Comparison of Turbulence Models in OpenFOAM for 3D Simulation of Gas Flow in Solid Propellant Rocket Motor

Result code in IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F60162694%3AG43__%2F16%3A00535396" target="_blank" >RIV/60162694:G43__/16:00535396 - isvavai.cz</a>

Result on the web

<a href="http://aimt.unob.cz/vol11is2.htm" target="_blank" >http://aimt.unob.cz/vol11is2.htm</a>

DOI - Digital Object Identifier

<a href="http://dx.doi.org/10.3849/aimt01131" target="_blank" >10.3849/aimt01131</a>

Result language

angličtina

Original language name

Comparison of Turbulence Models in OpenFOAM for 3D Simulation of Gas Flow in Solid Propellant Rocket Motor

Original language description

The goal of this paper is comparison of various mathematical models simulating the turbulence flow in a solid propellant rocket engine. for comparison, the most frequently used models were chosen for simulation of flow in the S-5 rocket engine. For this type of engine the experimental data are available allowing comparison of simulation results with reality. The LES Smagorinsky model provided the best results, while type RANS models appeared to be less suitable for this task.

Czech name

—

Czech description

—

Type

J_SC - Article in a specialist periodical, which is included in the SCOPUS database

CEP classification

—

OECD FORD branch

20303 - Thermodynamics

Project

—

Continuities

I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace

Publication year

2016

Confidentiality

S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Name of the periodical

Advances in Military Technology

ISSN

1802-2308

e-ISSN

2533-4123

Volume of the periodical

11

Issue of the periodical within the volume

2/2016

Country of publishing house

CZ - CZECH REPUBLIC

Number of pages

13

Pages from-to

239-251

UT code for WoS article

—

EID of the result in the Scopus database

2-s2.0-85011005506