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    Numerical Solution of Stream Function Equations in Transonic Flows

    Source: Journal of Turbomachinery:;1987:;volume( 109 ):;issue: 004::page 508
    Author:
    J. Z. Xu
    ,
    W. Y. Ni
    ,
    J. Y. Du
    DOI: 10.1115/1.3262140
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In order to develop the transonic stream function approach, in this paper one of the momentum equations is employed to form the principal equation of the stream function which does not contain vorticity and entropy terms, and the other one is used to calculate the density directly. Since the density is uniquely determined, the problem that the density is a double-valued function of mass flux in the stream function formulation disappears and the entropy increase across the shock is naturally included. The numerical results for the transonic cascade flow show that the shock obtained from the present method is slightly weaker and is placed farther downstream compared to the irrotational stream function calculation, and is closer to the experimental data. From a standpoint of computation the iterative procedure of this formulation is simple and the alternating use of two momentum equations makes the calculation more effective.
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      Numerical Solution of Stream Function Equations in Transonic Flows

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    http://yetl.yabesh.ir/yetl1/handle/yetl/103189
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    contributor authorJ. Z. Xu
    contributor authorW. Y. Ni
    contributor authorJ. Y. Du
    date accessioned2017-05-08T23:25:58Z
    date available2017-05-08T23:25:58Z
    date copyrightOctober, 1987
    date issued1987
    identifier issn0889-504X
    identifier otherJOTUEI-28586#508_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/103189
    description abstractIn order to develop the transonic stream function approach, in this paper one of the momentum equations is employed to form the principal equation of the stream function which does not contain vorticity and entropy terms, and the other one is used to calculate the density directly. Since the density is uniquely determined, the problem that the density is a double-valued function of mass flux in the stream function formulation disappears and the entropy increase across the shock is naturally included. The numerical results for the transonic cascade flow show that the shock obtained from the present method is slightly weaker and is placed farther downstream compared to the irrotational stream function calculation, and is closer to the experimental data. From a standpoint of computation the iterative procedure of this formulation is simple and the alternating use of two momentum equations makes the calculation more effective.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleNumerical Solution of Stream Function Equations in Transonic Flows
    typeJournal Paper
    journal volume109
    journal issue4
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.3262140
    journal fristpage508
    journal lastpage512
    identifier eissn1528-8900
    treeJournal of Turbomachinery:;1987:;volume( 109 ):;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
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