Numerical simulation of combustion in small jet engines by using segregated algorithm

Kód výsledku v IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00010669%3A_____%2F19%3AN0000019" target="_blank" >RIV/00010669:_____/19:N0000019 - isvavai.cz</a>

Výsledek na webu

<a href="https://aip.scitation.org/doi/pdf/10.1063/1.5138616?download=true" target="_blank" >https://aip.scitation.org/doi/pdf/10.1063/1.5138616?download=true</a>

DOI - Digital Object Identifier

<a href="http://dx.doi.org/10.1063/1.5138616" target="_blank" >10.1063/1.5138616</a>

Jazyk výsledku

angličtina

Název v původním jazyce

Numerical simulation of combustion in small jet engines by using segregated algorithm

Popis výsledku v původním jazyce

This paper deals with simulations of reacting flow filed in combustion chambers which are designed for application in small jet engines. A segregated algorithm is used in these simulations. This algorithm is based on the splitting of the computational domain between reacting and non-reacting part and is designed for reduction of computational time due to optimization of the computational model in non-reacting part. A module for heat transfer in a solid region has been implemented into this algorithm to allow detail study of wall cooling. Application of algorithm is shown in the case of combustion of liquid fuels in the combustion chamber which was developed at Czech Aerospace Research Centre.

Název v anglickém jazyce

Numerical simulation of combustion in small jet engines by using segregated algorithm

Popis výsledku anglicky

This paper deals with simulations of reacting flow filed in combustion chambers which are designed for application in small jet engines. A segregated algorithm is used in these simulations. This algorithm is based on the splitting of the computational domain between reacting and non-reacting part and is designed for reduction of computational time due to optimization of the computational model in non-reacting part. A module for heat transfer in a solid region has been implemented into this algorithm to allow detail study of wall cooling. Application of algorithm is shown in the case of combustion of liquid fuels in the combustion chamber which was developed at Czech Aerospace Research Centre.

Druh

D - Stať ve sborníku

CEP obor

—

OECD FORD obor

20304 - Aerospace engineering

Projekt

—

Návaznosti

I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace

Rok uplatnění

2019

Kód důvěrnosti údajů

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

Název statě ve sborníku

AIP Conference Proceedings 2189, 020004

ISBN

978-073541936-0

ISSN

0094243X

e-ISSN

1551-7616

Počet stran výsledku

4

Strana od-do

nestrankovano

Název nakladatele

American Institute of Physics Inc.

Místo vydání

Neuveden

Místo konání akce

Plzeň

Datum konání akce

11. 6. 2019

Typ akce podle státní příslušnosti

WRD - Celosvětová akce

Kód UT WoS článku

—