Tuning Of The Ansys Fluent System For The Analysis Of Supersonic Flight Of A 762x39 Caliber Projectile

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but.event.date27.04.2021cs
but.event.titleSTUDENT EEICT 2021cs
dc.contributor.authorMaxa, Filip
dc.date.accessioned2021-07-21T07:06:56Z
dc.date.available2021-07-21T07:06:56Z
dc.date.issued2021cs
dc.description.abstractThis article deals with the circumflow of the probe tips in external ballistic and with thecomparison of results obtained using Ansys Fluent system with the results obtained from experimentof the given projectile according to the cited literature. Conclusions obtained will serve as abasis for further research in given research area.en
dc.formattextcs
dc.format.extent15-19cs
dc.format.mimetypeapplication/pdfen
dc.identifier.citationProceedings I of the 27st Conference STUDENT EEICT 2021: General papers. s. 15-19. ISBN 978-80-214-5942-7cs
dc.identifier.isbn978-80-214-5942-7
dc.identifier.urihttp://hdl.handle.net/11012/200734
dc.language.isocscs
dc.publisherVysoké učení technické v Brně, Fakulta elektrotechniky a komunikačních technologiícs
dc.relation.ispartofProceedings I of the 27st Conference STUDENT EEICT 2021: General papersen
dc.relation.urihttps://conf.feec.vutbr.cz/eeict/index/pages/view/ke_stazenics
dc.rights© Vysoké učení technické v Brně, Fakulta elektrotechniky a komunikačních technologiícs
dc.rights.accessopenAccessen
dc.subjectShockwaveen
dc.subjectANSYS Fluenten
dc.subjectBallisticen
dc.subject7,62 x 39en
dc.titleTuning Of The Ansys Fluent System For The Analysis Of Supersonic Flight Of A 762x39 Caliber Projectileen
dc.type.driverconferenceObjecten
dc.type.statusPeer-revieweden
dc.type.versionpublishedVersionen
eprints.affiliatedInstitution.departmentFakulta elektrotechniky a komunikačních technologiícs
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