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    Noncanonical Short Hole Jets-in-Crossflow for Turbine Film Cooling

    Source: Journal of Applied Mechanics:;2006:;volume( 073 ):;issue: 003::page 474
    Author:
    Michael W. Plesniak
    DOI: 10.1115/1.2130359
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents a review of research done over the past several years at Purdue on non-canonical jets-in-crossflow. It is a retrospective and an integrative compilation of results previously reported as well as some new ones. The emphasis is on jets emanating from “short” holes, with length-diameter ratios of one or less. A canonical jet-in-crossflow configuration is one in which a fully developed jet issues from a long pipe fed by a large plenum, into a semi-infinite cross flow. The configuration presented here is noncanonical in the sense that jet issues from a short hole and thus the flow is unable to “adjust” to the hole, unlike the case of a long hole in which fully developed pipe flow can be attained. This is motivated by gas turbine film cooling applications. Experimental results acquired with particle image velocimetry will primarily be presented, with some complementary information gained from RANS simulations of the flow. Many different aspects of the problem have been investigated, and in this paper the focus will be on structural features within the hole and in the developing jet and crossflow interaction. A significant result is that the in-hole vortical structures, depending on their sense of rotation, tend to augment or weaken the primary counter-rotating vortex pair. This impacts global features such as jet trajectory and spreading.
    keyword(s): Jets , Flow (Dynamics) , Vortices , Cooling , Particulate matter , Trajectories (Physics) , Fluids , Boundary layers AND Turbines ,
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      Noncanonical Short Hole Jets-in-Crossflow for Turbine Film Cooling

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    contributor authorMichael W. Plesniak
    date accessioned2017-05-09T00:18:40Z
    date available2017-05-09T00:18:40Z
    date copyrightMay, 2006
    date issued2006
    identifier issn0021-8936
    identifier otherJAMCAV-26599#474_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/133055
    description abstractThis paper presents a review of research done over the past several years at Purdue on non-canonical jets-in-crossflow. It is a retrospective and an integrative compilation of results previously reported as well as some new ones. The emphasis is on jets emanating from “short” holes, with length-diameter ratios of one or less. A canonical jet-in-crossflow configuration is one in which a fully developed jet issues from a long pipe fed by a large plenum, into a semi-infinite cross flow. The configuration presented here is noncanonical in the sense that jet issues from a short hole and thus the flow is unable to “adjust” to the hole, unlike the case of a long hole in which fully developed pipe flow can be attained. This is motivated by gas turbine film cooling applications. Experimental results acquired with particle image velocimetry will primarily be presented, with some complementary information gained from RANS simulations of the flow. Many different aspects of the problem have been investigated, and in this paper the focus will be on structural features within the hole and in the developing jet and crossflow interaction. A significant result is that the in-hole vortical structures, depending on their sense of rotation, tend to augment or weaken the primary counter-rotating vortex pair. This impacts global features such as jet trajectory and spreading.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleNoncanonical Short Hole Jets-in-Crossflow for Turbine Film Cooling
    typeJournal Paper
    journal volume73
    journal issue3
    journal titleJournal of Applied Mechanics
    identifier doi10.1115/1.2130359
    journal fristpage474
    journal lastpage482
    identifier eissn1528-9036
    keywordsJets
    keywordsFlow (Dynamics)
    keywordsVortices
    keywordsCooling
    keywordsParticulate matter
    keywordsTrajectories (Physics)
    keywordsFluids
    keywordsBoundary layers AND Turbines
    treeJournal of Applied Mechanics:;2006:;volume( 073 ):;issue: 003
    contenttypeFulltext
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