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    Improvements to the Ainley-Mathieson Method of Turbine Performance Prediction

    Source: Journal of Engineering for Gas Turbines and Power:;1970:;volume( 092 ):;issue: 003::page 252
    Author:
    J. Dunham
    ,
    P. M. Came
    DOI: 10.1115/1.3445349
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In 1951 Ainley and Mathieson published a method of predicting the design and off-design performance of an axial turbine (British ARC, R & M 2974). The flow and hence the losses were calculated at a single “reference diameter” for each blade row. This method has been widely used ever since. A critical review of the method has been made, based on detailed comparisons between the measured and predicted performance of a wide range of modern turbines. As a result, improvements have been made in the formulas for secondary loss and tip clearance loss prediction. The accuracy of the improved method has been assessed. Despite its relatively simple approach, it is believed that it will remain of great value in project work and preliminary design work.
    keyword(s): Turbines , Design , Blades , Formulas , Flow (Dynamics) AND Clearances (Engineering) ,
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      Improvements to the Ainley-Mathieson Method of Turbine Performance Prediction

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/142200
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorJ. Dunham
    contributor authorP. M. Came
    date accessioned2017-05-09T00:35:53Z
    date available2017-05-09T00:35:53Z
    date copyrightJuly, 1970
    date issued1970
    identifier issn1528-8919
    identifier otherJETPEZ-26687#252_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/142200
    description abstractIn 1951 Ainley and Mathieson published a method of predicting the design and off-design performance of an axial turbine (British ARC, R & M 2974). The flow and hence the losses were calculated at a single “reference diameter” for each blade row. This method has been widely used ever since. A critical review of the method has been made, based on detailed comparisons between the measured and predicted performance of a wide range of modern turbines. As a result, improvements have been made in the formulas for secondary loss and tip clearance loss prediction. The accuracy of the improved method has been assessed. Despite its relatively simple approach, it is believed that it will remain of great value in project work and preliminary design work.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleImprovements to the Ainley-Mathieson Method of Turbine Performance Prediction
    typeJournal Paper
    journal volume92
    journal issue3
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3445349
    journal fristpage252
    journal lastpage256
    identifier eissn0742-4795
    keywordsTurbines
    keywordsDesign
    keywordsBlades
    keywordsFormulas
    keywordsFlow (Dynamics) AND Clearances (Engineering)
    treeJournal of Engineering for Gas Turbines and Power:;1970:;volume( 092 ):;issue: 003
    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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