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    Unsteady Navier–Stokes Simulation of Transonic Cascade Flow Using an Unfactored Implicit Upwind Relaxation Scheme With Inner Iterations 

    Source: Journal of Turbomachinery:;1992:;volume( 114 ):;issue: 003:;page 599
    Author(s): M. Furukawa; T. Nakano; M. Inoue
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An implicit upwind scheme has been developed for Navier–Stokes simulations of unsteady flows in transonic cascades. The two-dimensional, Reynolds-averaged Navier–Stokes equations are discretized in ...
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    A Zonal Approach for Navier–Stokes Computations of Compressible Cascade Flow Fields Using a TVD Finite Volume Method 

    Source: Journal of Turbomachinery:;1991:;volume( 113 ):;issue: 004:;page 573
    Author(s): M. Furukawa; M. Yamasaki; M. Inoue
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A new zonal approach for computation of compressible viscous flows in cascades has been developed. The two-dimensional, Reynolds-averaged Navier–Stokes equations are discretized spatially by a ...
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    Behavior of Three-Dimensional Boundary Layers in a Radial Inflow Turbine Scroll 

    Source: Journal of Turbomachinery:;1994:;volume( 116 ):;issue: 003:;page 446
    Author(s): K. Hara; M. Furukawa; M. Inoue
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A detailed experimental investigation was carried out to examine the three-dimensional boundary layer characteristics in a radial inflow turbine scroll. Some basic flow phenomena and growth of ...
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    Closure to “Discussion of ‘Effects of Stream Surface Inclination on Tip Leakage Flow Fields in Compressor Rotors’” (1998, ASME J. Turbomach., 120, p. 693) 

    Source: Journal of Turbomachinery:;1998:;volume( 120 ):;issue: 004:;page 693
    Author(s): M. Furukawa; K. Saiki; K. Nagayoshi; M. Kuroumaru; M. Inoue
    Publisher: The American Society of Mechanical Engineers (ASME)
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    Effects of Stream Surface Inclination on Tip Leakage Flow Fields in Compressor Rotors 

    Source: Journal of Turbomachinery:;1998:;volume( 120 ):;issue: 004:;page 683
    Author(s): M. Furukawa; K. Saiki; K. Nagayoshi; M. Kuroumaru; M. Inoue
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Experimental and computational results of tip leakage flow fields in a diagonal flow rotor at the design flow rate are compared with those in an axial flow rotor. In the diagonal flow rotor, ...
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    The Role of Tip Leakage Vortex Breakdown in Compressor Rotor Aerodynamics 

    Source: Journal of Turbomachinery:;1999:;volume( 121 ):;issue: 003:;page 469
    Author(s): M. Furukawa; M. Inoue; K. Saiki; K. Yamada
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The breakdown of tip leakage vortex has been investigated on a low-speed axial compressor rotor with moderate blade loading. Effects of the breakdown on the rotor aerodynamics are elucidated ...
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    Propagation of Multiple Short-Length-Scale Stall Cells in an Axial Compressor Rotor 

    Source: Journal of Turbomachinery:;2000:;volume( 122 ):;issue: 001:;page 45
    Author(s): M. Inoue; M. Kuroumaru; T. Tanino; M. Furukawa
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Evolution and structure of multiple stall cells with short-length-scale in an axial compressor rotor have been investigated experimentally. In a low-speed research compressor rotor tested, a ...
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    Comparative Studies on Short and Long Length-Scale Stall Cell Propagating in an Axial Compressor Rotor 

    Source: Journal of Turbomachinery:;2001:;volume( 123 ):;issue: 001:;page 24
    Author(s): M. Inoue; M. Kuroumaru; T. Tanino; S. Yoshida; M. Furukawa
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In a low-speed compressor test rig at Kyushu University, multiple short length-scale stall cells appeared under a mild stall condition and turned into a long length-scale cell under a deep ...
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    Short and Long Length-Scale Disturbances Leading to Rotating Stall in an Axial Compressor Stage With Different Stator/Rotor Gaps 

    Source: Journal of Turbomachinery:;2002:;volume( 124 ):;issue: 003:;page 376
    Author(s): M. Inoue; M. Kuroumaru; S. Yoshida; M. Furukawa
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The transient processes of rotating stall evolution have been investigated experimentally in a low-speed axial compressor stage with three stator-rotor gaps. The pressure traces at eight circumferential ...
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