MODELING OF DYNAMICS OF PERFECT GAS IN ANNULAR NOZZLES OF AIRCRAFTS
Abstract
The dynamics of perfect gas in annular nozzles of aircrafts is considered.
The computational field of annular nozzles and system equations for mathematical
modeling of unsteady axisymmetric compound flows of perfect gas in integral
form are presented. The solving of system equations carry out by procedure of
assignment with using scheme S.K. Godunov – V.P. Kolgan. The results of mathematical modeling of flows of perfect gas in annular nozzle with short-cut central
body are presented.
Issue
Section
Calculation and design