Comprehensive Research on the Effects of Different Launch Conditions on Pump-jet Propulsor Performance

This paper compares the cavitation of a pump-jet propulsor under different launch conditions and discusses the effects of cavitation on the performance and noise of the pump-jet propulsor rotor blade. At the same time, the load and deformation of the rotor blade under the conditions of cavitation are studied via the one-way fluid-structure interaction (FSI) approach. The results show that the cavitation of the pump-jet propulsor decreases with increasing launch depth and speed. The performance decreases with increasing launch speed at large depths, whereas the performance improves with increasing launch speed at small depths due to the improvement of the cavitation on the rotor blades. Increasing launch speed and depth increase the noise caused by the rotor of the pump-jet propulsor, and the increase in flow rate caused by the improvement of cavitation also increases the noise level. Moreover, increasing launch depth increases the overall load of the blade and produces a larger deformation, while the speed affects the distribution of the load on the blade. In addition, with the improvement of cavitation caused by increasing launch speed, the deformation of the blade decreases.

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Publication Details

Journal
Journal of Applied Fluid Mechanics
Published
2025-02-05
DOI
https://doi.org/10.47176/jafm.18.4.2937
Primary Topic
Rocket and propulsion systems research
Type
article
Field-Weighted Citation Impact
0.00

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article

Comprehensive Research on the Effects of Different Launch Conditions on Pump-jet Propulsor Performance

Journal of Applied Fluid Mechanics
Rocket and propulsion systems research
article

Comprehensive Research on the Effects of Different Launch Conditions on Pump-jet Propulsor Performance

article en

Abstract

This paper compares the cavitation of a pump-jet propulsor under different launch conditions and discusses the effects of cavitation on the performance and noise of the pump-jet propulsor rotor blade. At the same time, the load and deformation of the rotor blade under the conditions of cavitation are studied via the one-way fluid-structure interaction (FSI) approach. The results show that the cavitation of the pump-jet propulsor decreases with increasing launch depth and speed. The performance decreases with increasing launch speed at large depths, whereas the performance improves with increasing launch speed at small depths due to the improvement of the cavitation on the rotor blades. Increasing launch speed and depth increase the noise caused by the rotor of the pump-jet propulsor, and the increase in flow rate caused by the improvement of cavitation also increases the noise level. Moreover, increasing launch depth increases the overall load of the blade and produces a larger deformation, while the speed affects the distribution of the load on the blade. In addition, with the improvement of cavitation caused by increasing launch speed, the deformation of the blade decreases.

Journal of Applied Fluid MechanicsVol. 18(4)
Jiangsu University (CN)
National Natural Science Foundation of China
Affordable and clean energy
Openalex Percentile: Top 97%
Rocket and propulsion systems research
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Comprehensive Research on the Effects of Different Launch Conditions on Pump-jet Propulsor Performance · Journal of Applied Fluid Mechanics (2025) | TGRS Research Map | TGRS