Propulsion and Power Plants
Аuthors
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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