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

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

Internet

http://jrnl.nau.edu.ua/index.php/visnik/article/view/9855

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