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    Further Investigation on Transonic Compressor Stall Margin Enhancement With Stall Precursor Suppressed Casing Treatment

    Source: Journal of Turbomachinery:;2016:;volume( 138 ):;issue: 002::page 21001
    Author:
    Sun, Dakun
    ,
    Nie, Chaoqun
    ,
    Liu, Xiaohua
    ,
    Lin, Feng
    ,
    Sun, Xiaofeng
    DOI: 10.1115/1.4031775
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A kind of casing treatment, named as stall precursorsuppressed (SPS), has been developed recently, which was proved to be able to effectively improve stall margin (SM) without significant efficiency loss in lowspeed axial flow compressors and a transonic compressor rotor. In this paper, the effectiveness of the SPS casing treatment is investigated in a singlestage transonic compressor. Based on an extended stall inception model, the quantitative evaluation of the SM enhancement by the SPS casing treatment is presented for the transonic compressor stage. The model predicts that a 2.5–6.8% of stall margin improvement (SMI), which is defined in terms of mass flow rate at stall inception, can be achieved at the design rotational speed. The experimental results show that the SPS casing treatment can achieve 3.5–9.3% of the SMI at 95% design rotational speed. Due to the fact that the distributions of the total pressure ratio along the spanwise direction are kept the same as those of the solid wall casing at the same mass flow rate, the SPS casing treatments with a small open area ratio and large backchamber enhance the SM without a recognizable efficiency loss and a migration of the pressurerise characteristics. Furthermore, the mechanism of SMI with the SPS casing treatment is investigated in the experiments. In comparison with the solid wall casing, the emergence and the evolution of the stall inception waves are suppressed and the nonlinear development of the stall process is delayed with the SPS casing treatment.
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      Further Investigation on Transonic Compressor Stall Margin Enhancement With Stall Precursor Suppressed Casing Treatment

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    contributor authorSun, Dakun
    contributor authorNie, Chaoqun
    contributor authorLiu, Xiaohua
    contributor authorLin, Feng
    contributor authorSun, Xiaofeng
    date accessioned2017-05-09T01:34:00Z
    date available2017-05-09T01:34:00Z
    date issued2016
    identifier issn0889-504X
    identifier otherturbo_138_02_021001.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/162732
    description abstractA kind of casing treatment, named as stall precursorsuppressed (SPS), has been developed recently, which was proved to be able to effectively improve stall margin (SM) without significant efficiency loss in lowspeed axial flow compressors and a transonic compressor rotor. In this paper, the effectiveness of the SPS casing treatment is investigated in a singlestage transonic compressor. Based on an extended stall inception model, the quantitative evaluation of the SM enhancement by the SPS casing treatment is presented for the transonic compressor stage. The model predicts that a 2.5–6.8% of stall margin improvement (SMI), which is defined in terms of mass flow rate at stall inception, can be achieved at the design rotational speed. The experimental results show that the SPS casing treatment can achieve 3.5–9.3% of the SMI at 95% design rotational speed. Due to the fact that the distributions of the total pressure ratio along the spanwise direction are kept the same as those of the solid wall casing at the same mass flow rate, the SPS casing treatments with a small open area ratio and large backchamber enhance the SM without a recognizable efficiency loss and a migration of the pressurerise characteristics. Furthermore, the mechanism of SMI with the SPS casing treatment is investigated in the experiments. In comparison with the solid wall casing, the emergence and the evolution of the stall inception waves are suppressed and the nonlinear development of the stall process is delayed with the SPS casing treatment.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleFurther Investigation on Transonic Compressor Stall Margin Enhancement With Stall Precursor Suppressed Casing Treatment
    typeJournal Paper
    journal volume138
    journal issue2
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.4031775
    journal fristpage21001
    journal lastpage21001
    identifier eissn1528-8900
    treeJournal of Turbomachinery:;2016:;volume( 138 ):;issue: 002
    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
    yabeshDSpacePersian