Tuning Of The Ansys Fluent System For The Analysis Of Supersonic Flight Of A 762x39 Caliber Projectile
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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.
Document typePeer reviewed
Document versionFinal PDF
SourceProceedings I of the 27st Conference STUDENT EEICT 2021: General papers. s. 15-19. ISBN 978-80-214-5942-7
- Student EEICT 2021