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    A Method for Transonic Inverse Cascade Design With a Stream Function Equation

    Source: Journal of Turbomachinery:;1986:;volume( 108 ):;issue: 002::page 200
    Author:
    Manchu Ge
    ,
    Yiping Lou
    ,
    Zhengti Yu
    DOI: 10.1115/1.3262038
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A new profile design method is developed on the basis of [1–3] for transonic flow. The rotational dynamic stream function equation, which is expressed in functional form using calculated coordinates, is deduced. This method can be used for the calculation of cascade and S1 stream surface of a transonic flow with a local shock wave on the blade suction surface. This method consists of two parts: an inverse method with a given velocity distribution along the suction surface and a given thickness distribution; and an inverse method with given velocity distributions on suction and pressure surfaces. Using this method it is easy to obtain a blade profile with prescribed velocity and thickness distributions. The design of optimal profile may then be done with the calculated optimal velocity distribution on the blade surface. The rotational condition is satisfied when the stream function equation is adopted with the entropy term. If the compatibility condition can be fulfilled between the S1 and S2 equations, the iterative calculations of two kinds of stream surfaces in three-dimensional flow will be convergent. In this paper a unique value of density can be determined from the known stream function value. The computational program is written with this method and several transonic examples have been calculated. These results are quite good.
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      A Method for Transonic Inverse Cascade Design With a Stream Function Equation

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/101828
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    contributor authorManchu Ge
    contributor authorYiping Lou
    contributor authorZhengti Yu
    date accessioned2017-05-08T23:23:40Z
    date available2017-05-08T23:23:40Z
    date copyrightOctober, 1986
    date issued1986
    identifier issn0889-504X
    identifier otherJOTUEI-28578#200_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/101828
    description abstractA new profile design method is developed on the basis of [1–3] for transonic flow. The rotational dynamic stream function equation, which is expressed in functional form using calculated coordinates, is deduced. This method can be used for the calculation of cascade and S1 stream surface of a transonic flow with a local shock wave on the blade suction surface. This method consists of two parts: an inverse method with a given velocity distribution along the suction surface and a given thickness distribution; and an inverse method with given velocity distributions on suction and pressure surfaces. Using this method it is easy to obtain a blade profile with prescribed velocity and thickness distributions. The design of optimal profile may then be done with the calculated optimal velocity distribution on the blade surface. The rotational condition is satisfied when the stream function equation is adopted with the entropy term. If the compatibility condition can be fulfilled between the S1 and S2 equations, the iterative calculations of two kinds of stream surfaces in three-dimensional flow will be convergent. In this paper a unique value of density can be determined from the known stream function value. The computational program is written with this method and several transonic examples have been calculated. These results are quite good.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleA Method for Transonic Inverse Cascade Design With a Stream Function Equation
    typeJournal Paper
    journal volume108
    journal issue2
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.3262038
    journal fristpage200
    journal lastpage205
    identifier eissn1528-8900
    treeJournal of Turbomachinery:;1986:;volume( 108 ):;issue: 002
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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