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    Numerical Solutions for Unsteady Subsonic Vortical Flows Around Loaded Cascades

    Source: Journal of Turbomachinery:;1993:;volume( 115 ):;issue: 004::page 810
    Author:
    J. Fang
    ,
    H. M. Atassi
    DOI: 10.1115/1.2929319
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A frequency domain linearized unsteady aerodynamic analysis is presented for three-dimensional unsteady vortical flows around a cascade of loaded airfoils. The analysis fully accounts for the distortion of the impinging vortical disturbances by the mean flow. The entire unsteady flow field is calculated in response to upstream three-dimensional harmonic disturbances. Numerical results are presented for two standard cascade configurations representing turbine and compressor bladings for a reduced frequency range from 0.1 to 5. Results show that the upstream gust conditions and blade sweep strongly affect the unsteady blade response.
    keyword(s): Vortex flow , Blades , Cascades (Fluid dynamics) , Turbines , Flow (Dynamics) , Compressors , Unsteady flow AND Airfoils ,
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      Numerical Solutions for Unsteady Subsonic Vortical Flows Around Loaded Cascades

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/112769
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    • Journal of Turbomachinery

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    contributor authorJ. Fang
    contributor authorH. M. Atassi
    date accessioned2017-05-08T23:42:48Z
    date available2017-05-08T23:42:48Z
    date copyrightOctober, 1993
    date issued1993
    identifier issn0889-504X
    identifier otherJOTUEI-28633#810_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/112769
    description abstractA frequency domain linearized unsteady aerodynamic analysis is presented for three-dimensional unsteady vortical flows around a cascade of loaded airfoils. The analysis fully accounts for the distortion of the impinging vortical disturbances by the mean flow. The entire unsteady flow field is calculated in response to upstream three-dimensional harmonic disturbances. Numerical results are presented for two standard cascade configurations representing turbine and compressor bladings for a reduced frequency range from 0.1 to 5. Results show that the upstream gust conditions and blade sweep strongly affect the unsteady blade response.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleNumerical Solutions for Unsteady Subsonic Vortical Flows Around Loaded Cascades
    typeJournal Paper
    journal volume115
    journal issue4
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.2929319
    journal fristpage810
    journal lastpage816
    identifier eissn1528-8900
    keywordsVortex flow
    keywordsBlades
    keywordsCascades (Fluid dynamics)
    keywordsTurbines
    keywordsFlow (Dynamics)
    keywordsCompressors
    keywordsUnsteady flow AND Airfoils
    treeJournal of Turbomachinery:;1993:;volume( 115 ):;issue: 004
    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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