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contributor authorA. H. Stenning
contributor authorA. A. Schachenmann
date accessioned2017-05-09T01:36:33Z
date available2017-05-09T01:36:33Z
date copyrightSeptember, 1973
date issued1973
identifier issn0098-2202
identifier otherJFEGA4-26849#401_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/163876
description abstractIn studies of a diffuser operating with inlet flow oscillations, it has been found that large amplification of the inlet velocity oscillations occurs within the diffuser when the throat Reynolds number lies in the range 103 to 104 . This phenomenon is caused by travelling waves in the wall boundary layer which are initiated in the laminar portion of the boundary layer and propagate into the turbulent boundary layer, causing large variations in the displacement thickness.
publisherThe American Society of Mechanical Engineers (ASME)
titleOscillatory Flow Phenomena in Diffusers at Low Reynolds Numbers
typeJournal Paper
journal volume95
journal issue3
journal titleJournal of Fluids Engineering
identifier doi10.1115/1.3447043
journal fristpage401
journal lastpage407
identifier eissn1528-901X
keywordsDiffusers
keywordsFlow (Dynamics)
keywordsReynolds number
keywordsOscillations
keywordsBoundary layers
keywordsBoundary layer turbulence
keywordsDisplacement
keywordsThickness AND Waves
treeJournal of Fluids Engineering:;1973:;volume( 095 ):;issue: 003
contenttypeFulltext


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