Transactions of FAMENA, Vol. 45 No. 1, 2021.
Original scientific paper
https://doi.org/10.21278/TOF.451004819
Investigation of Key Parameters for Hydraulic Optimization of an Inlet Duct Based on a Whole Waterjet Propulsion Pump System
Weixuan Jiao
; College of Hydraulic Science and Engineering, Yangzhou University, Yangzhou, Jiangsu, P.R. China
Li Cheng
; College of Hydraulic Science and Engineering, Yangzhou University, Yangzhou, Jiangsu, P.R. China
Di Zhang
; College of Hydraulic Science and Engineering, Yangzhou University, Yangzhou, Jiangsu, P.R. China
Bowen Zhang
; College of Hydraulic Science and Engineering, Yangzhou University, Yangzhou, Jiangsu, P.R. China
Yeping Su
; College of Hydraulic Science and Engineering, Yangzhou University, Yangzhou, Jiangsu, P.R. China
Abstract
The hydraulic performance of an inlet duct directly affects the overall performance of a waterjet propulsion system. Key parameters for the hydraulic optimization of the inlet duct are explored using the computational fluid dynamics (CFD) technology to improve the hydraulic performance of the waterjet propulsion system. In the CFD simulation and experiment, an inlet duct with different flow and geometric parameters is simulated. By comparing grid sensitivity and different turbulence models, a suitable grid size and a turbulence model are determined. The comparison between the numerical simulation and the experiment shows that the numerical results are reliable. The results of the calculation and analysis of different speed cases show that the ship speed affects the efficiency of the waterjet propulsion system. In particular, the system efficiency increases first and then decreases with an increase in the ship speed. Under the conditions of constant ship speed and rotational speed, the influence of the length and dip angle of the inlet duct on the waterjet propulsion system is investigated using a single factor method. The results show that the dip angle has an obvious effect on the hydraulic performance of the inlet duct, and an extremely small angle of inclination will lead to poor flow patterns in the inlet passage. When the length is approximately six times the inlet duct outlet diameter, and the dip angle is 30°–35°, the hydraulic performance of the waterjet propulsion pump system is satisfactory.
Keywords
hydraulic performance; waterjet propulsion; inlet duct; optimization
Hrčak ID:
256369
URI
Publication date:
19.5.2021.
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