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.