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contributor authorW. J. Comfort
contributor authorC. T. Crowe
date accessioned2017-05-08T23:09:11Z
date available2017-05-08T23:09:11Z
date copyrightMarch, 1980
date issued1980
identifier issn0098-2202
identifier otherJFEGA4-26955#54_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/93527
description abstractIn a dispersed two-phase flow, the mixture chokes at a velocity well below the vapor choking velocity, as shown by the velocity at the throat of a converging-diverging, two-phase, supersonic nozzle. The formation and abruptness of a normal shock wave in a two-phase mixture depends strongly on the coupling between phases, particularly upon droplet size. As droplet size becomes small, the mixture behaves as a continuum, and sharp discontinuities can occur at velocities above the two-phase choking velocity but below the vapor sonic velocity. An approximate analysis is performed to incidate the droplet size at which continuum behavior might be expected to occur. A numerical model, which includes the drag, buoyancy, Basset force, and the force associated with the virtual mass effect, is used to show droplet-size dependence in two-phase normal shock waves. For the examples presented, continuum behavior apparently is approached at droplet diameters between 1 and 2 μm, even through normal shock waves.
publisherThe American Society of Mechanical Engineers (ASME)
titleDependence of Shock Characteristics on Droplet Size in Supersonic Two-Phase Mixtures
typeJournal Paper
journal volume102
journal issue1
journal titleJournal of Fluids Engineering
identifier doi10.1115/1.3240624
journal fristpage54
journal lastpage58
identifier eissn1528-901X
keywordsShock (Mechanics)
keywordsMixtures
keywordsShock waves
keywordsForce
keywordsVapors
keywordsComputer simulation
keywordsDrag (Fluid dynamics)
keywordsBuoyancy
keywordsNozzles AND Two-phase flow
treeJournal of Fluids Engineering:;1980:;volume( 102 ):;issue: 001
contenttypeFulltext


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