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    Performance Improvement of Weis-Fogh Type Ship’s Propulsion Mechanism Using a Wing Restrained by an Elastic Spring 

    Source: Journal of Fluids Engineering:;2010:;volume( 132 ):;issue: 004:;page 41101
    Author(s): Kideok Ro
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This study was conducted in an attempt to improve the hydrodynamic performance of a Weis-Fogh type ship propulsion mechanism by installing a spring to the wing so that the opening angle of ...
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    Numerical Analysis of Unsteady Flow in the Weis-Fogh Mechanism by the 3D Discrete Vortex Method With GRAPE3A 

    Source: Journal of Fluids Engineering:;1997:;volume( 119 ):;issue: 001:;page 96
    Author(s): Kideok Ro; Michihisa Tsutahara
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The three-dimensional flows in the Weis-Fogh mechanism are studied by flow visualization and numerical simulation by a discrete vortex method. In this mechanism, two wings open, touching their ...
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    Ship’s Propulsion Mechanism of Two-Stage “Weis-Fogh” Type 

    Source: Journal of Fluids Engineering:;1994:;volume( 116 ):;issue: 002:;page 278
    Author(s): Michihisa Tsutahara; Kideok Ro; Takeyoshi Kimura
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The dynamic properties of a ship’s two-stage “Weis-Fogh” type propulsion mechanism are experimentally and numerically investigated. In order to study the effects of the interaction of the two ...
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    Numerical Analysis of Unsteady Viscous Flow Through a Weis-Fogh-Type Ship Propulsion Mechanism Using the Advanced Vortex Method 

    Source: Journal of Fluids Engineering:;2006:;volume( 128 ):;issue: 003:;page 481
    Author(s): Kideok Ro; Baoshan Zhu; Hokeun Kang
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The velocity and pressure field of a ship’s Weis-Fogh-type propulsion mechanism are studied in this paper using an advanced vortex method. The wing (NACA0010 airfoil) and channel are approximated ...
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