Detail publikace

Temperature profile analysis in supersonic flow in the experimental chamber

ŠABACKÁ, P. MAXA, J. VYROUBAL, P.

Originální název

Temperature profile analysis in supersonic flow in the experimental chamber

Typ

článek ve sborníku mimo WoS a Scopus

Jazyk

angličtina

Originální abstrakt

This article deals with the preparation of the experimental chamber on which, among other things, stagnation and static temperature will be measured. The results obtained from the measurements will be compared with the results of mathematical - physics analyzes of the Ansys Fluent system. Analyzes of the expected stagnation temperatures at the tip of the probes were performed with respect to the course of the Mach number from the aperture.

Klíčová slova

ESEM, Ansys,, Static Pressure, Total Pressure, Dynamic Pressure, Recovery Factor, Differentially Pumped Chamber

Autoři

ŠABACKÁ, P.; MAXA, J.; VYROUBAL, P.

Vydáno

7. 9. 2020

ISBN

978-80-214-5109-4

Kniha

21st ABAF

Strany od

119

Strany do

122

Strany počet

4

BibTex

@inproceedings{BUT165667,
  author="Pavla {Šabacká} and Jiří {Maxa} and Petr {Vyroubal}",
  title="Temperature profile analysis in supersonic flow in the experimental chamber",
  booktitle="21st ABAF",
  year="2020",
  pages="119--122",
  isbn="978-80-214-5109-4"
}