A swirlingstyle propellant water ramjet model was established on the basis of a particular model of columnstyle propellant water ramjet. The effect of swirling flow on the flow and reaction characteristics in the water ramjet was simulated by Fluent software. Turbulent flow simulation was performed using the standard kε two equation functions
and combustion reaction was calculated by finiterate/eddydissipation model. The functions were solved by implicit coupling calculation method based on the density. Results show that
adding swirling vanes and increasing the swirling angle can improve the maximum temperature
the average temperature
the outlet velocity and the specific impulse
which proves that adding swirling vanes make drastic improvements of flow and combustion reaction in the water ramjet engine
and the greater swirling angle means the better results.