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    Loss and Flow Path Studies on Centrifugal Compressors—Part II

    Source: Journal of Engineering for Gas Turbines and Power:;1970:;volume( 092 ):;issue: 003::page 287
    Author:
    O. E. Baljé
    DOI: 10.1115/1.3445353
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The flow conditions in a mixed flow rotor are investigated for a “pressure balanced” flow path design. Boundary layer arguments are applied to calculate the losses in the rotor as well as in the subsequent diffuser section. The resulting efficiency data imply a comparatively high efficiency potential for mixed flow compressors with multiple cascaded components, designed on the premise of a “pressure balanced” rotor flow path.
    keyword(s): Flow (Dynamics) , Compressors , Rotors , Pressure , Diffusers , Boundary layers AND Design ,
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      Loss and Flow Path Studies on Centrifugal Compressors—Part II

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    https://yetl.yabesh.ir/yetl1/handle/yetl/142244
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorO. E. Baljé
    date accessioned2017-05-09T00:35:57Z
    date available2017-05-09T00:35:57Z
    date copyrightJuly, 1970
    date issued1970
    identifier issn1528-8919
    identifier otherJETPEZ-26687#287_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/142244
    description abstractThe flow conditions in a mixed flow rotor are investigated for a “pressure balanced” flow path design. Boundary layer arguments are applied to calculate the losses in the rotor as well as in the subsequent diffuser section. The resulting efficiency data imply a comparatively high efficiency potential for mixed flow compressors with multiple cascaded components, designed on the premise of a “pressure balanced” rotor flow path.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleLoss and Flow Path Studies on Centrifugal Compressors—Part II
    typeJournal Paper
    journal volume92
    journal issue3
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3445353
    journal fristpage287
    journal lastpage300
    identifier eissn0742-4795
    keywordsFlow (Dynamics)
    keywordsCompressors
    keywordsRotors
    keywordsPressure
    keywordsDiffusers
    keywordsBoundary layers AND Design
    treeJournal of Engineering for Gas Turbines and Power:;1970:;volume( 092 ):;issue: 003
    contenttypeFulltext
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