A simulation of mass and heat exchange within model combustion chambers

Spacecraft and Rockets


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

Some results are presented to demonstrate application of the Fastest-3D package for simulation of turbulent processes with heat and mass transfer in model combustion chambers. A comparison of numerical and experimental data is presented.

Keywords:

diffuser; heat and mass transfer; Reynolds stresses; adiabatic boundary conditions; experiment; cooling through slit and holes

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