自由端狭缝吸气控制三维方柱绕流

曾令伟; 王汉封; 彭思

doi:10.7638/kqdlxxb-2018.0205

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自由端狭缝吸气控制三维方柱绕流

研究论文 | 更新时间：2026-05-28

- 自由端狭缝吸气控制三维方柱绕流
- Flow control around a three dimensional square cylinder with free-end slot suction
- 空气动力学学报 2020年38卷第6期页码：1093-1101
- 作者机构：
  
  1. 中南大学土木工程学院,长沙,410075
  2. 中南大学高速铁路建造技术国家工程实验室,长沙,410075
- 作者简介：
  
  曾令伟(1993-), 男, 湖北潜江人, 硕士研究生, 研究方向:钝体空气动力学.E-mail:174812223@csu.edu.cn
  王汉封(1976-), 男, 博士, 教授, 博导.E-mail:wanghf@csu.edu.cn
- 基金信息：
  
  国家自然科学基金（11472312）;中南大学研究生自主创新科研基金（2018zzt665）
- DOI：10.7638/kqdlxxb-2018.0205
  中图分类号： V211.3
- 纸质出版：2020
- 稿件说明：
移动端阅览
曾令伟, 王汉封, 彭思. 自由端狭缝吸气控制三维方柱绕流[J]. 空气动力学学报, 2020, 38(6): 1093-1101.

ZENG Lingwei, WANG Hanfeng, PENG Si. Flow control around a three dimensional square cylinder with free-end slot suction[J]. 2020, 38(6): 1093-1101.
曾令伟, 王汉封, 彭思. 自由端狭缝吸气控制三维方柱绕流[J]. 空气动力学学报, 2020, 38(6): 1093-1101. DOI： 10.7638/kqdlxxb-2018.0205.

ZENG Lingwei, WANG Hanfeng, PENG Si. Flow control around a three dimensional square cylinder with free-end slot suction[J]. 2020, 38(6): 1093-1101. DOI： 10.7638/kqdlxxb-2018.0205.

摘要

利用大涡模拟（LES）方法研究了顶部定常狭缝吸气对正方形截面有限长柱体的气动力与绕流特性的影响规律。对比了吸气系数

=0、1、3时的气动力特性及绕流情况，尤其是自由端附近的流动结构。

∞

，其中

为吸气狭缝入口风速，

∞

为自由来流速度。研究发现，顶部定常吸气可以有效地抑制三维柱体气动力，且

=1时抑制效果最为显著，相对于无控制工况，时均阻力$\overline{C_{D}}$、脉动阻力

和脉动升力

分别减少了3.92%、19.08%和40.88%。在

=1时，柱体自由端负压和压力脉动最为显著，有利于柱体两侧形成上升流；顶面压力脉动最强有利于自由端剪切流与尾流间的动量交换，可以有效地抑制柱体展向涡脱落，减小柱体气动力；同时柱体顶面流动出现再附分离现象；而在

=3时柱体顶面大部分区域流动分离被完全抑制。

Abstract

Large eddy simulation (LES) is used to study the influence of free-end steady slot suction on the aerodynamic forces and flow around a three dimensional finite-length square cylinder with a square cross-section. The aerodynamic forces and the flow around the cylinder have been compared systematically for the suction ratios

1 and 3. Special attention is paid on the flow around the free end of the cylinder. It is found that free-end steady slot suction can effectively suppress the aerodynamic forces of the model.

The Controlling result is the best when

=1. Relative to the none control case

the mean drag

fluctuating drag

and fluctuating lift are decreased by 3.92%

19.08%

and 40.88%

respectively. The mean negative pressure and fluctuating pressure on the free end are most significant at

which enhances the upwash flow along cylinder side faces and the momentum exchange between free-end shear flow and near wake flow. Thus

this behavior effectively suppresses the spanwise vortex shedding and the aerodynamic forces of the cylinder; at the same time

the flow separation and reattachment occurred on the top of the cylinder. When

the flow separation in most areas of the top surface of the cylinder is completely inhibited.

关键词

Keywords

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