The method for calculating the fuel jet geometric parameters for a open combustion chambers of medium-reverse engines
This article describes the calculation method for determination of the range and a cone angle of a fuel jet in its movement process occured in open combustion chambers of medium-reverse diesel engines. The method proposed synthesizes a turbulent and a zone model that allows the pulsed nature of injection, the effect of the pressure front and the sprayed fuel jet supply to be taken into account. There are given the calculation algorithm according to Lyshevsky’s criteria equations. The calculation results are presented and compared to the experimental results.