Numerical analysis of unsteady hydrodynamic performance of pump-jet propulsor in oblique flow

International Journal of Naval Architecture and Ocean Engineering

Yao Shi¹  Guang Pan¹  Qiaogao Huang²  Chengcheng Qiu² 

[1] Key Laboratory for Unmanned Vehicle, Northwestern Polytechnical University, Xi'an, 710072, China;School of Marine Science and Technology, Northwestern Polytechnical University, Xi'an, 710072, China;

关键词: Pump-jet propulsor;    Oblique flow;    Unsteady hydrodynamic performance;    Bearing force;    Fluctuating pressure;   

DOI  :  

来源: DOAJ

【 摘 要 】

In this study, the SST k−ω turbulence model and the sliding mesh technology based on RANS method have been adopted to simulate the exciting force and hydrodynamic of a pump-jet propulsor in different oblique inflow angle (0°, 10°, 20°, 30°) and different advance ratio (J = 0.95, J = 1.18, J = 1.58).The fully structured grid and full channel model have been adopted to improved computational accuracy. The classical skewed marine propeller E779A with different advance ratio was carried out to verify the accuracy of the numerical simulation method. The grid independence was verified. The time-domain data of pump-jet propulsor exciting force including bearing force and fluctuating pressure in different working conditions was monitored, and then which was converted to frequency domain data by fast Fourier transform (FFT). The variation laws of bearing force and fluctuating pressure in different advance ratio and different oblique flow angle has been presented. The influence of the peak of pulsation pressure in different oblique flow angle and different advance ratio has been presented. The results show that the exciting force increases with the increase of the advance ratio, the closer which is to the rotor domain and the closer to the blades tip, the greater the variation of the pulsating pressure. At the same time, the exciting force decrease with the oblique flow angle increases. And the vertical and transverse forces will change more obviously, which is the main cause of the exciting force. In addition, the pressure distribution and the velocity distribution of rotor blades tip in different oblique flow angles has been investigated.

【 授权许可】

Unknown