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    Influence of Leading-Edge Geometry on Profile Losses in Turbines at Off-Design Incidence: Experimental Results and an Improved Correlation

    Source: Journal of Turbomachinery:;1997:;volume( 119 ):;issue: 002::page 193
    Author:
    M. W. Benner
    ,
    S. H. Moustapha
    ,
    S. A. Sjolander
    DOI: 10.1115/1.2841101
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The most recent correlations for turbine profile losses at off-design incidence include the leading-edge diameter as the only aspect of the leading-edge geometry that influences the losses. Cascade measurements are presented for two turbine blades that differ primarily in their leading-edge geometries. The incidence was varied over a range of ±20 deg and the results show significant discrepancies between the observed profile losses and those predicted by the available correlations. Using data from the present experiments, as well as cases from the literature for which sufficient geometric data are given, a revised correlation has been developed. The new correlation is a function of both the leading-edge diameter and the wedge angle, and it is significantly more successful than the existing correlations. It is argued that the off-design loss behavior of the blade is influenced by the magnitude of the discontinuity in curvature at the points where the leading-edge circle meets the rest of the blade profile. The wedge angle appears to be an approximate and convenient measure of the discontinuity in curvature at these blend points.
    keyword(s): Design , Turbines , Geometry , Wedges , Blades , Measurement , Turbine blades AND Cascades (Fluid dynamics) ,
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      Influence of Leading-Edge Geometry on Profile Losses in Turbines at Off-Design Incidence: Experimental Results and an Improved Correlation

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/119625
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    contributor authorM. W. Benner
    contributor authorS. H. Moustapha
    contributor authorS. A. Sjolander
    date accessioned2017-05-08T23:55:09Z
    date available2017-05-08T23:55:09Z
    date copyrightApril, 1997
    date issued1997
    identifier issn0889-504X
    identifier otherJOTUEI-28659#193_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/119625
    description abstractThe most recent correlations for turbine profile losses at off-design incidence include the leading-edge diameter as the only aspect of the leading-edge geometry that influences the losses. Cascade measurements are presented for two turbine blades that differ primarily in their leading-edge geometries. The incidence was varied over a range of ±20 deg and the results show significant discrepancies between the observed profile losses and those predicted by the available correlations. Using data from the present experiments, as well as cases from the literature for which sufficient geometric data are given, a revised correlation has been developed. The new correlation is a function of both the leading-edge diameter and the wedge angle, and it is significantly more successful than the existing correlations. It is argued that the off-design loss behavior of the blade is influenced by the magnitude of the discontinuity in curvature at the points where the leading-edge circle meets the rest of the blade profile. The wedge angle appears to be an approximate and convenient measure of the discontinuity in curvature at these blend points.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleInfluence of Leading-Edge Geometry on Profile Losses in Turbines at Off-Design Incidence: Experimental Results and an Improved Correlation
    typeJournal Paper
    journal volume119
    journal issue2
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2841101
    journal fristpage193
    journal lastpage200
    identifier eissn1528-8900
    keywordsDesign
    keywordsTurbines
    keywordsGeometry
    keywordsWedges
    keywordsBlades
    keywordsMeasurement
    keywordsTurbine blades AND Cascades (Fluid dynamics)
    treeJournal of Turbomachinery:;1997:;volume( 119 ):;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
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