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    Eigensolutions of Grouped Turbo Blades Solved by the Generalized Differential Quadrature Method

    Source: Journal of Engineering for Gas Turbines and Power:;2002:;volume( 124 ):;issue: 004::page 1011
    Author:
    J. H. Kuang
    ,
    M. H. Hsu
    DOI: 10.1115/1.1492833
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The eigenvalue problems of grouped turbo blades were numerically formulated by using the generalized differential quadrature method (GDQM). Different boundary approaches accompanying the GDQM to transform the partial differential equations of grouped turbo blades into a discrete eigenvalue problem are discussed. Effects of the number of sample points and the different boundary approaches on the accuracy of the calculated natural frequencies are also studied. Numerical results demonstrated the validity and the efficiency of the GDQM in treating this type of problem.
    keyword(s): Blades , Eigenvalues AND Frequency ,
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      Eigensolutions of Grouped Turbo Blades Solved by the Generalized Differential Quadrature Method

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/126720
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorJ. H. Kuang
    contributor authorM. H. Hsu
    date accessioned2017-05-09T00:07:24Z
    date available2017-05-09T00:07:24Z
    date copyrightOctober, 2002
    date issued2002
    identifier issn1528-8919
    identifier otherJETPEZ-26816#1011_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/126720
    description abstractThe eigenvalue problems of grouped turbo blades were numerically formulated by using the generalized differential quadrature method (GDQM). Different boundary approaches accompanying the GDQM to transform the partial differential equations of grouped turbo blades into a discrete eigenvalue problem are discussed. Effects of the number of sample points and the different boundary approaches on the accuracy of the calculated natural frequencies are also studied. Numerical results demonstrated the validity and the efficiency of the GDQM in treating this type of problem.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleEigensolutions of Grouped Turbo Blades Solved by the Generalized Differential Quadrature Method
    typeJournal Paper
    journal volume124
    journal issue4
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.1492833
    journal fristpage1011
    journal lastpage1017
    identifier eissn0742-4795
    keywordsBlades
    keywordsEigenvalues AND Frequency
    treeJournal of Engineering for Gas Turbines and Power:;2002:;volume( 124 ):;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
    yabeshDSpacePersian