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    Performance Analysis of the Test Results on a Two-Stage Transonic Fan

    Source: Journal of Engineering for Gas Turbines and Power:;1983:;volume( 105 ):;issue: 001::page 125
    Author:
    Baoshi Chen
    ,
    Tianyi Zhang
    DOI: 10.1115/1.3227372
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Test results obtained from a two-stage fan are analysed and the reasons that caused the design performance target not to be attained are presented in this paper. Addition of a partspan shroud on rotor 1 caused higher losses and changed radial distribution of parameters. Modification on the flowpath and chord length of stator 1 resulted in excessively high inlet Mach number and flow separation in the hub region. The high load and high incidence at the hub of rotor 2 caused higher losses and reduced stall margin of the fan.
    keyword(s): Mach number , Stress , Chords (Trusses) , Design , Rotors , Flow separation AND Stators ,
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      Performance Analysis of the Test Results on a Two-Stage Transonic Fan

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    http://yetl.yabesh.ir/yetl1/handle/yetl/97135
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorBaoshi Chen
    contributor authorTianyi Zhang
    date accessioned2017-05-08T23:15:37Z
    date available2017-05-08T23:15:37Z
    date copyrightJanuary, 1983
    date issued1983
    identifier issn1528-8919
    identifier otherJETPEZ-26779#125_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/97135
    description abstractTest results obtained from a two-stage fan are analysed and the reasons that caused the design performance target not to be attained are presented in this paper. Addition of a partspan shroud on rotor 1 caused higher losses and changed radial distribution of parameters. Modification on the flowpath and chord length of stator 1 resulted in excessively high inlet Mach number and flow separation in the hub region. The high load and high incidence at the hub of rotor 2 caused higher losses and reduced stall margin of the fan.
    publisherThe American Society of Mechanical Engineers (ASME)
    titlePerformance Analysis of the Test Results on a Two-Stage Transonic Fan
    typeJournal Paper
    journal volume105
    journal issue1
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3227372
    journal fristpage125
    journal lastpage129
    identifier eissn0742-4795
    keywordsMach number
    keywordsStress
    keywordsChords (Trusses)
    keywordsDesign
    keywordsRotors
    keywordsFlow separation AND Stators
    treeJournal of Engineering for Gas Turbines and Power:;1983:;volume( 105 ):;issue: 001
    contenttypeFulltext
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