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    A Design Calculation Procedure for Shock-Free or Strong Passage Shock Turbomachinery Cascades

    Source: Journal of Engineering for Gas Turbines and Power:;1983:;volume( 105 ):;issue: 002::page 369
    Author:
    Siu Shing Tong
    ,
    W. T. Thompkins
    DOI: 10.1115/1.3227425
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A previously described, inviscid design technique has been substantially improved to allow the generation of either shock-free, weak-shock or low total pressure loss supersonic rotor cascade designs. Improvements have been introduced in inflow-outflow boundary conditions, imposition of geometric constraints and in shock pressure rise specifications. Calculation examples are presented for precompression type rotor designs.
    keyword(s): Shock (Mechanics) , Design , Turbomachinery , Pressure , Rotors , Boundary-value problems , Cascades (Fluid dynamics) , Inflow AND Outflow ,
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      A Design Calculation Procedure for Shock-Free or Strong Passage Shock Turbomachinery Cascades

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/97109
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorSiu Shing Tong
    contributor authorW. T. Thompkins
    date accessioned2017-05-08T23:15:34Z
    date available2017-05-08T23:15:34Z
    date copyrightApril, 1983
    date issued1983
    identifier issn1528-8919
    identifier otherJETPEZ-26781#369_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/97109
    description abstractA previously described, inviscid design technique has been substantially improved to allow the generation of either shock-free, weak-shock or low total pressure loss supersonic rotor cascade designs. Improvements have been introduced in inflow-outflow boundary conditions, imposition of geometric constraints and in shock pressure rise specifications. Calculation examples are presented for precompression type rotor designs.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleA Design Calculation Procedure for Shock-Free or Strong Passage Shock Turbomachinery Cascades
    typeJournal Paper
    journal volume105
    journal issue2
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3227425
    journal fristpage369
    journal lastpage376
    identifier eissn0742-4795
    keywordsShock (Mechanics)
    keywordsDesign
    keywordsTurbomachinery
    keywordsPressure
    keywordsRotors
    keywordsBoundary-value problems
    keywordsCascades (Fluid dynamics)
    keywordsInflow AND Outflow
    treeJournal of Engineering for Gas Turbines and Power:;1983:;volume( 105 ):;issue: 002
    contenttypeFulltext
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