Original title: Analyses Of Static Pressure In Oblique Shockwave On The Probe Tip
Authors: Jenáček, Jakub
Document type: Papers
Language: cze
Publisher: Vysoké učení technické v Brně, Fakulta elektrotechniky a komunikačních technologií
Abstract: This article deals with the debugging analyses of Ansys Fluent for supersonic flowanalyzes. It is about analyzes on which the debugging of Ansys Fluent was made for analyzes ofsupersonic flow circumfluent the tip of the probe compared with the theory of isoentropic onedimensionalflow as a basic step for further analyzes in low pressures. The results shown in this paperwill further serve as a basis for experimental measuring of given problem.
Keywords: Ansys Fluent; Differentially pumped chamber; Pitot’s tube; 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/11012/200723

Permalink: http://www.nusl.cz/ntk/nusl-447768


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