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    A New Technique for Stabilizing the Flow and Improving the Performance of Vaneless Radial Diffusers

    Source: Journal of Turbomachinery:;1987:;volume( 109 ):;issue: 001::page 36
    Author:
    A. N. Abdel-Hamid
    DOI: 10.1115/1.3262067
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Experiments were conducted to investigate the effects of using small exit vanes on the characteristics of an otherwise vaneless radial diffuser of outer radius and width-to-inlet radius ratios of 1.75 and 0.116, respectively. The steady and unsteady characteristics of the diffuser were evaluated as the angle of the vanes was varied continuously at several diffuser inlet conditions. The measurements showed that the influence of the adjustable exit vanes on the diffuser flow field increased as the diffuser inlet flow angle was decreased. Elimination of the self-excited flow oscillations in the diffuser was possible for all operating conditions by appropriate setting of the exit vane angle. Moreover for the diffuser investigated here and with optimum setting of the exit vanes angle the static pressure rise coefficient was significantly improved compared to the case of a pure vaneless diffuser and was found to remain almost constant at low values of diffuser inlet angles. Relative to other techniques for controlling flow instability in vaneless diffusers the proposed method offers mechanical simplicity and improved overall performance.
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      A New Technique for Stabilizing the Flow and Improving the Performance of Vaneless Radial Diffusers

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/103261
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    • Journal of Turbomachinery

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    contributor authorA. N. Abdel-Hamid
    date accessioned2017-05-08T23:26:06Z
    date available2017-05-08T23:26:06Z
    date copyrightJanuary, 1987
    date issued1987
    identifier issn0889-504X
    identifier otherJOTUEI-28581#36_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/103261
    description abstractExperiments were conducted to investigate the effects of using small exit vanes on the characteristics of an otherwise vaneless radial diffuser of outer radius and width-to-inlet radius ratios of 1.75 and 0.116, respectively. The steady and unsteady characteristics of the diffuser were evaluated as the angle of the vanes was varied continuously at several diffuser inlet conditions. The measurements showed that the influence of the adjustable exit vanes on the diffuser flow field increased as the diffuser inlet flow angle was decreased. Elimination of the self-excited flow oscillations in the diffuser was possible for all operating conditions by appropriate setting of the exit vane angle. Moreover for the diffuser investigated here and with optimum setting of the exit vanes angle the static pressure rise coefficient was significantly improved compared to the case of a pure vaneless diffuser and was found to remain almost constant at low values of diffuser inlet angles. Relative to other techniques for controlling flow instability in vaneless diffusers the proposed method offers mechanical simplicity and improved overall performance.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleA New Technique for Stabilizing the Flow and Improving the Performance of Vaneless Radial Diffusers
    typeJournal Paper
    journal volume109
    journal issue1
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.3262067
    journal fristpage36
    journal lastpage40
    identifier eissn1528-8900
    treeJournal of Turbomachinery:;1987:;volume( 109 ):;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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