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    An Explanation for Flow Features of Spike Type Stall Inception in an Axial Compressor Rotor 

    Source: Journal of Turbomachinery:;2013:;volume( 135 ):;issue: 002:;page 21023
    Author(s): Yamada, Kazutoyo; Kikuta, Hiroaki; Iwakiri, Ken; Furukawa, Masato; Gunjishima, Satoshi
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The unsteady behavior and threedimensional flow structure of spiketype stall inception in an axial compressor rotor were investigated by experimental and numerical analyses. Previous studies revealed that the test compressor ...
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    The Effect of Tip Leakage Vortex for Operating Range Enhancement of Centrifugal Compressor 

    Source: Journal of Turbomachinery:;2013:;volume( 135 ):;issue: 005:;page 51020
    Author(s): Tomita, Isao; Ibaraki, Seiichi; Furukawa, Masato; Yamada, Kazutoyo
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Recently, the application of turbochargers is increasing because they are effective in improving fuel consumption of engines. One of the most important turbocharger characteristics is compressor operating range, since it ...
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    Applying Ensemble Kalman Filter to Transonic Flows Through a Two-Dimensional Turbine Cascade 

    Source: Journal of Fluids Engineering:;2021:;volume( 143 ):;issue: 012:;page 0121113-1
    Author(s): Ito, Sasuga; Furukawa, Masato; Yamada, Kazutoyo; Manabe, Kaito
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Turbulence is one of the most important phenomena in fluid dynamics. Large eddy simulation (LES) generally allows us to analyze smaller eddies than when using simulations based on unsteady Reynolds-averaged Navier–Stokes ...
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    Large-Scale Detached-Eddy Simulation Analysis of Stall Inception Process in a Multistage Axial Flow Compressor 

    Source: Journal of Turbomachinery:;2017:;volume( 139 ):;issue: 007:;page 71002
    Author(s): Yamada, Kazutoyo; Furukawa, Masato; Tamura, Yuki; Saito, Seishiro; Matsuoka, Akinori; Nakayama, Kentaro
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper describes the flow mechanisms of rotating stall inception in a multistage axial flow compressor of an actual gas turbine. Large-scale numerical simulations of the unsteady have been conducted. The compressor ...
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