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    Lip Separate Flow Blowing and Analysis of Coherence of Inlet

    Source: Journal of Engineering for Gas Turbines and Power:;1986:;volume( 108 ):;issue: 003::page 562
    Author:
    Z. W. He
    ,
    S. Y. Zhang
    DOI: 10.1115/1.3239947
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: It is found experimentally that blowing at the lip separation of an inlet obviously reduces the turbulence at the inlet exit, and apparently reduces the intensity of pressure fluctuations caused by the shock-boundary layer interaction downstream of the throat. The coherence between pressure in the interaction region and total pressure at the exit is also reduced. The coherence between the pressure in the lip separation region and total pressure at the exit is 0.32. If, in addition, there is a stronger shock downstream of the throat, the abovementioned coherence is reduced to 0.06.
    keyword(s): Pressure , Flow (Dynamics) , Separation (Technology) , Turbulence , Fluctuations (Physics) AND Shock (Mechanics) ,
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      Lip Separate Flow Blowing and Analysis of Coherence of Inlet

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/101113
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorZ. W. He
    contributor authorS. Y. Zhang
    date accessioned2017-05-08T23:22:26Z
    date available2017-05-08T23:22:26Z
    date copyrightJuly, 1986
    date issued1986
    identifier issn1528-8919
    identifier otherJETPEZ-26637#562_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/101113
    description abstractIt is found experimentally that blowing at the lip separation of an inlet obviously reduces the turbulence at the inlet exit, and apparently reduces the intensity of pressure fluctuations caused by the shock-boundary layer interaction downstream of the throat. The coherence between pressure in the interaction region and total pressure at the exit is also reduced. The coherence between the pressure in the lip separation region and total pressure at the exit is 0.32. If, in addition, there is a stronger shock downstream of the throat, the abovementioned coherence is reduced to 0.06.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleLip Separate Flow Blowing and Analysis of Coherence of Inlet
    typeJournal Paper
    journal volume108
    journal issue3
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3239947
    journal fristpage562
    journal lastpage565
    identifier eissn0742-4795
    keywordsPressure
    keywordsFlow (Dynamics)
    keywordsSeparation (Technology)
    keywordsTurbulence
    keywordsFluctuations (Physics) AND Shock (Mechanics)
    treeJournal of Engineering for Gas Turbines and Power:;1986:;volume( 108 ):;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
    yabeshDSpacePersian