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contributor authorN. I. Abou-Haidar
contributor authorS. L. Dixon
date accessioned2017-05-08T23:45:50Z
date available2017-05-08T23:45:50Z
date copyrightJuly, 1994
date issued1994
identifier issn0889-504X
identifier otherJOTUEI-28637#535_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/114557
description abstractThis paper considers the compressible flow pressure losses in sharp-cornered wye-junctions with symmetric branches under dividing and combining flow conditions. Determination of the additional total pressure losses occurring in flow through several three-leg junctions, using dry air as the working fluid, has been made experimentally. Results covering a wide speed range up to choking are presented for 30, 60, and 90 deg wye-junctions. Separate flow visualization schlieren tests detected the presence of normal shock waves, located at up to one duct diameter downstream of the junction, and therefore confirmed the choking of the flow at the vena contracta. The highest attainable Mach number (M3 ) of the averaged whole flow was 0.9 for one of the dividing flow geometries and 0.65 for several of the combining flow cases. These values of M3 were the maximum possible and hence represent a limiting condition dictated by choking. In general, the compressible flow loss coefficients, caused by the presence of the wye-junctions, can be expected to be higher for dividing flows and lower for combining flows than would be the case for incompressible flows because of the influence of Mach number, M3 .
publisherThe American Society of Mechanical Engineers (ASME)
titleMeasurement of Compressible Flow Pressure Losses in Wye-Junctions
typeJournal Paper
journal volume116
journal issue3
journal titleJournal of Turbomachinery
identifier doi10.1115/1.2929442
journal fristpage535
journal lastpage541
identifier eissn1528-8900
keywordsPressure
keywordsCompressible flow
keywordsJunctions
keywordsFlow (Dynamics)
keywordsMach number
keywordsFluids
keywordsShock waves
keywordsFlow visualization
keywordsBifurcation AND Ducts
treeJournal of Turbomachinery:;1994:;volume( 116 ):;issue: 003
contenttypeFulltext


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