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contributor authorD. W. Choi
contributor authorF. B. Gessner
contributor authorG. C. Oates
date accessioned2017-05-08T23:22:50Z
date available2017-05-08T23:22:50Z
date copyrightMarch, 1986
date issued1986
identifier issn0098-2202
identifier otherJFEGA4-27018#39_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/101337
description abstractThe mixing of a subsonic confined air jet with a coaxial secondary air stream is investigated experimentally. This work differs from previous studies in that emphasis is placed on the effects of an imposed adverse pressure gradient on mixing characteristics in the initial mixing (potential core) and transition regions. The results indicate that the presence of an adverse pressure gradient promotes more rapid mixing and spreading of the shear layer in the initial mixing region, as well as elevated turbulent normal stress and shear stress levels in the outer portion of the mixing layer after the primary and secondary streams have merged. Significant radial static pressure variations occur in both the initial mixing and transition regions as a result of turbulent normal stress gradients and streamline curvature effects induced by potential core entrainment.
publisherThe American Society of Mechanical Engineers (ASME)
titleMeasurements of Confined, Coaxial Jet Mixing With Pressure Gradient
typeJournal Paper
journal volume108
journal issue1
journal titleJournal of Fluids Engineering
identifier doi10.1115/1.3242541
journal fristpage39
journal lastpage46
identifier eissn1528-901X
keywordsMeasurement
keywordsPressure gradient
keywordsStress
keywordsShear (Mechanics)
keywordsTurbulence
keywordsPressure
keywordsAir jets AND Gradients
treeJournal of Fluids Engineering:;1986:;volume( 108 ):;issue: 001
contenttypeFulltext


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