船舶 ›› 2020, Vol. 31 ›› Issue (05): 11-20.DOI: 10.19423/j.cnki.31-1561/u.2020.05.011

• 研究与设计 • 上一篇    下一篇

导管剖面倾角和拱度对泵喷与艇体相互作用影响的数值分析

董新国1,2, 林辉1, 严鹏1,2, 李宁1,2   

  1. 1.中国船舶及海洋工程设计研究院 上海200011;
    2.喷水推进技术重点实验室 上海200011
  • 收稿日期:2020-03-03 修回日期:2020-03-12 出版日期:2020-10-25 发布日期:2021-08-20
  • 作者简介:董新国(1979-),男,博士,研究员。研究方向:喷水推进。林 辉(1977-),男,硕士,高级工程师。研究方向:喷水推进。严 鹏(1990-),男,博士,工程师。研究方向:喷水推进。李 宁(1983-),男,博士,研究员。研究方向:喷水推进。
  • 基金资助:
    国家部委基金资助项目(JCKY2019206D006)

Numerical Analysis of Influence of Duct Inclination Angle and Camber on Interaction between Pump Jet and Hull

DONG Xin-guo1,2, LIN Hui1, YAN Peng1,2, LI Ning1,2   

  1. 1. Marine Design & Research Institute of China, Shanghai 200011, China;
    2. Science and Technology on Water Jet Propulsion Laboratory, Shanghai 200011, China
  • Received:2020-03-03 Revised:2020-03-12 Online:2020-10-25 Published:2021-08-20

摘要: 导管是泵喷推进器的重要组成部分,为剖面机翼型、轴对称环形结构,是推进器内外流场的控制面。为分析导管对泵喷与艇体相互作用的影响,文章以SUBOFF艇尾15°去流角配置NACA66-0.8翼型导管为对象,通过数值计算方法,采用虚拟盘模型模拟转定子推力,分析了导管翼剖面倾角与拱度变化对推力减额、动量影响系数及流量的影响及变化趋势。最后,给出了泵喷工程设计中导管翼剖面倾角、拱度取值的建议,为泵喷导管优化设计提供参考。

关键词: 泵喷, 导管, 倾角, 拱度, 推力减额, 动量影响系数

Abstract: The duct which is the axisymmetric annular structure with airfoil section is the important component of a pumpjet propulsor.It is the surface that controls the internal and external flow field of the propulsor. The influence of the duct on the interaction between the pump jet and the hull has been analyzed based on the duct with the section profile of NACA66-0.8 equipped at the SUBOFF stern with the exit angle of 15°. The thrusts of the rotor and stator are numerically calculated by the virtual disk model in order to analyze the influence of the section inclination angle and the camber of the duct on the thrust deduction fraction, momentum impact factor and mass flow rate, as well as its variation law. Finally, suggestions are given for the inclination angle and camber of the duct section in the engineering design of the pump jet. It can provide reference for the optimal design of the duct of the pump jet.

Key words: pumpjet, duct, inclination angle, camber, thrust deduction fraction, momentum impact factor

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