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Aeroacoustic Analysis of a Jet Nozzle
dc.creator | Ivanov, Toni | |
dc.creator | Fotev, Vasko | |
dc.creator | Petrović, Nebojša | |
dc.creator | Trivković, Zorana | |
dc.creator | Komarov, Dragan | |
dc.date.accessioned | 2023-03-07T19:08:37Z | |
dc.date.available | 2023-03-07T19:08:37Z | |
dc.date.issued | 2016 | |
dc.identifier.issn | 978-86-81123-82-9 | |
dc.identifier.uri | https://machinery.mas.bg.ac.rs/handle/123456789/5436 | |
dc.description.abstract | Computational fluid dynamics (CFD) based on the finite volume method were used in order to obtain the aerodynamic characteristics of a jet nozzle. After the transient CFD results were gained the Ffowcs Williams-Hawking formulation for far-field noise modeling was used for aeroacoustic computation. A grid sensitivity was done and different turbulence models were tested. The obtained results were then compared with publicly available experimental data after which a conclusion was derived. | sr |
dc.language.iso | en | sr |
dc.publisher | Military Technical Institute, Srbija | sr |
dc.relation | info:eu-repo/grantAgreement/MESTD/Technological Development (TD or TR)/35035/RS// | sr |
dc.rights | closedAccess | sr |
dc.rights.uri | https://creativecommons.org/licenses/by/4.0/ | |
dc.source | 7th International Scientific Conference od Defensive Technologies - OTEH 2016 - Proceedings | sr |
dc.subject | computational aeroacoustics | sr |
dc.subject | computational fluid dynamics | sr |
dc.subject | jet noise | sr |
dc.title | Aeroacoustic Analysis of a Jet Nozzle | sr |
dc.type | conferenceObject | sr |
dc.rights.license | BY | sr |
dc.citation.epage | 28 | |
dc.citation.rank | M33 | |
dc.citation.spage | 24 | |
dc.identifier.rcub | https://hdl.handle.net/21.15107/rcub_machinery_5436 | |
dc.type.version | publishedVersion | sr |