FINITE DIFFERENCE METHOD FOR CALCULATING OF THE GAS FLOW IN A SUBSONIC GAS EJECTOR

Describe analysis of eddy viscosity actual mathematical models for numerical simulation a reversal gas flow in subsonic gas ejector. Considered advantages and disadvantages each of it. Proposed use method of finite elements for provides viscous gas flow calculation of gas ejectors.

Bibliographic Details
Main Authors:	Kostjantin Kapitanchuk, Pavlo Grekov, Mykola Bohdanov, Galina Nikitina
Format:	Article
Language:	English
Published:	National Aviation University 2015-12-01
Series:	Vìsnik Nacìonalʹnogo Avìacìjnogo Unìversitetu
Subjects:	calculation finite elements method gas ejector gas turbine engine navier-stokes combined equations subsonic gas flow
Online Access:	http://jrnl.nau.edu.ua/index.php/visnik/article/view/9855

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spelling	doaj-1b3a1f8ad23444eca56c0120ed2cce952020-11-25T03:18:51ZengNational Aviation UniversityVìsnik Nacìonalʹnogo Avìacìjnogo Unìversitetu1813-11662306-14722015-12-01654556010.18372/2306-1472.65.98559527FINITE DIFFERENCE METHOD FOR CALCULATING OF THE GAS FLOW IN A SUBSONIC GAS EJECTORKostjantin Kapitanchuk0Pavlo Grekov1Mykola Bohdanov2Galina Nikitina3National Aviation University, Kiev, UkraineNational Aviation University, Kiev, UkraineNational Aviation University, Kiev, UkraineNational Aviation University, Kiev, UkraineDescribe analysis of eddy viscosity actual mathematical models for numerical simulation a reversal gas flow in subsonic gas ejector. Considered advantages and disadvantages each of it. Proposed use method of finite elements for provides viscous gas flow calculation of gas ejectors.http://jrnl.nau.edu.ua/index.php/visnik/article/view/9855calculationfinite elements methodgas ejectorgas turbine enginenavier-stokes combined equationssubsonic gas flow
collection	DOAJ
language	English
format	Article
sources	DOAJ
author	Kostjantin Kapitanchuk Pavlo Grekov Mykola Bohdanov Galina Nikitina
spellingShingle	Kostjantin Kapitanchuk Pavlo Grekov Mykola Bohdanov Galina Nikitina FINITE DIFFERENCE METHOD FOR CALCULATING OF THE GAS FLOW IN A SUBSONIC GAS EJECTOR Vìsnik Nacìonalʹnogo Avìacìjnogo Unìversitetu calculation finite elements method gas ejector gas turbine engine navier-stokes combined equations subsonic gas flow
author_facet	Kostjantin Kapitanchuk Pavlo Grekov Mykola Bohdanov Galina Nikitina
author_sort	Kostjantin Kapitanchuk
title	FINITE DIFFERENCE METHOD FOR CALCULATING OF THE GAS FLOW IN A SUBSONIC GAS EJECTOR
title_short	FINITE DIFFERENCE METHOD FOR CALCULATING OF THE GAS FLOW IN A SUBSONIC GAS EJECTOR
title_full	FINITE DIFFERENCE METHOD FOR CALCULATING OF THE GAS FLOW IN A SUBSONIC GAS EJECTOR
title_fullStr	FINITE DIFFERENCE METHOD FOR CALCULATING OF THE GAS FLOW IN A SUBSONIC GAS EJECTOR
title_full_unstemmed	FINITE DIFFERENCE METHOD FOR CALCULATING OF THE GAS FLOW IN A SUBSONIC GAS EJECTOR
title_sort	finite difference method for calculating of the gas flow in a subsonic gas ejector
publisher	National Aviation University
series	Vìsnik Nacìonalʹnogo Avìacìjnogo Unìversitetu
issn	1813-1166 2306-1472
publishDate	2015-12-01
description	Describe analysis of eddy viscosity actual mathematical models for numerical simulation a reversal gas flow in subsonic gas ejector. Considered advantages and disadvantages each of it. Proposed use method of finite elements for provides viscous gas flow calculation of gas ejectors.
topic	calculation finite elements method gas ejector gas turbine engine navier-stokes combined equations subsonic gas flow
url	http://jrnl.nau.edu.ua/index.php/visnik/article/view/9855
work_keys_str_mv	AT kostjantinkapitanchuk finitedifferencemethodforcalculatingofthegasflowinasubsonicgasejector AT pavlogrekov finitedifferencemethodforcalculatingofthegasflowinasubsonicgasejector AT mykolabohdanov finitedifferencemethodforcalculatingofthegasflowinasubsonicgasejector AT galinanikitina finitedifferencemethodforcalculatingofthegasflowinasubsonicgasejector
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FINITE DIFFERENCE METHOD FOR CALCULATING OF THE GAS FLOW IN A SUBSONIC GAS EJECTOR

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