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    Unsteady Pressure Distributions on Oscillating Airfoils in a Supersonic Cascade 

    Source: Journal of Engineering for Gas Turbines and Power:;1976:;volume( 098 ):;issue: 004:;page 553
    Author(s): M. Kurosaka
    Publisher: The American Society of Mechanical Engineers (ASME)
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    The Oscillatory Boundary Layer Growth Over the Top and Bottom Plates of a Rotating Channel 

    Source: Journal of Fluids Engineering:;1973:;volume( 095 ):;issue: 001:;page 68
    Author(s): M. Kurosaka
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The behavior of the steady boundary layers formed over the top and bottom surfaces of a rotating channel is theoretically investigated. At the leading edge, not surprisingly, the flow behaves ...
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    Discussion: “An Investigation of the Flow Characteristics and of Losses in Radial Nozzle Cascades” (Hashemi, S. G. R., Lemak, R. J., and Owczarek, J. A., 1984, ASME J. Eng. Gas Turbines Power, 106, pp. 502–509) 

    Source: Journal of Engineering for Gas Turbines and Power:;1984:;volume( 106 ):;issue: 002:;page 510
    Author(s): M. Kurosaka
    Publisher: The American Society of Mechanical Engineers (ASME)
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    On the Unsteady Supersonic Cascade With a Subsonic Leading Edge—An Exact First Order Theory—Part 2 

    Source: Journal of Engineering for Gas Turbines and Power:;1974:;volume( 096 ):;issue: 001:;page 23
    Author(s): M. Kurosaka
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Pursuant to Part 1, the analysis of the aerodynamic forces acting on slowly oscillating airfoils in a supersonic cascade with a subsonic leading edge is presented. First the flow field between ...
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    On the Unsteady Supersonic Cascade With a Subsonic Leading Edge—An Exact First Order Theory—Part 1 

    Source: Journal of Engineering for Gas Turbines and Power:;1974:;volume( 096 ):;issue: 001:;page 13
    Author(s): M. Kurosaka
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents, in two parts, the theoretical predictions of the aerodynamic forces acting on slowly oscillating airfoils in a supersonic cascade with a subsonic leading edge. The analysis ...
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    Discussion: “The Unsteady Aerodynamics of a Finite Supersonic Cascade With Subsonic Axial Flow” (Verdon, J. M., 1973, ASME J. Appl. Mech., 40, pp. 667–671) 

    Source: Journal of Applied Mechanics:;1974:;volume( 041 ):;issue: 002:;page 539
    Author(s): M. Kurosaka
    Publisher: The American Society of Mechanical Engineers (ASME)
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