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    Wall Stall in Compressor Cascades

    Source: Journal of Fluids Engineering:;1966:;volume( 088 ):;issue: 003::page 637
    Author:
    J. H. Horlock
    ,
    J. F. Louis
    ,
    P. M. E. Percival
    ,
    B. Lakshminarayana
    DOI: 10.1115/1.3645925
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The “wall stall” in compressor cascades has been observed by many research workers. There is a region of high loss in the corner bounded by the end wall and the suction surface of a blade. It is the separation of the flow in this region which is largely responsible for the increase in the axial velocity across the midspan section of the blades when there is no end-wall suction. It is important to differentiate between this wall stall and the two-dimensional stall of the blading. The work on wall stall described in the paper was carried out at the University of Cambridge and the University of Liverpool in the period 1955-1962.
    keyword(s): Compressors , Suction , Blades , Corners (Structural elements) , Flow (Dynamics) AND Separation (Technology) ,
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      Wall Stall in Compressor Cascades

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/113201
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    • Journal of Fluids Engineering

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    contributor authorJ. H. Horlock
    contributor authorJ. F. Louis
    contributor authorP. M. E. Percival
    contributor authorB. Lakshminarayana
    date accessioned2017-05-08T23:43:31Z
    date available2017-05-08T23:43:31Z
    date copyrightSeptember, 1966
    date issued1966
    identifier issn0098-2202
    identifier otherJFEGA4-27283#637_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/113201
    description abstractThe “wall stall” in compressor cascades has been observed by many research workers. There is a region of high loss in the corner bounded by the end wall and the suction surface of a blade. It is the separation of the flow in this region which is largely responsible for the increase in the axial velocity across the midspan section of the blades when there is no end-wall suction. It is important to differentiate between this wall stall and the two-dimensional stall of the blading. The work on wall stall described in the paper was carried out at the University of Cambridge and the University of Liverpool in the period 1955-1962.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleWall Stall in Compressor Cascades
    typeJournal Paper
    journal volume88
    journal issue3
    journal titleJournal of Fluids Engineering
    identifier doi10.1115/1.3645925
    journal fristpage637
    journal lastpage648
    identifier eissn1528-901X
    keywordsCompressors
    keywordsSuction
    keywordsBlades
    keywordsCorners (Structural elements)
    keywordsFlow (Dynamics) AND Separation (Technology)
    treeJournal of Fluids Engineering:;1966:;volume( 088 ):;issue: 003
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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