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    Experimental and Numerical Verification of an Optimization of a Fast Rotating High-Performance Radial Compressor Impeller

    Source: Journal of Turbomachinery:;2017:;volume( 139 ):;issue: 010::page 101007
    Author:
    Elfert, M.
    ,
    Weber, A.
    ,
    Wittrock, D.
    ,
    Peters, A.
    ,
    Voss, C.
    ,
    Nicke, E.
    DOI: 10.1115/1.4036357
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An optimization has been performed on a well-proven radial compressor design known as the SRV4 impeller (the Krain impeller), which has been extensively tested in the past, using the autoopti tool developed at DLR's Institute of Propulsion Technology. This tool has shown its capability in several tasks, mainly for axial compressor and fan design as well as for turbine design. The optimization package autoopti was applied to the redesign and optimization of a radial compressor stage with a vaneless diffusor. This optimization was performed for the SRV4 compressor geometry without fillets using a relatively coarse structured mesh in combination with wall functions. The impeller geometry deduced by the optimization had to be slightly modified due to manufacturing constraints. In order to filter out the improvements of the new so-called SRV5 radial compressor design, two work packages were conducted: The first one was the manufacturing of the new impeller and its installation on a test rig to investigate the complex flow inside the machine. The aim was, first of all, the evaluation of a classical performance map and the efficiency chart achieved by the new compressor design. The efficiencies realized in the performance chart were enhanced by nearly 1.5%. A 5% higher maximum mass flow rate was measured in agreement with the Reynolds-averaged Navier–Stokes (RANS) simulations during the design process. The second work package comprises the computational fluid dynamics (CFD) analysis. The numerical investigations were conducted with the exact geometries of both the baseline SRV4 as well as the optimized SRV5 impeller including the exact fillet geometries. To enhance the prediction accuracy of pressure ratio and impeller efficiency, the geometries were discretized by high-resolution meshes of approximately 5 × 106 cells. For the blade walls as well as for the hub region, the mesh resolution allows a low-Reynolds approach in order to get high-quality results. The comparison of the numerical predictions and the experimental results shows a very good agreement and confirms the improvement of the compressor performance using the optimization tool autoopti.
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      Experimental and Numerical Verification of an Optimization of a Fast Rotating High-Performance Radial Compressor Impeller

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    https://yetl.yabesh.ir/yetl1/handle/yetl/4236120
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    contributor authorElfert, M.
    contributor authorWeber, A.
    contributor authorWittrock, D.
    contributor authorPeters, A.
    contributor authorVoss, C.
    contributor authorNicke, E.
    date accessioned2017-11-25T07:19:56Z
    date available2017-11-25T07:19:56Z
    date copyright2017/9/5
    date issued2017
    identifier issn0889-504X
    identifier otherturbo_139_10_101007.pdf
    identifier urihttp://138.201.223.254:8080/yetl1/handle/yetl/4236120
    description abstractAn optimization has been performed on a well-proven radial compressor design known as the SRV4 impeller (the Krain impeller), which has been extensively tested in the past, using the autoopti tool developed at DLR's Institute of Propulsion Technology. This tool has shown its capability in several tasks, mainly for axial compressor and fan design as well as for turbine design. The optimization package autoopti was applied to the redesign and optimization of a radial compressor stage with a vaneless diffusor. This optimization was performed for the SRV4 compressor geometry without fillets using a relatively coarse structured mesh in combination with wall functions. The impeller geometry deduced by the optimization had to be slightly modified due to manufacturing constraints. In order to filter out the improvements of the new so-called SRV5 radial compressor design, two work packages were conducted: The first one was the manufacturing of the new impeller and its installation on a test rig to investigate the complex flow inside the machine. The aim was, first of all, the evaluation of a classical performance map and the efficiency chart achieved by the new compressor design. The efficiencies realized in the performance chart were enhanced by nearly 1.5%. A 5% higher maximum mass flow rate was measured in agreement with the Reynolds-averaged Navier–Stokes (RANS) simulations during the design process. The second work package comprises the computational fluid dynamics (CFD) analysis. The numerical investigations were conducted with the exact geometries of both the baseline SRV4 as well as the optimized SRV5 impeller including the exact fillet geometries. To enhance the prediction accuracy of pressure ratio and impeller efficiency, the geometries were discretized by high-resolution meshes of approximately 5 × 106 cells. For the blade walls as well as for the hub region, the mesh resolution allows a low-Reynolds approach in order to get high-quality results. The comparison of the numerical predictions and the experimental results shows a very good agreement and confirms the improvement of the compressor performance using the optimization tool autoopti.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleExperimental and Numerical Verification of an Optimization of a Fast Rotating High-Performance Radial Compressor Impeller
    typeJournal Paper
    journal volume139
    journal issue10
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.4036357
    journal fristpage101007
    journal lastpage101007-9
    treeJournal of Turbomachinery:;2017:;volume( 139 ):;issue: 010
    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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