Propulsion and Power Plants
Аuthors
Krylov B. A.1*,
Onishchik I. I.1*,
Yun A. A.2**
1. Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia
2. United Engine Corporation “Saturn”, 163, Lenin av., Rybinsk, Yaroslavl region, 152903, Russia
*e-mail: agulnik@mai.ru
**e-mail: alex@yun.su
Abstract
Results of three-dimensional simulation are presented for flows in a combustion chamber. The results are obtained by using of explicit algebraic model of Reynolds tensions. A comparison is carried out for the computed results and appropriate experimental data.
Keywords:
model of mixing combustion chamber; temperature fields; calculations; experiment