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    Experimental Study of Passive Jet Flow Control of Chamfered Square Cylinder

    Source: Journal of Aerospace Engineering:;2024:;Volume ( 037 ):;issue: 002::page 04023110-1
    Author:
    Feng Xu
    ,
    Zejia Lin
    ,
    Yancen Hou
    ,
    Danyu Li
    ,
    Bin Liu
    ,
    Yongfeng Cheng
    DOI: 10.1061/JAEEEZ.ASENG-4992
    Publisher: ASCE
    Abstract: This study conducted wind tunnel tests to verify a passive jet flow control method for suppressing the aerodynamic force on a chamfered square cylinder at a moderate Reynolds number, focusing on the influence of the opening parameters and the spanwise spacing ratio of hollow pipes on the jet flow control effect. The pressure coefficient distribution on the surface of the cylinder and the overall aerodynamic coefficient were considered in order to systematically analyze the influence of opening shape, opening number, opening height, pipe height, and pipe radial thickness, and to determine the optimal combination of opening parameters. Subsequently, we analyzed the influence of the spanwise spacing ratio on passive jet flow control. Furthermore, the optimal arrangement of the hollow pipe was derived by comparing the aerodynamic coefficients of uncontrolled and controlled cylinders. The results revealed that the passive jet hollow pipe significantly reduces the root mean-square value of the pressure coefficient and the fluctuation of the lift coefficient. Moreover, the platform area of the mean pressure coefficient at the leeward side of the cylinder increases and the mean drag coefficient decreases. The spectrum analysis results showed that the passive jet flow control pipe alters the frequency and intensity of vortex shedding in the wake region. All results indicated that the aerodynamic forces and wakes of a chamfered square cylinder are effectively controlled through jet flow control with perforated hollow pipes.
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      Experimental Study of Passive Jet Flow Control of Chamfered Square Cylinder

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4297168
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    contributor authorFeng Xu
    contributor authorZejia Lin
    contributor authorYancen Hou
    contributor authorDanyu Li
    contributor authorBin Liu
    contributor authorYongfeng Cheng
    date accessioned2024-04-27T22:39:04Z
    date available2024-04-27T22:39:04Z
    date issued2024/03/01
    identifier other10.1061-JAEEEZ.ASENG-4992.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4297168
    description abstractThis study conducted wind tunnel tests to verify a passive jet flow control method for suppressing the aerodynamic force on a chamfered square cylinder at a moderate Reynolds number, focusing on the influence of the opening parameters and the spanwise spacing ratio of hollow pipes on the jet flow control effect. The pressure coefficient distribution on the surface of the cylinder and the overall aerodynamic coefficient were considered in order to systematically analyze the influence of opening shape, opening number, opening height, pipe height, and pipe radial thickness, and to determine the optimal combination of opening parameters. Subsequently, we analyzed the influence of the spanwise spacing ratio on passive jet flow control. Furthermore, the optimal arrangement of the hollow pipe was derived by comparing the aerodynamic coefficients of uncontrolled and controlled cylinders. The results revealed that the passive jet hollow pipe significantly reduces the root mean-square value of the pressure coefficient and the fluctuation of the lift coefficient. Moreover, the platform area of the mean pressure coefficient at the leeward side of the cylinder increases and the mean drag coefficient decreases. The spectrum analysis results showed that the passive jet flow control pipe alters the frequency and intensity of vortex shedding in the wake region. All results indicated that the aerodynamic forces and wakes of a chamfered square cylinder are effectively controlled through jet flow control with perforated hollow pipes.
    publisherASCE
    titleExperimental Study of Passive Jet Flow Control of Chamfered Square Cylinder
    typeJournal Article
    journal volume37
    journal issue2
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/JAEEEZ.ASENG-4992
    journal fristpage04023110-1
    journal lastpage04023110-14
    page14
    treeJournal of Aerospace Engineering:;2024:;Volume ( 037 ):;issue: 002
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian