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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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