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contributor authorR. A. Bunnell
contributor authorGraduate Research Assistant
contributor authorS. D. Heister
date accessioned2017-05-09T00:02:37Z
date available2017-05-09T00:02:37Z
date copyrightDecember, 2000
date issued2000
identifier issn0098-2202
identifier otherJFEGA4-27157#791_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/123833
description abstractFully 3-D, unsteady, viscous simulations are performed on a plain-orifice pressure atomizer being fed by a manifold with a crossflow. This geometry replicates features present in both liquid rocket and diesel engine injectors. Both noncavitating and cavitating conditions are considered to determine the role of cavitation on the orifice discharge characteristics. The presence of cavitation is shown to affect both the mean and unsteady components of the orifice discharge coefficient. The presence of a significant cavitation zone can inhibit vorticity transport causing nearly all the fluid to be ejected through a crescent-shaped sector of the orifice exit plane. [S0098-2202(00)01604-7]
publisherThe American Society of Mechanical Engineers (ASME)
titleThree-Dimensional Unsteady Simulation of Cavitating Flows in Injector Passages
typeJournal Paper
journal volume122
journal issue4
journal titleJournal of Fluids Engineering
identifier doi10.1115/1.1315590
journal fristpage791
journal lastpage797
identifier eissn1528-901X
keywordsFlow (Dynamics)
keywordsCavitation
keywordsEjectors
keywordsSimulation
keywordsManifolds
keywordsFluids
keywordsDischarge coefficient
keywordsPressure
keywordsEngineering simulation AND Density
treeJournal of Fluids Engineering:;2000:;volume( 122 ):;issue: 004
contenttypeFulltext


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