Numerical analysis of cylindrical circumflow control based on pore scale porous medium

ZHANG Yihui; LIU Yong; XIANG Qian; PAN Fanfan

doi:10.7638/kqdlxxb-2023.0148

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Numerical analysis of cylindrical circumflow control based on pore scale porous medium

更新时间：2026-05-28

- Numerical analysis of cylindrical circumflow control based on pore scale porous medium
- Vol. 42, Issue 6, Pages: 96-107(2024)
- 作者机构：
  
  1. 南昌航空大学飞行器工程学院,南昌,330063
  2. 中国航空研究院,北京,100020
- 作者简介：
- 基金信息：
- DOI：10.7638/kqdlxxb-2023.0148
  CLC： V211.3;TB303
- Published：2024
- 稿件说明：
移动端阅览
张伊辉, 刘勇, 相倩, 等. 基于孔隙尺度多孔介质的圆柱绕流控制数值分析[J]. 空气动力学学报, 2024, 42(6): 96−107.

ZHANG Yihui, LIU Yong, XIANG Qian, et al. Numerical analysis of cylindrical circumflow control based on pore scale porous medium[J]. 2024, 42(6): 96-107.
张伊辉, 刘勇, 相倩, 等. 基于孔隙尺度多孔介质的圆柱绕流控制数值分析[J]. 空气动力学学报, 2024, 42(6): 96−107. DOI： 10.7638/kqdlxxb-2023.0148

ZHANG Yihui, LIU Yong, XIANG Qian, et al. Numerical analysis of cylindrical circumflow control based on pore scale porous medium[J]. 2024, 42(6): 96-107. DOI： 10.7638/kqdlxxb-2023.0148.

摘要

为深入理解多孔介质参数对圆柱绕流的影响机制及其效果，本文基于微观孔隙尺度，对覆盖有多孔介质的圆柱在雷诺数为150条件下的绕流流动进行了数值模拟。主要对不同孔隙率与结构下圆柱绕流的流动特性进行了分析，结果表明，多孔介质的覆盖改变了圆柱原有的流体动力学特征：改变多孔介质结构后，尾流稳定性特征均呈现为先增大后减小的趋势；随着多孔介质结构复杂化，圆柱尾部脱落涡的延迟程度有所降低，但涡的边缘化程度保持相对稳定，且流出多孔介质的流体会再次进入多孔介质，导致涡附着于多孔介质表面。在相同结构条件下，当孔隙率达到0.992时，多孔介质尾部涡的周期性脱落延迟与边缘化程度均达到最大值。以上现象归因于多孔介质内部的小尺度流动，流体在穿越小圆柱时经历多次分离与剪切，特别是在多孔介质尾部流出量较大时，形成的剪切层加厚，从而延长了圆柱尾部涡的脱落过程。此外，随着结构复杂化，流体更倾向于在多孔介质尾部附近流出，这进一步增加了多孔介质上下表面剪切层的厚度。本研究揭示了多孔介质孔隙尺度内流体的流动行为对圆柱绕流的影响规律，可为多孔介质在流动及噪声控制领域的工程应用提供参考。

Abstract

In order to deeply understand the influence of porous media parameters on the cylindrical flow and its mechanism

based on the microscopic pore scale of porous media

the flow around the cylinder covered with a Reynolds number of 150 is numerically simulated based on the microscopic pore scale of the porous medium

and the flow characteristics of the cylinder under different porosity and different structures are analyzed. After the cylinder is covered with porous media

the original fluid flow characteristics of the cylinder are changed

and the wake stability characteristics increase first and then decrease with the porosity after the structure of the porous medium is changed. However

with the complexity of the structure

the delay degree of the cylindrical tail shedding vortex decreases

while the marginalization degree of the tail vortex is basically the same

and the fluid flowing out of the porous medium will re-enter the porous medium

so that the vortex adheres to the surface of the porous medium. Under the same structure

when the porosity is 0.992

the periodic shedding delay and marginalization of the tail vortex of the porous medium are the largest. Due to the existence of small-scale flow in the porous medium

multiple separation and shear flow occur when passing through the small cylinder. When the fluid flows out more in the tail of the porous medium

the resulting shear flow forms a thick shear layer at the trailing edge of the porous medium

resulting in the elongation of the vortex detachment of the cylindrical tail. As the structure becomes more complex

the fluid flowing into the porous medium will flow out close to the tail of the porous medium

increasing the thickness of the shear layer on the upper and lower surfaces of the porous medium. The flow behavior of the fluid in the pore scale of porous media plays a key role in the influence of cylindrical flow

and this study can provide theoretical guidance for the effective control of flow and noise in porous media in engineering.

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references

HE M Y, ZHU Z X, NI H Y, et al . Study on influencing factors of college students' air travel[J ] . Times Finance, 2019 ( 21 ): 116 − 118 (in Chinese). doi: SUN:YNJR.0.2019-21-058 SUN:YNJR.0.2019-21-058

CATALANO P, WANG M, IACCARINO G, et al . Numerical simulation of the flow around a circular cylinder at high Reynolds numbers[J ] . International Journal of Heat and Fluid Flow, 2003 , 24 ( 4 ): 463 − 469 .

SARWAR W, MELLIBOVSKY F . Characterization of three-dimensional vortical structures in the wake past a circular cylinder in the transitional regime[J ] . Physics of Fluids, 2020 , 32 ( 7 ): 074104 .

GUO L, MIAO X D, YANG J, et al . Study on noise reduction of high-speed train pantograph by using jet device based on numerical simulation and wind tunnel test[J ] . Journal of the China Railway Society, 2023 , 45 ( 1 ): 20 − 27 (in Chinese).

BRUNEAU C, CREUSÉ E, DEPEYRAS D, et al . Active and passive flow control around simplified ground vehicles[J ] . Journal of Applied Fluid Mechanics, 2012 , 5 ( 1 ): 89 − 93 .

DU H, SHI Z W, CHENG K M, et al . Topological structures of vortex flow on a flying wing aircraft, controlled by a nanosecond pulse discharge plasma actuator[J ] . Applied Physics Letters, 2016 , 108 ( 24 ): 244105 .

RUI T M, SUN L . Drag reduction mechanism of circular cylinder with V-groove structure with different depths[J ] . Ship Engineering, 2021 , 43 ( 4 ): 128 − 135 (in Chinese).

LIAO S H, WU Z H, XIN Z Q . A numerical study on the passive control of flow over cylinder with a flexible plate[J ] . Fly Ash Comprehensive Utilization, 2021 , 35 ( 2 ): 70 − 77, 135 (in Chinese).

SUEKI T, IKEDA M, TAKAISHI T . Aerodynamic noise reduction using porous materials and their application to high-speed pantographs[J ] . Quarterly Report of RTRI, 2009 , 50 ( 1 ): 26 − 31 .

LIU Y, TANG C H, ZHONG B W, et al . Numerical study of aeroacoustic control with bionics airfoil for aircraft[J ] . Journal of Nanchang Hangkong University (Natural Sciences), 2022 , 36 ( 3 ): 111 − 115 (in Chinese).

LIU H R, CHEN N S, LIU Y, et al . Review of porous media used in flow co ntrol and aerodynamic noise reduction[J ] . Acta Aeronautica et Astronautica Sinica, 2023 , 44 ( 16 ): 6 − 26 (in Chinese).

ABDI I A, HOOMAN K, KHASHEHCHI M . A comparison between the separated flow structures near the wake of a bare and a foam-covered circular cylinder[J ] . Journal of Fluids Engineering, 2014 , 136 ( 12 ): 121203 .

AGUIAR J, YAO H, LIU Y. Passive flow/noise control of a cylinder using metal foam[C]// 23rd international congress on sound and vibration, Athens, Greece, 2016.

XU C, MAO Y J, HU Z W . Control of cylinder wake flow and noise through a downstream porous treatment[J ] . Aerospace Science and Technology, 2019 , 88 : 233 − 243 .

DU H, ZHANG Q L, HE L Y, et al . Drag reduction characteristics and mechanism of cylinder covered with porous medium[J ] . Journal of Nanjing University of Aeronautics Astronautics, 2022 , 54 ( 4 ): 611 − 622 (in Chinese).

YUAN H D, XIA C, CHEN Y, et al. Flow around a finite circular cylinder coated with porous media[C]// 54th AIAA Aerospace Sciences Meeting, San Diego, California, USA. Reston, Virginia, 2016.

WEI Z, XIA C, YUAN H D, et al . Experimental study on the wake of a circular cylinder with porous layer coating[J ] . Acta Aerodynamica Sinica, 2017 , 35 ( 2 ): 265 − 270, 289 (in Chinese).

TONG F F, CHENG L A, ZHAO M, et al . The vortex shedding around four circular cylinders in an in-line square configuration[J ] . Physics of Fluids, 2014 , 26 ( 2 ): 024112 .

LINTON D, THORNBER B . Direct numerical simulation of transitional flow in a staggered tube bundle[J ] . Physics of Fluids, 2016 , 28 ( 2 ): 024111 .

NICOLLE A, EAMES I . Numerical study of flow through and around a circular array of cylinders[J ] . Journal of Fluid Mechanics, 2011 , 679 : 1 − 31 .

ARCONDOULIS E J G, LIU Y, RAGNI D, et al . Internal shear layer and vortex shedding development of a structured porous coated cylinder using tomographic particle image velocimetry[J ] . Journal of Fluid Mechanics, 2023 , 967 : A17 .

WEN K B, ARCONDOULIS E J G, LI Z Y, et al . Structure resolved simulations of flow around porous coated cylinders based on a simplified pore-scale model[J ] . Aerospace Science and Technology, 2021 , 119 : 107181 .

LIU C, HUANG J F, SHAO C . Research on wake structure of three-dimensional tandem multi-cylinder flow based on LBM-LES[J ] . Chinese Journal of Applied Mechanics, 2022 , 39 ( 1 ): 186 − 194 (in Chinese).

MÜLLER B . High order numerical simulation of aeolian tones[J ] . Computers Fluids, 2008 , 37 ( 4 ): 450 − 462 .

SATO Y, HATTORI Y . Mechanism of reduction of aeroacoustic sound by porous material: comparative study of microscopic and macroscopic models[J ] . Journal of Fluid Mechanics, 2021 , 929 : A34 .

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