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    Investigation of Nonaxisymmetric Endwall Contouring and Three Dimensional Airfoil Design in a 1.5 Stage Axial Turbine—Part I: Design and Novel Numerical Analysis Method

    Source: Journal of Turbomachinery:;2015:;volume( 137 ):;issue: 008::page 81009
    Author:
    Poehler, Thorsten
    ,
    Niewoehner, Jens
    ,
    Jeschke, Peter
    ,
    Guendogdu, Yavuz
    DOI: 10.1115/1.4029476
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents the results of the analysis of different 3D designs for the first stator and the rotor of a 1.5stage turbine test rig. A tangential endwall contouring for the hub and the shroud, a bowed profile stacking, and a combination of those have been designed for the first stator. In addition, a tangential endwall contouring has been designed for the hub of the unshrouded rotor. Part I of this twopart paper deals with the design process and the numerical analysis of the results. All designs have been optimized using the stage efficiency as target function. For the design of the 3D stator vanes, the optimization led to an unexpected result: The secondary flow vortex strength increased. However, the secondary flow pattern is rearranged by the 3Ddesigning, leading to a smoother radial exit flow angle distribution. A subsequent reduction of the rotor losses overcompensates the higher stator losses. In order to understand how the 3D vanes affect the stator secondary flow pattern, a detailed analysis of vortex stretching and vortex dissipation is presented in this paper. With this approach, the various impacts of the 3D designs on the secondary flow vortices' strength can be quantified. In addition, the potential theory effect of the selfinduced velocity is introduced here in order to explain the effects of a tangential endwall contouring on the trajectory of the pressure side leg of the horseshoe vortex (HVps). To the best of our knowledge, both approaches are new for the analysis of turbine secondary flows. The impact of the stronger but rearranged stator secondary flow on the rotor secondary loss development is analyzed by means of unsteady simulations. The results show that the rotor secondary flow can be effectively reduced through a proper stator secondary flow pattern. In Part II of this paper, the analysis of extensive experimental results validates and supplements the numerical analysis.
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      Investigation of Nonaxisymmetric Endwall Contouring and Three Dimensional Airfoil Design in a 1.5 Stage Axial Turbine—Part I: Design and Novel Numerical Analysis Method

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    https://yetl.yabesh.ir/yetl1/handle/yetl/159959
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    contributor authorPoehler, Thorsten
    contributor authorNiewoehner, Jens
    contributor authorJeschke, Peter
    contributor authorGuendogdu, Yavuz
    date accessioned2017-05-09T01:24:42Z
    date available2017-05-09T01:24:42Z
    date issued2015
    identifier issn0889-504X
    identifier otherturbo_137_08_081009.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/159959
    description abstractThis paper presents the results of the analysis of different 3D designs for the first stator and the rotor of a 1.5stage turbine test rig. A tangential endwall contouring for the hub and the shroud, a bowed profile stacking, and a combination of those have been designed for the first stator. In addition, a tangential endwall contouring has been designed for the hub of the unshrouded rotor. Part I of this twopart paper deals with the design process and the numerical analysis of the results. All designs have been optimized using the stage efficiency as target function. For the design of the 3D stator vanes, the optimization led to an unexpected result: The secondary flow vortex strength increased. However, the secondary flow pattern is rearranged by the 3Ddesigning, leading to a smoother radial exit flow angle distribution. A subsequent reduction of the rotor losses overcompensates the higher stator losses. In order to understand how the 3D vanes affect the stator secondary flow pattern, a detailed analysis of vortex stretching and vortex dissipation is presented in this paper. With this approach, the various impacts of the 3D designs on the secondary flow vortices' strength can be quantified. In addition, the potential theory effect of the selfinduced velocity is introduced here in order to explain the effects of a tangential endwall contouring on the trajectory of the pressure side leg of the horseshoe vortex (HVps). To the best of our knowledge, both approaches are new for the analysis of turbine secondary flows. The impact of the stronger but rearranged stator secondary flow on the rotor secondary loss development is analyzed by means of unsteady simulations. The results show that the rotor secondary flow can be effectively reduced through a proper stator secondary flow pattern. In Part II of this paper, the analysis of extensive experimental results validates and supplements the numerical analysis.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleInvestigation of Nonaxisymmetric Endwall Contouring and Three Dimensional Airfoil Design in a 1.5 Stage Axial Turbine—Part I: Design and Novel Numerical Analysis Method
    typeJournal Paper
    journal volume137
    journal issue8
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.4029476
    journal fristpage81009
    journal lastpage81009
    identifier eissn1528-8900
    treeJournal of Turbomachinery:;2015:;volume( 137 ):;issue: 008
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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