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    Evolution Process of Diffuser Stall in a Centrifugal Compressor With Vaned Diffuser 

    Source: Journal of Turbomachinery:;2019:;volume( 141 ):;issue: 004:;page 41009
    Author(s): Fujisawa, Nobumichi; Inui, Tetsuya; Ohta, Yutaka
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper describes in detailed flow field in a centrifugal compressor with a vaned diffuser at off design point. Especially, we conducted both the experimental and numerical analysis in order to investigate the evolution ...
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    Unsteady Pre-Stall Behavior in a Centrifugal Compressor With Vaned Diffuser 

    Source: Journal of Turbomachinery:;2023:;volume( 146 ):;issue: 004:;page 41006-1
    Author(s): Suzuki, Yutaro; Fujisawa, Nobumichi; Ohta, Yutaka
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Unsteady pre-stall behavior in a centrifugal compressor with a vaned diffuser was investigated by experimental and numerical analysis. The pre-stall disturbances occurred at a slightly higher flow coefficient at the stall ...
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    Unsteady Flow Mechanism of Impeller Stall Inception in a High-Pressure Ratio Centrifugal Compressor With Bleed Slots 

    Source: Journal of Turbomachinery:;2024:;volume( 147 ):;issue: 007:;page 71013-1
    Author(s): Fujisawa, Nobumichi; Yamamoto, Yuta; Ohta, Yutaka; Ogino, Atsushi; Nakayama, Ryo; Kitamura, Eijiro
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The impeller stall inception in a high-pressure ratio centrifugal compressor with bleed slots was investigated by experiments and unsteady numerical analysis. This study reported that the flow instability of the internal ...
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    Unsteady Flow Structure of Rotating Instability in a 1.5-Stage Axial Compressor 

    Source: Journal of Turbomachinery:;2024:;volume( 147 ):;issue: 004:;page 41010-1
    Author(s): Fujisawa, Nobumichi; Ohta, Yutaka; Yamagami, Mai; Goto, Takashi; Kato, Dai
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The unsteady flow structure of the rotating instability (RI) in a 1.5-stage axial compressor is investigated through experimental and numerical analyses. In the tested compressor, the total pressure rise of the rotor ...
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