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    Further Developments in the Aerodynamic Analysis of Unsteady Supersonic Cascades—Part 2: Aerodynamic Response Predictions 

    Source: Journal of Engineering for Gas Turbines and Power:;1977:;volume( 099 ):;issue: 004:;page 517
    Author(s): J. M. Verdon
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper is the second of a two-part report on a theoretical analysis of the aerodynamic response to an oscillating supersonic cascade in subsonic axial flow. Supersonic resonance criteria ...
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    Further Developments in the Aerodynamic Analysis of Unsteady Supersonic Cascades—Part 1: The Unsteady Pressure Field 

    Source: Journal of Engineering for Gas Turbines and Power:;1977:;volume( 099 ):;issue: 004:;page 509
    Author(s): J. M. Verdon
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents, in two parts, a theoretical investigation of the aerodynamic response produced by an oscillating cascade placed in a supersonic stream with subsonic axial velocity component. ...
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    The Unsteady Aerodynamics of a Finite Supersonic Cascade With Subsonic Axial Flow 

    Source: Journal of Applied Mechanics:;1973:;volume( 040 ):;issue: 003:;page 667
    Author(s): J. M. Verdon
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A method is presented for determining the unsteady flow field and the aerodynamic response which occurs when a finite oscillating cascade is placed in a supersonic stream, which has a subsonic ...
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    Response of a Single-Degree-of-Freedom System to Modulated White Noise 

    Source: Journal of Applied Mechanics:;1973:;volume( 040 ):;issue: 001:;page 296
    Author(s): J. M. Verdon
    Publisher: The American Society of Mechanical Engineers (ASME)
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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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    Validation of a Nonlinear Unsteady Aerodynamic Simulator for Vibrating Blade Rows 

    Source: Journal of Turbomachinery:;1998:;volume( 120 ):;issue: 001:;page 112
    Author(s): T. C. Ayer; J. M. Verdon
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A time-accurate Euler/Navier–Stokes analysis is applied to predict unsteady subsonic and transonic flows through a vibrating cascade. The intent is to validate this nonlinear analysis along with ...
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    Numerical Simulations of Unsteady Cascade Flows 

    Source: Journal of Turbomachinery:;1994:;volume( 116 ):;issue: 004:;page 665
    Author(s): D. J. Dorney; J. M. Verdon
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A time-accurate Navier–Stokes analysis is needed for understanding the relative importance of nonlinear and viscous effects on the unsteady flows associated with turbomachinery blade vibration and ...
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    A Nonlinear Numerical Simulator for Three-Dimensional Flows Through Vibrating Blade Rows 

    Source: Journal of Turbomachinery:;1999:;volume( 121 ):;issue: 002:;page 348
    Author(s): H. A. Chuang; J. M. Verdon
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The three-dimensional, multistage, unsteady, turbomachinery analysis, TURBO, has been extended to predict the aeroelastic response of a blade row operating within a cylindrical annular duct. In ...
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    A Linearized Unsteady Aerodynamic Analysis for Real Blade Supersonic Cascades 

    Source: Journal of Turbomachinery:;1997:;volume( 119 ):;issue: 004:;page 686
    Author(s): M. D. Montgomery; S. Fleeter; J. M. Verdon
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The prediction capabilities of a linearized unsteady potential analysis have been extended to include supersonic cascades with subsonic axial flow. The numerical analysis of this type of flow ...
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