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    A Quasi-Three-Dimensional Blade Surface Boundary Layer Analysis for Rotating Blade Rows 

    Source: Journal of Engineering for Gas Turbines and Power:;1982:;volume( 104 ):;issue: 002:;page 439
    Author(s): W. T. Thompkins; W. J. Usab
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A quasi-three-dimensional, finite difference boundary layer analysis for rotating blade rows has been developed which uses pressure distribution and streamline position data from a three-dimensional ...
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    On the Application of a Linearized Unsteady Potential-Flow Analysis to Fan-Tip Cascades 

    Source: Journal of Turbomachinery:;1986:;volume( 108 ):;issue: 001:;page 59
    Author(s): W. J. Usab; J. M. Verdon
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A linearized potential flow analysis, which accounts for the effects of nonuniform steady flow phenomena on the unsteady response to prescribed blade motions, has been applied to five two-dimensional ...
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    Advances in the Numerical Analysis of Linearized Unsteady Cascade Flows 

    Source: Journal of Turbomachinery:;1991:;volume( 113 ):;issue: 004:;page 633
    Author(s): W. J. Usab; J. M. Verdon
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper describes two new developments in the numerical analysis of linearized unsteady cascade flows, which have been motivated by the need for an accurate analytical procedure for predicting ...
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