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    Development of an Experimental Correlation for Transonic Turbine Flow

    Source: Journal of Turbomachinery:;1987:;volume( 109 ):;issue: 002::page 246
    Author:
    F. Martelli
    ,
    A. Boretti
    DOI: 10.1115/1.3262092
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Optimization of transonic turbine bladings over a broad range of operating conditions calls for better understanding of the relationship between blade profile loss and cascade geometric parameters. In fact, many of the experimental correlations published to date have failed to take into due consideration transonic effects, while others have considered far too few of the numerous geometric parameters affecting profile loss in transonic flows. Through examination of the experimental data gathered by some 20 authors regarding the effects of the most significant blading geometric parameters on profile losses, a loss correlation procedure has been developed. The procedure is especially advantageous in that it allows continuous updating as new experimental data become available.
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      Development of an Experimental Correlation for Transonic Turbine Flow

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    contributor authorF. Martelli
    contributor authorA. Boretti
    date accessioned2017-05-08T23:26:04Z
    date available2017-05-08T23:26:04Z
    date copyrightApril, 1987
    date issued1987
    identifier issn0889-504X
    identifier otherJOTUEI-28583#246_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/103246
    description abstractOptimization of transonic turbine bladings over a broad range of operating conditions calls for better understanding of the relationship between blade profile loss and cascade geometric parameters. In fact, many of the experimental correlations published to date have failed to take into due consideration transonic effects, while others have considered far too few of the numerous geometric parameters affecting profile loss in transonic flows. Through examination of the experimental data gathered by some 20 authors regarding the effects of the most significant blading geometric parameters on profile losses, a loss correlation procedure has been developed. The procedure is especially advantageous in that it allows continuous updating as new experimental data become available.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleDevelopment of an Experimental Correlation for Transonic Turbine Flow
    typeJournal Paper
    journal volume109
    journal issue2
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.3262092
    journal fristpage246
    journal lastpage250
    identifier eissn1528-8900
    treeJournal of Turbomachinery:;1987:;volume( 109 ):;issue: 002
    contenttypeFulltext
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