The invention discloses a method for analyzing swing high-speed jet characteristics of an
underwater engine
nozzle, and belongs to the field of fluid
mechanical engineering. The implementation methodcomprises the following steps of: through establishing a geometric model of an
underwater solid rocket engine
nozzle, establishing a fluid calculation domain, carrying out geometric optimization on aninterface of the
two fluid calculation domains, setting an interface between the calculation domains for
data transmission to achieve
simulation of the swing working condition of the
nozzle, carryingout grid division on the fluid domains in a partitioned mode, carrying out grid independence
verification, and obtaining the optimal grid number; importing the obtained final
grid file into a FLUENTsolver, setting boundary conditions, an adopted calculation model and a calculation method, and carrying out solving; carrying out numerical
simulation analysis and post-
processing on a numerical calculation result. The
rocket engine nozzle swing high-speed
jet flow characteristic is accurately simulated and analyzed, the nozzle swing high-speed
jet flow rule and mechanism can be easily disclosed,a theoretical basis is provided for the engine nozzle structure design of
underwater powered
missile launching, and the actual
engineering application problem of underwater powered
missile launchingis solved.