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    Shear-Layer Detection in Poststenotic Flow by Spectrum Analysis of Doppler Signals

    Source: Journal of Biomechanical Engineering:;1988:;volume( 110 ):;issue: 004::page 320
    Author:
    T. Tamura
    ,
    A. Fronek
    DOI: 10.1115/1.3108448
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Spectrum analysis of the Doppler signals was performed 0.5 tube diameters downstream from an axisymmetric constriction with an area reduction of 80 percent in steady flow at a jet Reynolds number of 2840. Both pulsed and continuous wave (CW) Doppler spectra showed significant reverse flow components in the separated flow. The pulsed Doppler spectra exhibited sudden changes when the sample volume crossed the shear layer between the center jet and the separated flow. A power spectrum equation was theoretically derived from continuity of flow to define the Doppler shift frequency for the shear layer velocity. The CW Doppler spectrum showed a minimum spectrum density at a frequency which equalled the shear layer Doppler shift frequency derived from the equation. The pulsed spectra exhibited the sudden changes at the same frequency as well.
    keyword(s): Flow (Dynamics) , Emission spectroscopy , Shear (Mechanics) , Signals , Spectra (Spectroscopy) , Doppler effect , Equations , Density , Reynolds number AND Waves ,
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      Shear-Layer Detection in Poststenotic Flow by Spectrum Analysis of Doppler Signals

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/103634
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    • Journal of Biomechanical Engineering

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    contributor authorT. Tamura
    contributor authorA. Fronek
    date accessioned2017-05-08T23:26:43Z
    date available2017-05-08T23:26:43Z
    date copyrightNovember, 1988
    date issued1988
    identifier issn0148-0731
    identifier otherJBENDY-25841#320_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/103634
    description abstractSpectrum analysis of the Doppler signals was performed 0.5 tube diameters downstream from an axisymmetric constriction with an area reduction of 80 percent in steady flow at a jet Reynolds number of 2840. Both pulsed and continuous wave (CW) Doppler spectra showed significant reverse flow components in the separated flow. The pulsed Doppler spectra exhibited sudden changes when the sample volume crossed the shear layer between the center jet and the separated flow. A power spectrum equation was theoretically derived from continuity of flow to define the Doppler shift frequency for the shear layer velocity. The CW Doppler spectrum showed a minimum spectrum density at a frequency which equalled the shear layer Doppler shift frequency derived from the equation. The pulsed spectra exhibited the sudden changes at the same frequency as well.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleShear-Layer Detection in Poststenotic Flow by Spectrum Analysis of Doppler Signals
    typeJournal Paper
    journal volume110
    journal issue4
    journal titleJournal of Biomechanical Engineering
    identifier doi10.1115/1.3108448
    journal fristpage320
    journal lastpage325
    identifier eissn1528-8951
    keywordsFlow (Dynamics)
    keywordsEmission spectroscopy
    keywordsShear (Mechanics)
    keywordsSignals
    keywordsSpectra (Spectroscopy)
    keywordsDoppler effect
    keywordsEquations
    keywordsDensity
    keywordsReynolds number AND Waves
    treeJournal of Biomechanical Engineering:;1988:;volume( 110 ):;issue: 004
    contenttypeFulltext
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