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    Laser Anemometer Measurements in a Transonic Axial Flow Compressor Rotor

    Source: Journal of Engineering for Gas Turbines and Power:;1981:;volume( 103 ):;issue: 002::page 430
    Author:
    A. J. Strazisar
    ,
    J. A. Powell
    DOI: 10.1115/1.3230738
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A laser anemometer system employing an efficient data acquisition technique has been used to make measurements upstream, within, and downstream of the compressor rotor. A fluorescent dye technique allowed measurements within endwall boundary layers. Adjustable laser beam orientation minimized shadowed regions and enabled radial velocity measurements outside of the blade row. The flow phenomena investigated include flow variations from passage to passage, the rotor shock system, three-dimensional flows in the blade wake, and the development of the outer endwall boundary layer. Laser anemometer measurements are compared to a numerical solution of the streamfunction equations and to measurements made with conventional instrumentation.
    keyword(s): Lasers , Measurement , Rotors , Axial flow , Flow (Dynamics) , Boundary layers , Blades , Equations , Velocity measurement , Data acquisition , Compressors , Laser beams , Wakes , Shock (Mechanics) AND Instrumentation ,
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      Laser Anemometer Measurements in a Transonic Axial Flow Compressor Rotor

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/94542
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorA. J. Strazisar
    contributor authorJ. A. Powell
    date accessioned2017-05-08T23:11:08Z
    date available2017-05-08T23:11:08Z
    date copyrightApril, 1981
    date issued1981
    identifier issn1528-8919
    identifier otherJETPEZ-26765#430_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/94542
    description abstractA laser anemometer system employing an efficient data acquisition technique has been used to make measurements upstream, within, and downstream of the compressor rotor. A fluorescent dye technique allowed measurements within endwall boundary layers. Adjustable laser beam orientation minimized shadowed regions and enabled radial velocity measurements outside of the blade row. The flow phenomena investigated include flow variations from passage to passage, the rotor shock system, three-dimensional flows in the blade wake, and the development of the outer endwall boundary layer. Laser anemometer measurements are compared to a numerical solution of the streamfunction equations and to measurements made with conventional instrumentation.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleLaser Anemometer Measurements in a Transonic Axial Flow Compressor Rotor
    typeJournal Paper
    journal volume103
    journal issue2
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3230738
    journal fristpage430
    journal lastpage437
    identifier eissn0742-4795
    keywordsLasers
    keywordsMeasurement
    keywordsRotors
    keywordsAxial flow
    keywordsFlow (Dynamics)
    keywordsBoundary layers
    keywordsBlades
    keywordsEquations
    keywordsVelocity measurement
    keywordsData acquisition
    keywordsCompressors
    keywordsLaser beams
    keywordsWakes
    keywordsShock (Mechanics) AND Instrumentation
    treeJournal of Engineering for Gas Turbines and Power:;1981:;volume( 103 ):;issue: 002
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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