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contributor authorD. Sivakumar
contributor authorB. N. Raghunandan
date accessioned2017-05-08T23:53:46Z
date available2017-05-08T23:53:46Z
date copyrightDecember, 1997
date issued1997
identifier issn0098-2202
identifier otherJFEGA4-27123#923_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/118858
description abstractAn interesting feature of jets from liquid-liquid coaxial swirl atomizers used in bipropellant rockets or elsewhere is that the outer jet results in a tulip shaped liquid bulb even at operating pressure levels. In this context, experiments have been performed to study the discharge and tulip characteristics of annular jets through qualitative simulation of outer jet flow conditions at which tulip bulb prevails. It is shown that the discharge coefficient increases steeply with Reynolds number, a trend which is distinct from that of circular orifices. The range of flow conditions at which tulip bulb prevails decreases with the annular gap. If a swirl component is introduced into the annular jet, it alters the discharge characteristics and the tulip range with a tendency to form multiple tulips. Variation of tulip length for different annular gaps shows a common trend when plotted against liquid flow rate. The experimental data of tulip length agree reasonably with the theoretical model reported in literature.
publisherThe American Society of Mechanical Engineers (ASME)
titleA Study on Converging Thin Annular Jets
typeJournal Paper
journal volume119
journal issue4
journal titleJournal of Fluids Engineering
identifier doi10.1115/1.2819518
journal fristpage923
journal lastpage928
identifier eissn1528-901X
keywordsJets
keywordsFlow (Dynamics)
keywordsReynolds number
keywordsSimulation
keywordsPressure
keywordsDischarge coefficient
keywordsOrifices AND Rockets
treeJournal of Fluids Engineering:;1997:;volume( 119 ):;issue: 004
contenttypeFulltext


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