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    The Effects of Some Design Parameters of an Isolated Rotor on Inlet Flow Distortions

    Source: Journal of Engineering for Gas Turbines and Power:;1980:;volume( 102 ):;issue: 001::page 178
    Author:
    A. M. Yocum
    ,
    R. E. Henderson
    DOI: 10.1115/1.3230219
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A study of the effects of rotor-blade geometry, steady loading, and distortion wavelength on the distortion flow field upstream and downstream of an unstalled isolated rotor shows that the attenuation of the distortion as it passes through the rotor is a function of the blade stagger angle and the distortion-reduced frequency or the ratio of rotor blade spacing to the distortion wavelength s/l . Maximum attenuation occurs when s/l = 0.5 and increases with increasing stagger angle. Little influence of rotor incidence angle or steady loading was observed.
    keyword(s): Design , Rotors , Flow (Dynamics) , Blades , Wavelength AND Geometry ,
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      The Effects of Some Design Parameters of an Isolated Rotor on Inlet Flow Distortions

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/93336
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorA. M. Yocum
    contributor authorR. E. Henderson
    date accessioned2017-05-08T23:08:48Z
    date available2017-05-08T23:08:48Z
    date copyrightJanuary, 1980
    date issued1980
    identifier issn1528-8919
    identifier otherJETPEZ-26754#178_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/93336
    description abstractA study of the effects of rotor-blade geometry, steady loading, and distortion wavelength on the distortion flow field upstream and downstream of an unstalled isolated rotor shows that the attenuation of the distortion as it passes through the rotor is a function of the blade stagger angle and the distortion-reduced frequency or the ratio of rotor blade spacing to the distortion wavelength s/l . Maximum attenuation occurs when s/l = 0.5 and increases with increasing stagger angle. Little influence of rotor incidence angle or steady loading was observed.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleThe Effects of Some Design Parameters of an Isolated Rotor on Inlet Flow Distortions
    typeJournal Paper
    journal volume102
    journal issue1
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3230219
    journal fristpage178
    journal lastpage186
    identifier eissn0742-4795
    keywordsDesign
    keywordsRotors
    keywordsFlow (Dynamics)
    keywordsBlades
    keywordsWavelength AND Geometry
    treeJournal of Engineering for Gas Turbines and Power:;1980:;volume( 102 ):;issue: 001
    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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