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    Dynamic Mode Decomposition Analysis of the Unsteady Flow in a Centrifugal Compressor Volute

    Source: Journal of Aerospace Engineering:;2019:;Volume ( 032 ):;issue: 001
    Author:
    Xiaocheng Zhu; Chenxing Hu; Xiaojian Yang; Zhaohui Du
    DOI: 10.1061/(ASCE)AS.1943-5525.0000951
    Publisher: American Society of Civil Engineers
    Abstract: The volute has a significant effect on the unsteady characteristics of the centrifugal compressor. The flow in the centrifugal compressor volute is unsteady and complex. In this paper, the dynamic mode decomposition (DMD) method is used to extract the most dominant flow structures in a turbocharger centrifugal compressor volute under design and mild surge conditions. Large-scale perturbations with synchronic frequencies corresponding to the shaft rotating speed are correctly captured. In addition, nonsynchronic frequency and flow mode in the volute are illustrated. The results show that the high-frequency unsteady flow mode corresponding to the main and splitter blade passing becomes weak in the volute. The development of the unsteady flow mode at the mild surge condition is vividly shown by the reconstruction. Two clear cells in the vaneless diffuser occur under the influence of the volute.
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      Dynamic Mode Decomposition Analysis of the Unsteady Flow in a Centrifugal Compressor Volute

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    contributor authorXiaocheng Zhu; Chenxing Hu; Xiaojian Yang; Zhaohui Du
    date accessioned2019-03-10T12:02:29Z
    date available2019-03-10T12:02:29Z
    date issued2019
    identifier other%28ASCE%29AS.1943-5525.0000951.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4254728
    description abstractThe volute has a significant effect on the unsteady characteristics of the centrifugal compressor. The flow in the centrifugal compressor volute is unsteady and complex. In this paper, the dynamic mode decomposition (DMD) method is used to extract the most dominant flow structures in a turbocharger centrifugal compressor volute under design and mild surge conditions. Large-scale perturbations with synchronic frequencies corresponding to the shaft rotating speed are correctly captured. In addition, nonsynchronic frequency and flow mode in the volute are illustrated. The results show that the high-frequency unsteady flow mode corresponding to the main and splitter blade passing becomes weak in the volute. The development of the unsteady flow mode at the mild surge condition is vividly shown by the reconstruction. Two clear cells in the vaneless diffuser occur under the influence of the volute.
    publisherAmerican Society of Civil Engineers
    titleDynamic Mode Decomposition Analysis of the Unsteady Flow in a Centrifugal Compressor Volute
    typeJournal Paper
    journal volume32
    journal issue1
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)AS.1943-5525.0000951
    page04018136
    treeJournal of Aerospace Engineering:;2019:;Volume ( 032 ):;issue: 001
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
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