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    Boundary Layer Development on Turbine Airfoil Suction Surfaces

    Source: Journal of Engineering for Gas Turbines and Power:;1982:;volume( 104 ):;issue: 003::page 698
    Author:
    O. P. Sharma
    ,
    R. H. Schlinker
    ,
    D. A. Bailey
    ,
    R. A. Wells
    DOI: 10.1115/1.3227334
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents results of a study, supported by NASA Contract NAS3-20646 under the Energy Efficient Engine Program, conducted to investigate the development of boundary layers under the influence of velocity distributions simulating the suction sides of two state-of-the-art turbine airfoils. One velocity distribution represented a forward loaded airfoil (“squared-off” design) while the other represented an aft loaded airfoil (“aft loaded” design). These velocity distributions were simulated in a low-speed high aspect ratio wind tunnel specifically designed for boundary layer investigations. It is intended that the detailed data presented in this paper be used to develop an improved turbulence model suitable for application to turbine airfoil design.
    keyword(s): Suction , Boundary layers , Turbines , Airfoils , Design , Engines , Turbulence AND Wind tunnels ,
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      Boundary Layer Development on Turbine Airfoil Suction Surfaces

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/95775
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorO. P. Sharma
    contributor authorR. H. Schlinker
    contributor authorD. A. Bailey
    contributor authorR. A. Wells
    date accessioned2017-05-08T23:13:12Z
    date available2017-05-08T23:13:12Z
    date copyrightJuly, 1982
    date issued1982
    identifier issn1528-8919
    identifier otherJETPEZ-26776#698_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/95775
    description abstractThis paper presents results of a study, supported by NASA Contract NAS3-20646 under the Energy Efficient Engine Program, conducted to investigate the development of boundary layers under the influence of velocity distributions simulating the suction sides of two state-of-the-art turbine airfoils. One velocity distribution represented a forward loaded airfoil (“squared-off” design) while the other represented an aft loaded airfoil (“aft loaded” design). These velocity distributions were simulated in a low-speed high aspect ratio wind tunnel specifically designed for boundary layer investigations. It is intended that the detailed data presented in this paper be used to develop an improved turbulence model suitable for application to turbine airfoil design.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleBoundary Layer Development on Turbine Airfoil Suction Surfaces
    typeJournal Paper
    journal volume104
    journal issue3
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3227334
    journal fristpage698
    journal lastpage706
    identifier eissn0742-4795
    keywordsSuction
    keywordsBoundary layers
    keywordsTurbines
    keywordsAirfoils
    keywordsDesign
    keywordsEngines
    keywordsTurbulence AND Wind tunnels
    treeJournal of Engineering for Gas Turbines and Power:;1982:;volume( 104 ):;issue: 003
    contenttypeFulltext
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