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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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    Quasi-Three-Dimensional Analysis of Cavitation in an Inducer 

    Source: Journal of Fluids Engineering:;2004:;volume( 126 ):;issue: 005:;page 709
    Author(s): Hironori Horiguchi; Souhei Arai; Junichiro Fukutomi; Yoshinobu Tsujimoto; Yoshiyuki Nakase
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A method for the prediction of steady cavitation in turbopumps is proposed on the assumption that the fluid is inviscid and the stream surface is rotationally symmetric. The analysis in the ...
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