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contributor authorF. Muldoon
contributor authorS. Acharya
date accessioned2017-05-09T00:01:16Z
date available2017-05-09T00:01:16Z
date copyrightJuly, 1999
date issued1999
identifier issn0889-504X
identifier otherJOTUEI-28670#577_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/123016
description abstractResults of a three-dimensional unsteady computational study of a row of jets injected normal to a crossflow are presented with the aim of understanding the dynamics of the large-scale structures in the region near the jet. The jet to crossflow velocity ratio is 0.5. A modified version of the computer program (INS3D), which utilizes the method of artificial compressibility, is used for the computations. Results obtained clearly indicate that the near-field large-scale structures are extremely dynamic in nature, and undergo breakup and reconnection processes. The dynamic near-field structures identified include the counterrotating vortex pair (CVP), the horseshoe vortex, wake vortex, wall vortex, and shear layer vortex. The dynamic features of these vortices are presented in this paper. The CVP is observed to be a convoluted structure interacting with the wall and horseshoe vortices. The shear layer vortices are stripped by the crossflow, and undergo pairing and stretching events in the leeward side of the jet. The wall vortex is reoriented into the upright wake system. Comparison of the predictions with mean velocity measurements is made. Reasonable agreement is observed.
publisherThe American Society of Mechanical Engineers (ASME)
titleDynamics of Large-Scale Structures for Jets in a Crossflow
typeJournal Paper
journal volume121
journal issue3
journal titleJournal of Turbomachinery
identifier doi10.1115/1.2841355
journal fristpage577
journal lastpage587
identifier eissn1528-8900
keywordsDynamics (Mechanics)
keywordsJets
keywordsVortices
keywordsShear (Mechanics)
keywordsWakes
keywordsCompressibility
keywordsComputation
keywordsComputer software
keywordsVelocity measurement AND Wake turbulence
treeJournal of Turbomachinery:;1999:;volume( 121 ):;issue: 003
contenttypeFulltext


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