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    An Empirical Prediction Method For Secondary Losses In Turbines—Part II: A New Secondary Loss Correlation

    Source: Journal of Turbomachinery:;2006:;volume( 128 ):;issue: 002::page 281
    Author:
    M. W. Benner
    ,
    S. A. Sjolander
    ,
    S. H. Moustapha
    DOI: 10.1115/1.2162594
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A new empirical prediction method for design and off-design secondary losses in turbines has been developed. The empirical prediction method is based on a new loss breakdown scheme, and as discussed in Part I, the secondary loss definition in this new scheme differs from that in the conventional one. Therefore, a new secondary loss correlation for design and off-design incidence values has been developed. It is based on a database of linear cascade measurements from the present authors’ experiments as well as cases available in the open literature. The new correlation is based on correlating parameters that are similar to those used in existing correlations. This paper also focuses on providing physical insights into the relationship between these parameters and the loss generation mechanisms in the endwall region. To demonstrate the improvements achieved with the new prediction method, the measured cascade data are compared to predictions from the most recent design and off-design secondary loss correlations ( and , 1982, ASME J. Turbomach., 104, pp. 111-119, , , and , 1990, ASME J. Turbomach., 112, pp. 267–276) using the conventional loss breakdown. The Kacker and Okapuu correlation is based on rotating-rig and engine data, and a scaling factor is needed to make their correlation predictions apply to the linear cascade environment. This suggests that there are additional and significant losses in the engine that are not present in the linear cascade environment.
    keyword(s): Cascades (Fluid dynamics) , Boundary layers , Design , Turbines , Databases , Flow (Dynamics) , Measurement , Airfoils , Engines , Thickness AND Mechanisms ,
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      An Empirical Prediction Method For Secondary Losses In Turbines—Part II: A New Secondary Loss Correlation

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    http://yetl.yabesh.ir/yetl1/handle/yetl/134845
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    contributor authorM. W. Benner
    contributor authorS. A. Sjolander
    contributor authorS. H. Moustapha
    date accessioned2017-05-09T00:21:58Z
    date available2017-05-09T00:21:58Z
    date copyrightApril, 2006
    date issued2006
    identifier issn0889-504X
    identifier otherJOTUEI-28728#281_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/134845
    description abstractA new empirical prediction method for design and off-design secondary losses in turbines has been developed. The empirical prediction method is based on a new loss breakdown scheme, and as discussed in Part I, the secondary loss definition in this new scheme differs from that in the conventional one. Therefore, a new secondary loss correlation for design and off-design incidence values has been developed. It is based on a database of linear cascade measurements from the present authors’ experiments as well as cases available in the open literature. The new correlation is based on correlating parameters that are similar to those used in existing correlations. This paper also focuses on providing physical insights into the relationship between these parameters and the loss generation mechanisms in the endwall region. To demonstrate the improvements achieved with the new prediction method, the measured cascade data are compared to predictions from the most recent design and off-design secondary loss correlations ( and , 1982, ASME J. Turbomach., 104, pp. 111-119, , , and , 1990, ASME J. Turbomach., 112, pp. 267–276) using the conventional loss breakdown. The Kacker and Okapuu correlation is based on rotating-rig and engine data, and a scaling factor is needed to make their correlation predictions apply to the linear cascade environment. This suggests that there are additional and significant losses in the engine that are not present in the linear cascade environment.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleAn Empirical Prediction Method For Secondary Losses In Turbines—Part II: A New Secondary Loss Correlation
    typeJournal Paper
    journal volume128
    journal issue2
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2162594
    journal fristpage281
    journal lastpage291
    identifier eissn1528-8900
    keywordsCascades (Fluid dynamics)
    keywordsBoundary layers
    keywordsDesign
    keywordsTurbines
    keywordsDatabases
    keywordsFlow (Dynamics)
    keywordsMeasurement
    keywordsAirfoils
    keywordsEngines
    keywordsThickness AND Mechanisms
    treeJournal of Turbomachinery:;2006:;volume( 128 ):;issue: 002
    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