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    Dynamics of Large-Scale Structures for Jets in a Crossflow

    Source: Journal of Turbomachinery:;1999:;volume( 121 ):;issue: 003::page 577
    Author:
    F. Muldoon
    ,
    S. Acharya
    DOI: 10.1115/1.2841355
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Results 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.
    keyword(s): Dynamics (Mechanics) , Jets , Vortices , Shear (Mechanics) , Wakes , Compressibility , Computation , Computer software , Velocity measurement AND Wake turbulence ,
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      Dynamics of Large-Scale Structures for Jets in a Crossflow

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    http://yetl.yabesh.ir/yetl1/handle/yetl/123016
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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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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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