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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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