Using of mathematical model for two-phase jet to compute parameters of plume for a fuel atomizer

Propulsion and Power Plants


Аuthors

Zuyev Y. V.

Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia

e-mail: yuri_zuev@bk.ru

Abstract

A mathematical model for some two-phase jet is proposed to compute plume parameters for a propellant atomizer. Results obtained by means of this model are compared with experimental data. The comparison demonstrates that accuracy of suggested model is quite enough for engineering purposes.

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