-428XUNSPECIFIED
Enghardt, LarsUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Date:1 April 2022
Journal or Publication Title:JASA Express Letters
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:Yes
Volume:2
DOI:10.1121/10.0009920
Page Range:042801
Publisher:Acoustical Society of America
ISSN:2691-1191
Status:Published
Keywords:Impedanz, perforierte Platte, Dimensionsanalyse, empirische Modellierung, akustische Messverfahren
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: Burgmayer, Ralf
Deposited On:27 Jun 2022 08:19
Last Modified:21 Jan 2025 12:41

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