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contributor authorH. S. Shen
contributor authorD. O. Rockwell
date accessioned2017-05-08T22:59:01Z
date available2017-05-08T22:59:01Z
date copyrightMarch, 1975
date issued1975
identifier issn0098-2202
identifier otherJFEGA4-26866#60_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/87693
description abstractPotential flow, control volume, and frozen vorticity models have been used to analyze the wall jet-receiver system. The potential flow model predicts well the extent of the region of influence upstream of the receiver entrance for jet widths the same order as the receiver width, but the assumption of irrotationality drastically mispredicts the receiver spill flow angle. A control volume model which accounts for the extent of influence upstream of the receiver entrance and the possibility of continuous wall stall accurately predicts the receiver spill flow angle for most receiver spill flow ratios. The frozen vorticity model predicts velocity profiles in the receiver entrance region reasonably well, and slightly overpredicts the pressure recovery coefficient in the receiver entrance region.
publisherThe American Society of Mechanical Engineers (ASME)
titleInviscid Approximations for Wall Jet-Receiver Interaction
typeJournal Paper
journal volume97
journal issue1
journal titleJournal of Fluids Engineering
identifier doi10.1115/1.3447217
journal fristpage60
journal lastpage66
identifier eissn1528-901X
keywordsApproximation
keywordsFlow (Dynamics)
keywordsVorticity
keywordsEntrance region
keywordsFlow control
keywordsVelocity AND Pressure
treeJournal of Fluids Engineering:;1975:;volume( 097 ):;issue: 001
contenttypeFulltext


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