A front-
stator pump-
jet propulsion device and fluid
analysis method, belonging to the field of
underwater propulsion technology, includes: a duct, a hub, and a propulsion
assembly. The duct, hub, and propulsion
assembly are coaxially arranged, with the hub and propulsion
assembly installed inside the duct. The propulsion assembly includes multiple
stator blades and multiple rotor blades, with an odd number of
stator blades, more stator blades than rotor blades. The stator blades are fixed to the
leading edge region of the inner wall of the duct, and the rotor blades are mounted on the hub. The stator blades are located upstream of the rotor blades and form an axially connected series structure, collectively constituting the energy conversion unit in the flow channel inside the duct. This invention, through the combination of an odd number of stator blades and an asymmetric number of rotor blades, effectively suppresses
harmonic resonance at the blade passing frequency, reduces the peak
noise levels of the shaft frequency and blade frequency, improves the hydrodynamic performance of the pump-
jet propulsion device under different operating conditions, reduces the excitation force and
noise of the pump-
jet propulsion device, and improves the stealth performance of
underwater vehicles.