Characteristics of surge and rotating stall in a three-stage axial flow compressor using shock tube

Daisuke Morita, Yutaka Fujita, Yutaka Ota, Eisuke Outa

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

    Abstract

    Transient characteristics as well as unsteady cascade flow fields of a three-stage axial flow compressor with compression plane wave injection from the compressor downstream were experimentally investigated by detail measurements of casing wall pressure fluctuations and unsteady velocity. The main feature of tested compressor is a shock tube facility connected in series to the compressor outlet duct in order to supply a compression plane wave which simulates the sudden rise of the compressor back pressure in a gas turbine system. Research attention is mainly focused on the unsteady behavior of surge and rotating stall coexistence phenomenon, and influence of the compression plane wave injection on the compressor operating conditions. When the compressor is connected to the capacity tank, surge and rotating stall occur simultaneously according to the capacitance increment of the whole compression system. The surge cycle changes irregularly with a throttling of the valve installed just behind the compressor and several different types of surge behaviors are observed. Furthermore, even though the compressor is operating under the stable condition, it goes into surge by injecting the compression plane wave.

    Original languageEnglish
    Title of host publicationASME-JSME-KSME 2011 Joint Fluids Engineering Conference, AJK 2011
    Pages595-602
    Number of pages8
    Volume1
    EditionPARTS A, B, C, D
    DOIs
    Publication statusPublished - 2011
    EventASME-JSME-KSME 2011 Joint Fluids Engineering Conference, AJK 2011 - Hamamatsu
    Duration: 2011 Jul 242011 Jul 29

    Other

    OtherASME-JSME-KSME 2011 Joint Fluids Engineering Conference, AJK 2011
    CityHamamatsu
    Period11/7/2411/7/29

    Fingerprint

    Axial-flow compressors
    Shock tubes
    Compressors
    Surge tanks
    Ducts
    Gas turbines
    Flow fields
    Capacitance

    ASJC Scopus subject areas

    • Fluid Flow and Transfer Processes

    Cite this

    Morita, D., Fujita, Y., Ota, Y., & Outa, E. (2011). Characteristics of surge and rotating stall in a three-stage axial flow compressor using shock tube. In ASME-JSME-KSME 2011 Joint Fluids Engineering Conference, AJK 2011 (PARTS A, B, C, D ed., Vol. 1, pp. 595-602) https://doi.org/10.1115/AJK2011-22015

    Characteristics of surge and rotating stall in a three-stage axial flow compressor using shock tube. / Morita, Daisuke; Fujita, Yutaka; Ota, Yutaka; Outa, Eisuke.

    ASME-JSME-KSME 2011 Joint Fluids Engineering Conference, AJK 2011. Vol. 1 PARTS A, B, C, D. ed. 2011. p. 595-602.

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

    Morita, D, Fujita, Y, Ota, Y & Outa, E 2011, Characteristics of surge and rotating stall in a three-stage axial flow compressor using shock tube. in ASME-JSME-KSME 2011 Joint Fluids Engineering Conference, AJK 2011. PARTS A, B, C, D edn, vol. 1, pp. 595-602, ASME-JSME-KSME 2011 Joint Fluids Engineering Conference, AJK 2011, Hamamatsu, 11/7/24. https://doi.org/10.1115/AJK2011-22015
    Morita D, Fujita Y, Ota Y, Outa E. Characteristics of surge and rotating stall in a three-stage axial flow compressor using shock tube. In ASME-JSME-KSME 2011 Joint Fluids Engineering Conference, AJK 2011. PARTS A, B, C, D ed. Vol. 1. 2011. p. 595-602 https://doi.org/10.1115/AJK2011-22015
    Morita, Daisuke ; Fujita, Yutaka ; Ota, Yutaka ; Outa, Eisuke. / Characteristics of surge and rotating stall in a three-stage axial flow compressor using shock tube. ASME-JSME-KSME 2011 Joint Fluids Engineering Conference, AJK 2011. Vol. 1 PARTS A, B, C, D. ed. 2011. pp. 595-602
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