The simulation of the working process in the mixing chamber through the tree-section burner with forced air supply

Аuthors

Shirokov I. N.^*, Abashev V. M.^**

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

*e-mail: Igor_Shirokov@hotmail.com
**e-mail: abashevVM@mai.ru

Abstract

A general principle of operation and a brief history of the multicircuit direct-flow combustion chambers on solid fuels are revealed. The design of an adjustable model mixing chamber is proposed, in which instead of a solid fuel charge three-section burner with forced air supply is used.

Keywords:

forced air gas burner, adjustable mixing chamber, supersonic, double-circuit, rocket-ramjet