Logo BSU

Please use this identifier to cite or link to this item: https://elib.bsu.by/handle/123456789/208922
Title: Computational model for fuel component supply into a combustion chamber of LRE
Authors: Teterev, A. V.
Mandrik, P. A.
Rudak, L. V.
Misyuchenko, N. I.
Keywords: ЭБ БГУ::ЕСТЕСТВЕННЫЕ И ТОЧНЫЕ НАУКИ::Математика
ЭБ БГУ::ОБЩЕСТВЕННЫЕ НАУКИ::Информатика
ЭБ БГУ::ЕСТЕСТВЕННЫЕ И ТОЧНЫЕ НАУКИ::Кибернетика
Issue Date: 2017
Citation: Journal of Physics: Conference Series. 2017. T. 937. №1. C.012054.
Abstract: A 2D-3D computational model for calculating a flow inside jet injectors that feed fuel components to a combustion chamber of a liquid rocket engine is described. The model is based on the gasdynamic calculation of compressible medium. Model software provides calculation of both one-and two-component injectors. Flow simulation in two-component injectors is realized using the scheme of separate supply of" gas-gas" or" gas-liquid" fuel components. An algorithm for converting a continuous liquid medium into a" cloud" of drops is described. Application areas of the developed model and the results of 2D simulation of injectors to obtain correction factors in the calculation formulas for fuel supply are discussed.
URI: http://elib.bsu.by/handle/123456789/208922
Appears in Collections:Статьи факультета прикладной математики и информатики

Files in This Item:
File Description SizeFormat 
Computational modelfor fuel component supply into.pdf2,36 MBAdobe PDFView/Open
Show full item record Google Scholar



PlumX

Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.