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dc.contributor.authorDamani, S
dc.contributor.authorTotten, E
dc.contributor.authorDavies, L
dc.contributor.authorAlexander, WN
dc.contributor.authorDevenport, WJ
dc.contributor.authorPearce, BP
dc.contributor.authorShelley, SR
dc.contributor.authorStarkey, TA
dc.contributor.authorHibbins, AP
dc.contributor.authorSambles, JR
dc.date.accessioned2020-07-10T08:28:02Z
dc.date.issued2020-06-08
dc.description.abstractThis experiment demonstrated the generation of trapped acoustic surface waves excited by a turbulent flow source through the coupling of pressure fluctuations at the interface between an acoustic metamaterial and a flow environment. The turbulent flow, which behaves as a stochastic pressure source, was produced using a fully developed turbulent wall jet. The plate in the wall jet was perforated with a single cavity. On the flow-side it was capped by a Kevlar weave to ensure the cavity did not significantly disturb the flow, whilst on the adjacent side the cavity was open to the quiescent (static) environment. The through-cavity opening, on the quiescent side, was flush with an acoustic metasurface waveguide, which, through evanescent diffractive coupling of the pressure field, produced an acoustic surface mode. This acoustic mode was trapped at the plate surface, with its mode dispersion determined by the surface geometry. The results of two different metasurface geometries are discussed; (1) a slotted cavity array, and (2) a meander connected cavity array, each demonstrating a different trapped surface wave dispersion behavior. Fourier transform and correlation analyses of spatially-resolved temporal acoustic signals, measured close to the metamaterial surface, were used to construct the frequency and wave vector-dependent acoustic mode dispersion. Results demonstrated the flow can indeed be used to excite these acoustic modes and that their mode dispersion can be tailored towards realizing novel control of turbulent flow through acoustic-flow interactionsen_GB
dc.description.sponsorshipDefence Science and Technology Laboratory (DSTL)en_GB
dc.identifier.citationAIAA Aviation 2020 Forum, 15-19 June 2020, article AIAA 2020-2587en_GB
dc.identifier.doi10.2514/6.2020-2587
dc.identifier.grantnumberMC_PC_15047en_GB
dc.identifier.urihttp://hdl.handle.net/10871/121887
dc.language.isoenen_GB
dc.publisherAmerican Institute of Aeronautics and Astronautics (AIAA)en_GB
dc.rights© 2020 American Institute of Aeronautics and Astronauticsen_GB
dc.subjectAeroacousticsen_GB
dc.titleExcitation of airborne acoustic surface modes driven by a turbulent flowen_GB
dc.typeConference proceedingsen_GB
dc.date.available2020-07-10T08:28:02Z
dc.identifier.isbn978-1-62410-598-2
dc.descriptionThis is the author accepted manuscript. The final version is available from AIAA via the DOI in this recorden_GB
dc.rights.urihttp://www.rioxx.net/licenses/all-rights-reserveden_GB
dcterms.dateAccepted2020-06-08
exeter.funder::Defence Science and Technology Laboratory (DSTL)en_GB
exeter.funder::Defence Science and Technology Laboratory (DSTL)en_GB
rioxxterms.versionAMen_GB
rioxxterms.licenseref.startdate2020-06-08
rioxxterms.typeConference Paper/Proceeding/Abstracten_GB
refterms.dateFCD2020-07-10T08:19:21Z
refterms.versionFCDAM
refterms.dateFOA2020-07-10T08:28:07Z
refterms.panelBen_GB


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