| 注册
首页|期刊导航|沈阳航空航天大学学报|三角形与梯形沟槽结构减阻特性对比

三角形与梯形沟槽结构减阻特性对比

王巍 周艾 王浩 冯贺

沈阳航空航天大学学报2025,Vol.42Issue(4):7-14,8.
沈阳航空航天大学学报2025,Vol.42Issue(4):7-14,8.DOI:10.3969/j.issn.2095-1248.2025.04.002

三角形与梯形沟槽结构减阻特性对比

Comparison of drag reduction characteristics between triangular and trapezoidal groove structure

王巍 1周艾 2王浩 2冯贺2

作者信息

  • 1. 沈阳航空航天大学 民用航空学院 沈阳 110136||辽宁通用航空研究院 飞机设计部,沈阳 110136
  • 2. 沈阳航空航天大学 民用航空学院 沈阳 110136
  • 折叠

摘要

Abstract

In order to investigate the drag reduction characteristics of groove structure,triangular and trapezoidal grooves with different dimensions were selected and simulation comparison on the drag reduction characteristics of flat models with two-dimensional transverse,three-dimensional transverse and three-dimensional longitudinal groove arrangements were carried out.The results show that the groove structure can generate low-speed fluid at the bottom of the groove.The low-speed fluid in the transverse groove can act as a rolling bearing.The drag reduction mechanism of the longitudinal groove can be explained from the perspective of protrusion height theory.The low-speed fluid in the grooves reduces the near-wall velocity gradient,thereby reducing friction drag.The groove structure can effectively reduce the turbulent kinetic energy and shear stress,leading to a reduction in viscous drag.The drag reduction effects of the two-dimensional transverse and the three-dimensional transverse groove model is similar,whereas longitudinal grooves exhibit a higher drag reduction rate than transverse grooves.Moreover,trapezoidal grooves achieve a higher drag reduction rate than triangular grooves.The optimal groove dimensions are a width of 0.1mm and a depth of 0.1mm,yielding a maximum drag reduction rate of 18.57%.

关键词

沟槽结构/低速流体/湍流动能/减阻特性/减阻率

Key words

groove structure/low-speed fluid/turbulent kinetic energy/drag reduction characteristics/drag reduction rate

分类

航空航天

引用本文复制引用

王巍,周艾,王浩,冯贺..三角形与梯形沟槽结构减阻特性对比[J].沈阳航空航天大学学报,2025,42(4):7-14,8.

基金项目

辽宁省自然科学基金(项目编号:2023-MS-243) (项目编号:2023-MS-243)

航空科学基金(项目编号:2020Z006054002) (项目编号:2020Z006054002)

辽宁省教育厅面上项目(项目编号:20240109). (项目编号:20240109)

沈阳航空航天大学学报

2095-1248

访问量0
|
下载量0
段落导航相关论文