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    The Transonic Flow Through a Plane Turbine Cascade as Measured in Four European Wind Tunnels

    Source: Journal of Engineering for Gas Turbines and Power:;1986:;volume( 108 ):;issue: 002::page 277
    Author:
    R. Kiock
    ,
    F. Lehthaus
    ,
    N. C. Baines
    ,
    C. H. Sieverding
    DOI: 10.1115/1.3239900
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Reliable cascade data are esssential to the development of high-speed turbomachinery, but it has long been suspected that the tunnel environment influences the test results. This has now been investigated by testing one plane gas turbine rotor blade section in four European wind tunnels of different test sections and instrumentation. The Reynolds number of the transonic flow tests was Re2 = 8 × 105 based on exit flow conditions. The turbulence was not increased artificially. A comparison of results from blade pressure distributions and wake traverse measurements reveals the order of magnitude of tunnel effects.
    keyword(s): Cascades (Fluid dynamics) , Turbines , Transonic flow , Wind tunnels , Tunnels , Blades , Turbomachinery , Wakes , Gas turbines , Instrumentation , Rotors , Testing , Pressure , Flow (Dynamics) , Measurement , Turbulence AND Reynolds number ,
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      The Transonic Flow Through a Plane Turbine Cascade as Measured in Four European Wind Tunnels

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/101122
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorR. Kiock
    contributor authorF. Lehthaus
    contributor authorN. C. Baines
    contributor authorC. H. Sieverding
    date accessioned2017-05-08T23:22:27Z
    date available2017-05-08T23:22:27Z
    date copyrightApril, 1986
    date issued1986
    identifier issn1528-8919
    identifier otherJETPEZ-26634#277_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/101122
    description abstractReliable cascade data are esssential to the development of high-speed turbomachinery, but it has long been suspected that the tunnel environment influences the test results. This has now been investigated by testing one plane gas turbine rotor blade section in four European wind tunnels of different test sections and instrumentation. The Reynolds number of the transonic flow tests was Re2 = 8 × 105 based on exit flow conditions. The turbulence was not increased artificially. A comparison of results from blade pressure distributions and wake traverse measurements reveals the order of magnitude of tunnel effects.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleThe Transonic Flow Through a Plane Turbine Cascade as Measured in Four European Wind Tunnels
    typeJournal Paper
    journal volume108
    journal issue2
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3239900
    journal fristpage277
    journal lastpage284
    identifier eissn0742-4795
    keywordsCascades (Fluid dynamics)
    keywordsTurbines
    keywordsTransonic flow
    keywordsWind tunnels
    keywordsTunnels
    keywordsBlades
    keywordsTurbomachinery
    keywordsWakes
    keywordsGas turbines
    keywordsInstrumentation
    keywordsRotors
    keywordsTesting
    keywordsPressure
    keywordsFlow (Dynamics)
    keywordsMeasurement
    keywordsTurbulence AND Reynolds number
    treeJournal of Engineering for Gas Turbines and Power:;1986:;volume( 108 ):;issue: 002
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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