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dc.creatorIvanov, Toni
dc.creatorFotev, Vasko
dc.creatorPetrović, Nebojša
dc.creatorTrivković, Zorana
dc.creatorKomarov, Dragan
dc.date.accessioned2023-03-07T19:08:37Z
dc.date.available2023-03-07T19:08:37Z
dc.date.issued2016
dc.identifier.issn978-86-81123-82-9
dc.identifier.urihttps://machinery.mas.bg.ac.rs/handle/123456789/5436
dc.description.abstractComputational 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.isoensr
dc.publisherMilitary Technical Institute, Srbijasr
dc.relationinfo:eu-repo/grantAgreement/MESTD/Technological Development (TD or TR)/35035/RS//sr
dc.rightsclosedAccesssr
dc.rights.urihttps://creativecommons.org/licenses/by/4.0/
dc.source7th International Scientific Conference od Defensive Technologies - OTEH 2016 - Proceedingssr
dc.subjectcomputational aeroacousticssr
dc.subjectcomputational fluid dynamicssr
dc.subjectjet noisesr
dc.titleAeroacoustic Analysis of a Jet Nozzlesr
dc.typeconferenceObjectsr
dc.rights.licenseBYsr
dc.citation.epage28
dc.citation.rankM33
dc.citation.spage24
dc.identifier.rcubhttps://hdl.handle.net/21.15107/rcub_machinery_5436
dc.type.versionpublishedVersionsr


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Приказ основних података о документу