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    Taylor-Görtler Instability of Turbulent Wall Jets Along Concave Surfaces 

    Source: Journal of Applied Mechanics:;1980:;volume( 047 ):;issue: 003:;page 671
    Author(s): R. Kobayashi; N. Fujisawa
    Publisher: The American Society of Mechanical Engineers (ASME)
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    Experimental Study on the Aerodynamic Performance of a Savonius Rotor 

    Source: Journal of Solar Energy Engineering:;1994:;volume( 116 ):;issue: 003:;page 148
    Author(s): Nobuyuki Fujisawa; Futoshi Gotoh
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The aerodynamic performance of a Savonius rotor has been studied by measuring the pressure distributions on the blade surfaces at various rotor angles and tip-speed ratios. It is found that ...
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    A Comparative Study of Navier-Stokes Calculations and Experiments for the Savonius Rotor 

    Source: Journal of Solar Energy Engineering:;1995:;volume( 117 ):;issue: 004:;page 344
    Author(s): Nobuyuki Fujisawa; Katsuya Ishimatsu; Kazuyuki Kage
    Publisher: The American Society of Mechanical Engineers (ASME)
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    Centrifugal Instability of Turbulent Wall Jets Along Strongly Concave Surfaces 

    Source: Journal of Applied Mechanics:;1985:;volume( 052 ):;issue: 002:;page 492
    Author(s): N. Fujisawa; R. Kobayashi; H. Shirai
    Publisher: The American Society of Mechanical Engineers (ASME)
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    Prediction of Multidimensional Deformation Behavior Based on Observed Values 

    Source: International Journal of Geomechanics:;2014:;Volume ( 014 ):;issue: 003
    Author(s): Shin-Ichi; Nishimura; Takayuki; Shuku; Kazunori; Fujisawa
    Publisher: American Society of Civil Engineers
    Abstract: In this study, a method is developed for predicting the future deformation of soft ground, based on measured data. Because it is difficult to predict the deformation behavior of soft ground on the basis of laboratory ...
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    Evolution Process of Diffuser Stall in a Centrifugal Compressor With Vaned Diffuser 

    Source: Journal of Turbomachinery:;2019:;volume( 141 ):;issue: 004:;page 41009
    Author(s): Fujisawa, Nobumichi; Inui, Tetsuya; Ohta, Yutaka
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper describes in detailed flow field in a centrifugal compressor with a vaned diffuser at off design point. Especially, we conducted both the experimental and numerical analysis in order to investigate the evolution ...
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    Method of Determining Locations of Unbalances in Rotating Machines 

    Source: Journal of Mechanical Design:;1982:;volume( 104 ):;issue: 002:;page 290
    Author(s): K. Shiohata; F. Fujisawa; K. Sato
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents a method of determining the locations of unbalances on a rotor when the unbalances occur abruptly during rotor running. The method makes use of journal vibrations, because, ...
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    Unsteady Pre-Stall Behavior in a Centrifugal Compressor With Vaned Diffuser 

    Source: Journal of Turbomachinery:;2023:;volume( 146 ):;issue: 004:;page 41006-1
    Author(s): Suzuki, Yutaro; Fujisawa, Nobumichi; Ohta, Yutaka
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Unsteady pre-stall behavior in a centrifugal compressor with a vaned diffuser was investigated by experimental and numerical analysis. The pre-stall disturbances occurred at a slightly higher flow coefficient at the stall ...
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    Unsteady Flow Mechanism of Impeller Stall Inception in a High-Pressure Ratio Centrifugal Compressor With Bleed Slots 

    Source: Journal of Turbomachinery:;2024:;volume( 147 ):;issue: 007:;page 71013-1
    Author(s): Fujisawa, Nobumichi; Yamamoto, Yuta; Ohta, Yutaka; Ogino, Atsushi; Nakayama, Ryo; Kitamura, Eijiro
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The impeller stall inception in a high-pressure ratio centrifugal compressor with bleed slots was investigated by experiments and unsteady numerical analysis. This study reported that the flow instability of the internal ...
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    Unsteady Flow Structure of Rotating Instability in a 1.5-Stage Axial Compressor 

    Source: Journal of Turbomachinery:;2024:;volume( 147 ):;issue: 004:;page 41010-1
    Author(s): Fujisawa, Nobumichi; Ohta, Yutaka; Yamagami, Mai; Goto, Takashi; Kato, Dai
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The unsteady flow structure of the rotating instability (RI) in a 1.5-stage axial compressor is investigated through experimental and numerical analyses. In the tested compressor, the total pressure rise of the rotor ...
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