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    An Analysis on the Flow in a Casing Induced by a Rotating Disk Using a Four-Layer Flow Model 

    Source: Journal of Fluids Engineering:;1976:;volume( 098 ):;issue: 002:;page 192
    Author(s): Y. Senoo; H. Hayami
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An analytical study has been made to clarify the details of the flow between a rotating disk and a stationary casing side-wall with and without an axisymmetric inward through-flow. The flow ...
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    Application of a Low-Solidity Cascade Diffuser to Transonic Centrifugal Compressor 

    Source: Journal of Turbomachinery:;1990:;volume( 112 ):;issue: 001:;page 25
    Author(s): H. Hayami; Y. Senoo; K. Utsunomiya
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Low-solidity circular cascades, conformally transformed from high-stagger linear cascades of double-circular-arc vanes with solidity 0.69, were used as a part of the diffuser system of a transonic ...
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    Flow in the Inducer of a Centrifugal Compressor Measured With a Laser Velocimeter 

    Source: Journal of Engineering for Gas Turbines and Power:;1985:;volume( 107 ):;issue: 002:;page 534
    Author(s): H. Hayami; H. Ueki; Y. Senoo
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The flow field in the inducer of a high-pressure-ratio centrifugal compressor has been measured with a laser-2-focus velocimeter (L2FV) at two flow rates that were on each side of the apparent ...
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    Experimental Study on Flow in a Supersonic Centrifugal Impeller 

    Source: Journal of Engineering for Gas Turbines and Power:;1979:;volume( 101 ):;issue: 001:;page 32
    Author(s): Y. Senoo; H. Hayami; Y. Kinoshita; H. Yamasaki
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An impeller of a supersonic centrifugal compressor was tested in a casing without a diffuser so that the flow range was not limited by the diffuser. Regarding the impeller, emphasis was placed ...
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    Effects of Tip Clearance of Nozzle Vanes on Performance of Radial Turbine Rotor 

    Source: Journal of Turbomachinery:;1990:;volume( 112 ):;issue: 001:;page 58
    Author(s): H. Hayami; Y. Senoo; Y. I. Hyun; M. Yamaguchi
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In radial turbines with variable nozzles, the flow downstream of the nozzles could be distorted by the leakage flow through the tip clearance of the upstream nozzle vanes. To investigate the ...
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    Blade Loading and Shock Wave in a Transonic Circular Cascade Diffuser 

    Source: Journal of Turbomachinery:;1993:;volume( 115 ):;issue: 003:;page 560
    Author(s): H. Hayami; M. Sawae; T. Nakamura; N. Kawaguchi
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A low-solidity circular cascade, conformally transformed from a high-stagger linear cascade of double-circular-arc vanes with solidity 0.69, was tested as a part of diffuser systems of a transonic ...
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