主动通气对螺旋桨尾流的影响

王志博; 顾津菁; 钱浩城

doi:10.12382/bgxb.2024.0905

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主动通气对螺旋桨尾流的影响

更新时间：2025-10-21

- 主动通气对螺旋桨尾流的影响
- The Influence of Active Ventilation on Propeller Wake
- 兵工学报 2025年46卷第9期页码：240905
- 作者机构：
  
  江苏海洋大学海洋工程学院, 江苏连云港 222005
- 作者简介：
  
  * 2021000063@jou.edu.cn
- 基金信息：
  
  国家自然科学基金项目(51709133);江苏省研究生科研与实践创新计划项目(SJCX23_1821)
- DOI：10.12382/bgxb.2024.0905
  中图分类号：
- 收稿：2024-09-29，
  
  网络出版：2025-09-24，
  
  纸质出版：2025-09-30
- 稿件说明：
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王志博, 顾津菁, 钱浩城. 主动通气对螺旋桨尾流的影响[J]. 兵工学报, 2025,46(9):240905.

Zhibo WANG, Jinjing GU, Haocheng QIAN. The Influence of Active Ventilation on Propeller Wake[J]. Acta Armamentarii, 2025, 46(9): 240905.
王志博, 顾津菁, 钱浩城. 主动通气对螺旋桨尾流的影响[J]. 兵工学报, 2025,46(9):240905. DOI： 10.12382/bgxb.2024.0905.

Zhibo WANG, Jinjing GU, Haocheng QIAN. The Influence of Active Ventilation on Propeller Wake[J]. Acta Armamentarii, 2025, 46(9): 240905. DOI： 10.12382/bgxb.2024.0905.

摘要

针对气泡流对于螺旋桨尾流的影响

基于剪切应力传输

(

为湍流动能

为湍流动能耗散率)分离涡模拟湍流模型与体积分数方程

结合滑移网格技术开展了螺旋桨在气泡流中尾流动力学特性的数值研究

对KP505桨绕流数值模型进行验证

基于多相来流中螺旋桨尾涡的演化机理

提出螺旋桨尾涡演化模型。研究结果表明:所提模型能够较为准确地模拟螺旋桨尾涡的演化过程

对螺旋桨尾流不稳定性的触发机理进行了揭示

径向通气位置影响螺旋桨的翼梢涡和桨毂涡强度与耗散

轴线处通气使桨毂涡膨胀

并使得翼梢涡在远场连通成为涡环

通气位置向翼梢移动

翼梢涡系加速扩张并迅速耗散;研究结果对为螺旋桨设计与制造具有一定的参考价值。

Abstract

In order to investigate the influence of bubbly flow on propeller wake

the wake dynamics characteristics of propellers in bubbly flow are numerically studied based on the SST

DES turbulence model and volume fraction equation

and the sliding grid technique.The KP505 propeller flow numerical model is verified.A propeller wake evolution model is proposed based on the evolution mechanis

m of propeller wake in multiphase inflow.The results show that the proposed model can accurately simulate the evolution process of propeller wake and reveal the triggering mechanism of propeller wake instability.The radial ventilation position affects the strength and dissipation of the tip vortex and hub vortex of propeller.The ventilation at the axis causes the hub vortex to expand and connects the tip vortex to form a vortex ring in the far field.The ventilation position moves towards the wing tip

and the vortex system at the wing tip accelerates and rapidly dissipates.The results have certain reference value for the design and manufacturing of propellers.

关键词

Keywords

references

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