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    Optimization of a U Bend for Minimal Pressure Loss in Internal Cooling Channels—Part I: Numerical Method

    Source: Journal of Turbomachinery:;2013:;volume( 135 ):;issue: 005::page 51015
    Author:
    Verstraete, Tom
    ,
    Coletti, Filippo
    ,
    Bulle, Jأ©rأ©my
    ,
    Vanderwielen, Timothأ©e
    ,
    Arts, Tony
    DOI: 10.1115/1.4023030
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This twopart paper addresses the design of a Ubend for serpentine internal cooling channels optimized for minimal pressure loss. The total pressure loss for the flow in a Ubend is a critical design parameter, as it augments the pressure required at the inlet of the cooling system, resulting in a lower global efficiency. In this first part of the paper, the design methodology of the cooling channel is presented. The minimization of the total pressure loss is achieved by means of a numerical optimization method that uses a metamodelassisted differential evolution algorithm in combination with an incompressible Navier–Stokes solver. The profiles of the internal and external side of the bend are parameterized using piecewise Bezier curves. This allows for a wide variety of shapes, respecting the manufacturability constraints of the design. The pressure loss is computed by the Navier–Stokes solver, which is based on a twoequation turbulence model and is available from the open source software OpenFOAM. The numerical method predicts an improvement of 36% in total pressure drop with respect to a circular Ubend, mainly due to the reduction of the separated flow region along the internal side of the bend. The resulting design is subjected to experimental validation, presented in Part II of the paper.
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      Optimization of a U Bend for Minimal Pressure Loss in Internal Cooling Channels—Part I: Numerical Method

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    contributor authorVerstraete, Tom
    contributor authorColetti, Filippo
    contributor authorBulle, Jأ©rأ©my
    contributor authorVanderwielen, Timothأ©e
    contributor authorArts, Tony
    date accessioned2017-05-09T01:03:49Z
    date available2017-05-09T01:03:49Z
    date issued2013
    identifier issn0889-504X
    identifier otherturb_135_05_051015.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/153496
    description abstractThis twopart paper addresses the design of a Ubend for serpentine internal cooling channels optimized for minimal pressure loss. The total pressure loss for the flow in a Ubend is a critical design parameter, as it augments the pressure required at the inlet of the cooling system, resulting in a lower global efficiency. In this first part of the paper, the design methodology of the cooling channel is presented. The minimization of the total pressure loss is achieved by means of a numerical optimization method that uses a metamodelassisted differential evolution algorithm in combination with an incompressible Navier–Stokes solver. The profiles of the internal and external side of the bend are parameterized using piecewise Bezier curves. This allows for a wide variety of shapes, respecting the manufacturability constraints of the design. The pressure loss is computed by the Navier–Stokes solver, which is based on a twoequation turbulence model and is available from the open source software OpenFOAM. The numerical method predicts an improvement of 36% in total pressure drop with respect to a circular Ubend, mainly due to the reduction of the separated flow region along the internal side of the bend. The resulting design is subjected to experimental validation, presented in Part II of the paper.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleOptimization of a U Bend for Minimal Pressure Loss in Internal Cooling Channels—Part I: Numerical Method
    typeJournal Paper
    journal volume135
    journal issue5
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.4023030
    journal fristpage51015
    journal lastpage51015
    identifier eissn1528-8900
    treeJournal of Turbomachinery:;2013:;volume( 135 ):;issue: 005
    contenttypeFulltext
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