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    Refinement of Cross‐Flow Turbine Design Parameters

    Source: Journal of Energy Engineering:;1994:;Volume ( 120 ):;issue: 003
    Author:
    Hara G. S. Totapally
    ,
    Nadim M. Aziz
    DOI: 10.1061/(ASCE)0733-9402(1994)120:3(133)
    Publisher: American Society of Civil Engineers
    Abstract: This paper discusses experiments that were conducted to refine some of the key cross‐flow turbine runner parameters for better performance. The parameters studied were identified by previous studies as key design parameters. The research included narrowing the range of the number of blades, the determination of the impact of the first‐stage exit angle, and the effect of flow stream spreading on the performance of the cross‐flow turbine. The results indicate an optimum number of blades that would produce maximum efficiency of the turbine, and a clear trend of the effect of the first‐stage exit angle and flow stream spreading on the efficiency. For the best nozzle‐runner combination, the maximum efficiency closest to the discharge averaged maximum efficiency is determined to be 92%, with an uncertainty of ±2.4%. This result is an improvement over the reported maximum efficiency of any cross‐flow turbine.
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      Refinement of Cross‐Flow Turbine Design Parameters

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/77677
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    • Journal of Energy Engineering

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    contributor authorHara G. S. Totapally
    contributor authorNadim M. Aziz
    date accessioned2017-05-08T22:19:30Z
    date available2017-05-08T22:19:30Z
    date copyrightDecember 1994
    date issued1994
    identifier other41215283.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/77677
    description abstractThis paper discusses experiments that were conducted to refine some of the key cross‐flow turbine runner parameters for better performance. The parameters studied were identified by previous studies as key design parameters. The research included narrowing the range of the number of blades, the determination of the impact of the first‐stage exit angle, and the effect of flow stream spreading on the performance of the cross‐flow turbine. The results indicate an optimum number of blades that would produce maximum efficiency of the turbine, and a clear trend of the effect of the first‐stage exit angle and flow stream spreading on the efficiency. For the best nozzle‐runner combination, the maximum efficiency closest to the discharge averaged maximum efficiency is determined to be 92%, with an uncertainty of ±2.4%. This result is an improvement over the reported maximum efficiency of any cross‐flow turbine.
    publisherAmerican Society of Civil Engineers
    titleRefinement of Cross‐Flow Turbine Design Parameters
    typeJournal Paper
    journal volume120
    journal issue3
    journal titleJournal of Energy Engineering
    identifier doi10.1061/(ASCE)0733-9402(1994)120:3(133)
    treeJournal of Energy Engineering:;1994:;Volume ( 120 ):;issue: 003
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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