A numerical modeling algorithm to investigate emitting of jet propulsion exhaust gas

Аuthors

Galitseysky K. B.

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

Abstract

A computer technique is presented to simulate heat emitting for chemically reacting two-phase jet flows. The technique is based on discovering of optical properties for the flow as well as on numerical algorithm to solve an emitting transport equation by means of discrete-ordinates method. This technique enables to investigate absorptance and radiant emittance for fuel combustion materials of jet propulsions. It is possible to compute emitting for chemically reacting jet flows.