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    Efficient Laser Anemometer for Intra-Rotor Flow Mapping in Turbomachinery

    Source: Journal of Engineering for Gas Turbines and Power:;1981:;volume( 103 ):;issue: 002::page 424
    Author:
    J. A. Powell
    ,
    A. J. Strazisar
    ,
    R. G. Seasholtz
    DOI: 10.1115/1.3230737
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Innovative features of the anemometer include: (1) a rapid and efficient data acquisition process, (2) a detailed real-time graphic display of the data being accumulated, and (3) input laser beam positioning that maximizes the size of the intra-rotor region being mapped. Results are presented that demonstrate the anemometer’s capability in flow mapping within a transonic axial-flow compressor rotor. Typically, a velocity profile, derived from 30,000 measurements along 1000 sequential circumferential positions covering 20 blade passages, can be obtained in 30 s. The use of fluorescent seed particles allows flow measurements near the rotor hub and the casing window.
    keyword(s): Flow (Dynamics) , Lasers , Rotors , Turbomachinery , Data acquisition , Axial flow , Blades , Flow measurement , Measurement , Particulate matter , Compressors AND Laser beams ,
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      Efficient Laser Anemometer for Intra-Rotor Flow Mapping in Turbomachinery

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/94541
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorJ. A. Powell
    contributor authorA. J. Strazisar
    contributor authorR. G. Seasholtz
    date accessioned2017-05-08T23:11:08Z
    date available2017-05-08T23:11:08Z
    date copyrightApril, 1981
    date issued1981
    identifier issn1528-8919
    identifier otherJETPEZ-26765#424_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/94541
    description abstractInnovative features of the anemometer include: (1) a rapid and efficient data acquisition process, (2) a detailed real-time graphic display of the data being accumulated, and (3) input laser beam positioning that maximizes the size of the intra-rotor region being mapped. Results are presented that demonstrate the anemometer’s capability in flow mapping within a transonic axial-flow compressor rotor. Typically, a velocity profile, derived from 30,000 measurements along 1000 sequential circumferential positions covering 20 blade passages, can be obtained in 30 s. The use of fluorescent seed particles allows flow measurements near the rotor hub and the casing window.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleEfficient Laser Anemometer for Intra-Rotor Flow Mapping in Turbomachinery
    typeJournal Paper
    journal volume103
    journal issue2
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3230737
    journal fristpage424
    journal lastpage429
    identifier eissn0742-4795
    keywordsFlow (Dynamics)
    keywordsLasers
    keywordsRotors
    keywordsTurbomachinery
    keywordsData acquisition
    keywordsAxial flow
    keywordsBlades
    keywordsFlow measurement
    keywordsMeasurement
    keywordsParticulate matter
    keywordsCompressors AND Laser beams
    treeJournal of Engineering for Gas Turbines and Power:;1981:;volume( 103 ):;issue: 002
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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