About: Modeling the flow and combustion in an aircraft gas turbine combustor

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rdf:type	skos:Concept http://linked.opendata.cz/ontology/domain/vavai/Vysledek
Description	The presented paper describes a numerical investigation of the performance of a can type combustor of the aircraft gas turbine with a commercial code STAR-CD. The flow is considered as incompressible computed by Navier-Stokes equations closed by k-epsiloModeling of swirler by momentum source coding is introduced and it is shown as a good approximation of a swirler. Modeling of gas fuel combustion is compared with experiment where kerosene fuel is used. Presumed pdf model with an equilibrium scheme and Eddy Break-Up (EDBR) models of combustion are compared. It is shown that the mean values of temperature and velocity at the outlet are very close to experimental results Patterns of velocity and temperature fields on the outlet are, however different. The presented paper describes a numerical investigation of the performance of a can type combustor of the aircraft gas turbine with a commercial code STAR-CD. The flow is considered as incompressible computed by Navier-Stokes equations closed by k-epsiloModeling of swirler by momentum source coding is introduced and it is shown as a good approximation of a swirler. Modeling of gas fuel combustion is compared with experiment where kerosene fuel is used. Presumed pdf model with an equilibrium scheme and Eddy Break-Up (EDBR) models of combustion are compared. It is shown that the mean values of temperature and velocity at the outlet are very close to experimental results Patterns of velocity and temperature fields on the outlet are, however different. (en)
Title	Modeling the flow and combustion in an aircraft gas turbine combustor Modeling the flow and combustion in an aircraft gas turbine combustor (en)
skos:prefLabel	Modeling the flow and combustion in an aircraft gas turbine combustor Modeling the flow and combustion in an aircraft gas turbine combustor (en)
skos:notation	RIV/00216305:26210/00:00000025!RIV/2001/MSM/262101/N
http://linked.open.../vavai/riv/strany	163
http://linked.open...avai/riv/aktivita	Z
http://linked.open...avai/riv/aktivity	Z(MSM 262100001)
http://linked.open...iv/cisloPeriodika	3
http://linked.open...vai/riv/dodaniDat	2001
http://linked.open...aciTvurceVysledku	Forman, Matěj Jícha, Miroslav
http://linked.open.../riv/druhVysledku	J - Článek v odborném periodiku
http://linked.open...iv/duvernostUdaju	S - Úplné a pravdivé údaje nepodléhající ochraně podle zvláštních právních předpisů
http://linked.open...titaPredkladatele	Vysoké učení technické v Brně / Fakulta strojního inženýrství
http://linked.open...dnocenehoVysledku	717732
http://linked.open...ai/riv/idVysledku	RIV/00216305:26210/00:00000025
http://linked.open...riv/jazykVysledku	eng - angličtina
http://linked.open.../riv/klicovaSlova	combustion; incompressible flow,;computational fluid dynamics; combustion modeling; swirler modeling (en)
http://linked.open.../riv/klicoveSlovo	combustion combustion modeling computational fluid dynamics incompressible flow swirler modeling
http://linked.open...odStatuVydavatele	US - Spojené státy americké
http://linked.open...ontrolniKodProRIV	[3FBA99BF324E]
http://linked.open...i/riv/nazevZdroje	Inženýrská mechanika
http://linked.open...in/vavai/riv/obor	JT
http://linked.open...ichTvurcuVysledku	2 (xsd:int)
http://linked.open...cetTvurcuVysledku	5 (xsd:int)
http://linked.open...UplatneniVysledku	2000
http://linked.open...v/svazekPeriodika	7
http://linked.open...iv/tvurceVysledku	Forman, Matěj Horák, Jiří Jícha, Miroslav Kmoch, Petr Alizadeh, Sohail
http://linked.open...n/vavai/riv/zamer	http://linked.opendata.cz/resource/domain/vavai/zamer/MSM%20262100001
issn	1210-2717
number of pages	12 (xsd:int)
http://localhost/t...ganizacniJednotka	26210

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