The study of aerodynamics and mass transfer in vortex burners of the combustion chambers of gas turbine engines.

Аuthors

Lanskii A. M.^*, Lukachev S. V.^**, Matveev S. G.

Samara National Research University named after Academician S.P. Korolev, 34, Moskovskoye shosse, Samara, 443086, Russia

*e-mail: amlansky@mail.com
**e-mail: lukachev@mail.ru

Abstract

Results of the investigations of aerodynamic flow structure and masoobmena a swirl burner combustion chambers of gas turbine engines. An empirical formula was obtained by the residence time of fuel-air mixture in the recirculation zone on the scale of the burnerthe swirl, the escape velocity, mixture composition and method of its filing.

Keywords:

flow structure; masoobmen; swirl burner; stay; area recycling.

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