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    Design of Curved Annular Diffusers II: Using Splitter Blades

    Source: Journal of Engineering for Gas Turbines and Power:;2022:;volume( 144 ):;issue: 008::page 85001-1
    Author:
    Kuchana
    ,
    Vinayender;Balakrishnan
    ,
    N.;Srinivasan
    ,
    Balamurugan
    DOI: 10.1115/1.4054580
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The use of splitter blade as a passive flow control mechanism in the design of separation free aggressive annular diffuser is explored through computational fluid dynamics simulations. The fundamental working principle of a splitter blade in case of a two-dimensional rectangular diffuser and an annular diffuser is discussed. The effects of splitter blade configuration on the end-wall adverse pressure gradients are discussed. An aggressive diffuser design space is identified with ducts of maximum slope of 50 deg and maximum divergence angle between the outer and inner walls of 10 deg for axial-length to inlet height ratio ranging from 1.25 to 2.5. One or more splitter blades are employed in the duct to eliminate flow separation for all the ducts in the aggressive design space considered. Requirement of number of splitter blades in the aggressive design space is demarcated. Performance charts for the ducts in this aggressive design space are also established.
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      Design of Curved Annular Diffusers II: Using Splitter Blades

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/4287174
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorKuchana
    contributor authorVinayender;Balakrishnan
    contributor authorN.;Srinivasan
    contributor authorBalamurugan
    date accessioned2022-08-18T12:57:42Z
    date available2022-08-18T12:57:42Z
    date copyright6/2/2022 12:00:00 AM
    date issued2022
    identifier issn0742-4795
    identifier othergtp_144_08_085001.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4287174
    description abstractThe use of splitter blade as a passive flow control mechanism in the design of separation free aggressive annular diffuser is explored through computational fluid dynamics simulations. The fundamental working principle of a splitter blade in case of a two-dimensional rectangular diffuser and an annular diffuser is discussed. The effects of splitter blade configuration on the end-wall adverse pressure gradients are discussed. An aggressive diffuser design space is identified with ducts of maximum slope of 50 deg and maximum divergence angle between the outer and inner walls of 10 deg for axial-length to inlet height ratio ranging from 1.25 to 2.5. One or more splitter blades are employed in the duct to eliminate flow separation for all the ducts in the aggressive design space considered. Requirement of number of splitter blades in the aggressive design space is demarcated. Performance charts for the ducts in this aggressive design space are also established.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleDesign of Curved Annular Diffusers II: Using Splitter Blades
    typeJournal Paper
    journal volume144
    journal issue8
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4054580
    journal fristpage85001-1
    journal lastpage85001-17
    page17
    treeJournal of Engineering for Gas Turbines and Power:;2022:;volume( 144 ):;issue: 008
    contenttypeFulltext
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