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    On the Interpretation of Measured Profile Losses in Unsteady Wake–Turbine Blade Interaction Studies

    Source: Journal of Turbomachinery:;1998:;volume( 120 ):;issue: 002::page 276
    Author:
    H. P. Hodson
    ,
    W. N. Dawes
    DOI: 10.1115/1.2841403
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The interaction of wakes shed by a moving blade row with a downstream blade row causes unsteady flow. The meaning of the free-stream stagnation pressure and stagnation enthalpy in these circumstances has been examined using simple analyses, measurements, and CFD. The unsteady flow in question arises from the behavior of the wakes as so-called negative jets. The interactions of the negative jets with the downstream blades lead to fluctuations in static pressure, which in turn generate fluctuations in the stagnation pressure and stagnation enthalpy. It is shown that the fluctuations of the stagnation quantities created by unsteady effects within the blade row are far greater than those within the incoming wake. The time-mean exit profiles of the stagnation pressure and stagnation enthalpy are affected by these large fluctuations. This phenomenon of energy separation is much more significant than the distortion of the time-mean exit profiles that is caused directly by the cross-passage transport associated with the negative jet, as described by Kerrebrock and Mikolajczak. Finally, it is shown that if only time-averaged values of loss are required across a blade row, it is nevertheless sufficient to determine the time-mean exit stagnation pressure.
    keyword(s): Turbine blades , Wakes , Blades , Pressure , Fluctuations (Physics) , Enthalpy , Unsteady flow , Jets , Computational fluid dynamics , Separation (Technology) AND Measurement ,
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      On the Interpretation of Measured Profile Losses in Unsteady Wake–Turbine Blade Interaction Studies

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    contributor authorH. P. Hodson
    contributor authorW. N. Dawes
    date accessioned2017-05-08T23:58:12Z
    date available2017-05-08T23:58:12Z
    date copyrightApril, 1998
    date issued1998
    identifier issn0889-504X
    identifier otherJOTUEI-28665#276_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/121328
    description abstractThe interaction of wakes shed by a moving blade row with a downstream blade row causes unsteady flow. The meaning of the free-stream stagnation pressure and stagnation enthalpy in these circumstances has been examined using simple analyses, measurements, and CFD. The unsteady flow in question arises from the behavior of the wakes as so-called negative jets. The interactions of the negative jets with the downstream blades lead to fluctuations in static pressure, which in turn generate fluctuations in the stagnation pressure and stagnation enthalpy. It is shown that the fluctuations of the stagnation quantities created by unsteady effects within the blade row are far greater than those within the incoming wake. The time-mean exit profiles of the stagnation pressure and stagnation enthalpy are affected by these large fluctuations. This phenomenon of energy separation is much more significant than the distortion of the time-mean exit profiles that is caused directly by the cross-passage transport associated with the negative jet, as described by Kerrebrock and Mikolajczak. Finally, it is shown that if only time-averaged values of loss are required across a blade row, it is nevertheless sufficient to determine the time-mean exit stagnation pressure.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleOn the Interpretation of Measured Profile Losses in Unsteady Wake–Turbine Blade Interaction Studies
    typeJournal Paper
    journal volume120
    journal issue2
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2841403
    journal fristpage276
    journal lastpage284
    identifier eissn1528-8900
    keywordsTurbine blades
    keywordsWakes
    keywordsBlades
    keywordsPressure
    keywordsFluctuations (Physics)
    keywordsEnthalpy
    keywordsUnsteady flow
    keywordsJets
    keywordsComputational fluid dynamics
    keywordsSeparation (Technology) AND Measurement
    treeJournal of Turbomachinery:;1998:;volume( 120 ):;issue: 002
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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