Detail publikačního výsledku

Numerical Modelling of Hypersonic Flow of Spacecrafts

MAČÁK, M.; VYROUBAL, P.

Originální název

Numerical Modelling of Hypersonic Flow of Spacecrafts

Anglický název

Numerical Modelling of Hypersonic Flow of Spacecrafts

Druh

Stať ve sborníku v databázi WoS či Scopus

Originální abstrakt

Numerical simulations of rarefied gas flows are an important area in the design of aerospace vehicles. They can provide a suitable alternative to experiments, which can be often too complicated due to extreme conditions. Navier-Stokes equations, which describe continuum fluid flow, generally lose their applicability in low pressures. As a result, it is necessary to adjust these equations or use alternative models. This article studies the possibility of using a continuum numerical model for a simulation of a hypersonic flow of a reentry module. Based on the Knudsen number, it was shown that it is still possible to use Navier-Stokes equations either without any adjustments or with the addition of a slip flow boundary condition.

Anglický abstrakt

Numerical simulations of rarefied gas flows are an important area in the design of aerospace vehicles. They can provide a suitable alternative to experiments, which can be often too complicated due to extreme conditions. Navier-Stokes equations, which describe continuum fluid flow, generally lose their applicability in low pressures. As a result, it is necessary to adjust these equations or use alternative models. This article studies the possibility of using a continuum numerical model for a simulation of a hypersonic flow of a reentry module. Based on the Knudsen number, it was shown that it is still possible to use Navier-Stokes equations either without any adjustments or with the addition of a slip flow boundary condition.

Klíčová slova

rarefied flow; Knudsen number; Ansys Fluent; hypersonic flow; spacecraft

Klíčová slova v angličtině

rarefied flow; Knudsen number; Ansys Fluent; hypersonic flow; spacecraft

Autoři

MAČÁK, M.; VYROUBAL, P.

Rok RIV

2023

Vydáno

26.04.2022

Nakladatel

Brno University of Technology, Faculty of Electrical Engineering Communication

Místo

Brno

ISBN

978-80-214-6030-0

Kniha

Proceedings II of the 28 th Conference STUDENT EEICT 2022 Selected Papers

Edice

1

Strany od

238

Strany do

242

Strany počet

5

URL

https://www.eeict.cz/eeict_download/archiv/sborniky/EEICT_2022_sbornik_2_v3.pdf

Plný text v Digitální knihovně

http://hdl.handle.net/

BibTex

@inproceedings{BUT179109,
  author="Martin {Mačák} and Petr {Vyroubal}",
  title="Numerical Modelling of Hypersonic Flow of Spacecrafts",
  booktitle="Proceedings II of the 28 th Conference STUDENT EEICT 2022 Selected Papers",
  year="2022",
  series="1",
  pages="238--242",
  publisher="Brno University of Technology, Faculty of Electrical Engineering Communication",
  address="Brno",
  isbn="978-80-214-6030-0",
  url="https://www.eeict.cz/eeict_download/archiv/sborniky/EEICT_2022_sbornik_2_v3.pdf"
}