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    Sinusoidal Excitation of a Free Turbulent Jet With Constant Amplitude Transverse Pressure Gradients Near the Nozzle Exit: Part II: An A-C Fluidic Model for the Jet Gain

    Source: Journal of Dynamic Systems, Measurement, and Control:;1973:;volume( 095 ):;issue: 002::page 174
    Author:
    A. K. Stiffler
    ,
    J. L. Shearer
    DOI: 10.1115/1.3426675
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A free turbulent jet is perturbed transverse to the flow direction by a sinusoidal pressure gradient near the nozzle exit. An a-c model for the jet gain, based upon the control region dynamics and a uniform deflection of the jet downstream of this region, is generally verified in conjunction with attenuated mean shear velocities. A method is given to experimentally determine the effective amplitude of the input signal at the interface of the jet.
    keyword(s): Turbulence , Nozzles , Pressure gradient , Signals , Deflection , Shear (Mechanics) , Dynamics (Mechanics) AND Flow (Dynamics) ,
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      Sinusoidal Excitation of a Free Turbulent Jet With Constant Amplitude Transverse Pressure Gradients Near the Nozzle Exit: Part II: An A-C Fluidic Model for the Jet Gain

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    http://yetl.yabesh.ir/yetl1/handle/yetl/163681
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    • Journal of Dynamic Systems, Measurement, and Control

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    contributor authorA. K. Stiffler
    contributor authorJ. L. Shearer
    date accessioned2017-05-09T01:36:15Z
    date available2017-05-09T01:36:15Z
    date copyrightJune, 1973
    date issued1973
    identifier issn0022-0434
    identifier otherJDSMAA-26001#174_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/163681
    description abstractA free turbulent jet is perturbed transverse to the flow direction by a sinusoidal pressure gradient near the nozzle exit. An a-c model for the jet gain, based upon the control region dynamics and a uniform deflection of the jet downstream of this region, is generally verified in conjunction with attenuated mean shear velocities. A method is given to experimentally determine the effective amplitude of the input signal at the interface of the jet.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleSinusoidal Excitation of a Free Turbulent Jet With Constant Amplitude Transverse Pressure Gradients Near the Nozzle Exit: Part II: An A-C Fluidic Model for the Jet Gain
    typeJournal Paper
    journal volume95
    journal issue2
    journal titleJournal of Dynamic Systems, Measurement, and Control
    identifier doi10.1115/1.3426675
    journal fristpage174
    journal lastpage179
    identifier eissn1528-9028
    keywordsTurbulence
    keywordsNozzles
    keywordsPressure gradient
    keywordsSignals
    keywordsDeflection
    keywordsShear (Mechanics)
    keywordsDynamics (Mechanics) AND Flow (Dynamics)
    treeJournal of Dynamic Systems, Measurement, and Control:;1973:;volume( 095 ):;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