Original title: Tuning Of The Ansys Fluent System For The Analysis Of Supersonic Flight Of A 762x39 Caliber Projectile
Authors: Maxa, Filip
Document type: Papers
Language: cze
Publisher: Vysoké učení technické v Brně, Fakulta elektrotechniky a komunikačních technologií
Abstract: This 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.
Keywords: 7,62 x 39; ANSYS Fluent; Ballistic; Shockwave
Host item entry: Proceedings I of the 27st Conference STUDENT EEICT 2021: General papers, ISBN 978-80-214-5942-7

Institution: Brno University of Technology (web)
Document availability information: Fulltext is available in the Brno University of Technology Digital Library.
Original record: http://hdl.handle.net/11012/200734

Permalink: http://www.nusl.cz/ntk/nusl-447779


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