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    Japanese Report 

    Source: Journal of Fluids Engineering:;1975:;volume( 097 ):;issue: 004:;page 399
    Author(s): Yasutoshi Senoo
    Publisher: The American Society of Mechanical Engineers (ASME)
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    Japanese Report: An Advanced Design Method for Pump/Turbines 

    Source: Journal of Fluids Engineering:;1974:;volume( 096 ):;issue: 004:;page 310
    Author(s): Yasutoshi Senoo
    Publisher: The American Society of Mechanical Engineers (ASME)
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    Foreign Report 

    Source: Journal of Fluids Engineering:;1980:;volume( 102 ):;issue: 004:;page 397
    Author(s): Yasutoshi Senoo
    Publisher: The American Society of Mechanical Engineers (ASME)
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    Influence of Inlet Flow Conditions and Geometries of Centrifugal Vaneless Diffusers on Critical Flow Angle for Reverse Flow 

    Source: Journal of Fluids Engineering:;1977:;volume( 099 ):;issue: 001:;page 98
    Author(s): Yasutoshi Senoo; Yoshifumi Kinoshita
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The authors’ preceding analysis on centrifugal vaneless diffusers is used to examine the influences of diffuser geometries and of flow inlet conditions on the critical flow angle for reverse ...
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    Behavior of Severely Asymmetric Flow in a Vaneless Diffuser 

    Source: Journal of Engineering for Gas Turbines and Power:;1975:;volume( 097 ):;issue: 003:;page 375
    Author(s): Yasutoshi Senoo; Masahiro Ishida
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: There is controversy about the mechanism of decay of the asymmetric flow in the vaneless diffuser of centrifugal blowers. In order to clearly observe the behavior of asymmetric flow, every ...
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    The Influence of Tip Clearance on Stall Limits of a Rectilinear Cascade of Compressor Blades 

    Source: Journal of Fluids Engineering:;1961:;volume( 083 ):;issue: 003:;page 371
    Author(s): Ghassan Khabbaz; Yasutoshi Senoo
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An experimental study of the influence of tip clearance on the stall limits of compressor blades was conducted on a rectilinear cascade. By using the mirror and image technique the end wall ...
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    A Blade Theory of an Impeller With an Arbitrary Surface of Revolution 

    Source: Journal of Engineering for Gas Turbines and Power:;1971:;volume( 093 ):;issue: 004:;page 454
    Author(s): Yasutoshi Senoo; Yoshiyuki Nakase
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In this report a method of analyzing subsonic inviscid flow between blades on a stream surface of revolution of a turbomachine, which may be an axial, a radial, or a mixed-flow type, is ...
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    An Analysis of Flow Through a Mixed Flow Impeller 

    Source: Journal of Engineering for Gas Turbines and Power:;1972:;volume( 094 ):;issue: 001:;page 43
    Author(s): Yasutoshi Senoo; Yoshiyuki Nakase
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In this report, a method of analyzing steady, three-dimensional, subsonic, nonviscous flow through a turbomachine with arbitrary hub and shroud shapes and with a finite number of blades is ...
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    Rotating Wakes in Vaneless Diffusers 

    Source: Journal of Fluids Engineering:;1960:;volume( 082 ):;issue: 003:;page 563
    Author(s): Robert C. Dean; Yasutoshi Senoo
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Experimental investigations have shown that the flow discharged from a centrifugal compressor or pump impeller into a diffuser is often unsteady and axially asymmetric. A theory based upon a ...
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    Asymmetric Flow in Vaneless Diffusers of Centrifugal Blowers 

    Source: Journal of Fluids Engineering:;1977:;volume( 099 ):;issue: 001:;page 104
    Author(s): Yasutoshi Senoo; Masahiro Ishida; Yoshifumi Kinoshita
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An analytical method is proposed to evaluate the flow behavior in vaneless diffusers assuming that the flow is not symmetric between the walls. In the analysis momentum integral equations are ...
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