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    Fluid Dynamics of a Bistable Diverter Under Ultrasonic Excitation—Part I: Performance Characteristic

    Source: Journal of Fluids Engineering:;2021:;volume( 143 ):;issue: 007::page 071201-1
    Author:
    Mair, Michael
    ,
    Bacic, Marko
    DOI: 10.1115/1.4050083
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper investigates an ultrasonically driven bistable fluidic diverter at inlet nozzle Mach numbers of up to Mn = 0.3 and operating pressure ratios of up to Pr = 1.1. Part I examines the switching characteristics with respect to nondimensional parameters of excitation amplitude, frequency, required energy, switching time and inlet total pressure. It is shown that to promote switching at turbulent jet Mach numbers of up to Mn = 0.3 it is necessary to excite a jet preferred mode of St = 0.45 which differs from previously reported laminar jet operation of the similar device. For the reference case the switching time amounts to 1.2 ms suggesting oscillation frequencies of up to 500 Hz. Part II is a combined experimental and numerical study that examines the triggered instability modes in the free shear layer using large eddy simulations (LES) and visualizes the flow field using Particle Image Velocimetry (PIV).
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      Fluid Dynamics of a Bistable Diverter Under Ultrasonic Excitation—Part I: Performance Characteristic

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    contributor authorMair, Michael
    contributor authorBacic, Marko
    date accessioned2022-02-05T22:17:11Z
    date available2022-02-05T22:17:11Z
    date copyright4/9/2021 12:00:00 AM
    date issued2021
    identifier issn0098-2202
    identifier otherfe_143_07_071201.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4277274
    description abstractThis paper investigates an ultrasonically driven bistable fluidic diverter at inlet nozzle Mach numbers of up to Mn = 0.3 and operating pressure ratios of up to Pr = 1.1. Part I examines the switching characteristics with respect to nondimensional parameters of excitation amplitude, frequency, required energy, switching time and inlet total pressure. It is shown that to promote switching at turbulent jet Mach numbers of up to Mn = 0.3 it is necessary to excite a jet preferred mode of St = 0.45 which differs from previously reported laminar jet operation of the similar device. For the reference case the switching time amounts to 1.2 ms suggesting oscillation frequencies of up to 500 Hz. Part II is a combined experimental and numerical study that examines the triggered instability modes in the free shear layer using large eddy simulations (LES) and visualizes the flow field using Particle Image Velocimetry (PIV).
    publisherThe American Society of Mechanical Engineers (ASME)
    titleFluid Dynamics of a Bistable Diverter Under Ultrasonic Excitation—Part I: Performance Characteristic
    typeJournal Paper
    journal volume143
    journal issue7
    journal titleJournal of Fluids Engineering
    identifier doi10.1115/1.4050083
    journal fristpage071201-1
    journal lastpage071201-9
    page9
    treeJournal of Fluids Engineering:;2021:;volume( 143 ):;issue: 007
    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