open source was used to simulate the spray combustion process in annular combustor of a certain turbojet engine.At first
the k-ε two-equation model
EBU (eddy break up) -Arrhenius turbulent combustion model
and particle stochastic trajectory model were selected to simulate the physical process of flow field.Then implicit coupled algorithm was described for solving gas flow
the Lagrangian method was used to track the movement of droplets in the fluid region
and two-way coupling was used for the effect between gas phase and droplet phase.Distributions of temperature
mach number
velocity and pressure obtained from simulation experiments were reasonable
and distribution of temperature was roughly in accord with that of the literature.This shows that implicit coupled method can well simulate the flow fields in combustion chamber