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    Inlet Distortion Generated Periodic Aerodynamic Rotor Response 

    Source: Journal of Turbomachinery:;1990:;volume( 112 ):;issue: 002:;page 298
    Author(s): S. R. Manwaring; S. Fleeter
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Fundamental inlet distortion-generated rotor blade row unsteady aerodynamics, including the effects of both the detailed aerodynamic forcing function for the first time and steady loading are ...
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    Rotor Blade Unsteady Aerodynamic Gust Response to Inlet Guide Vane Wakes 

    Source: Journal of Turbomachinery:;1993:;volume( 115 ):;issue: 001:;page 197
    Author(s): S. R. Manwaring; S. Fleeter
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A series of experiments is performed in an extensively instrumented axial flow research compressor to investigate the fundamental flow physics of wake-generated periodic rotor blade row unsteady ...
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    Forcing Function Effects on Rotor Periodic Aerodynamic Response 

    Source: Journal of Turbomachinery:;1991:;volume( 113 ):;issue: 002:;page 312
    Author(s): S. R. Manwaring; S. Fleeter
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A series of experiments are performed in an extensively instrumented axial flow research compressor to investigate the effects of different low reduced frequency aerodynamic forcing functions and ...
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    Unsteady Aerodynamics and Gust Response in Compressors and Turbines 

    Source: Journal of Turbomachinery:;1993:;volume( 115 ):;issue: 004:;page 724
    Author(s): S. R. Manwaring; D. C. Wisler
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A comprehensive series of experiments and analyses was performed on compressor and turbine blading to evaluate the ability of current, practical, engineering/analysis models to predict unsteady ...
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    Structures and Dynamics Committee Best Paper of 1996 Award: Inlet Distortion Generated Forced Response of a Low-Aspect-Ratio Transonic Fan 

    Source: Journal of Turbomachinery:;1997:;volume( 119 ):;issue: 004:;page 665
    Author(s): S. R. Manwaring; D. C. Rabe; C. B. Lorence; A. R. Wadia
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper describes a portion of an experimental and computational program (ADLARF), which incorporates, for the first time, measurements of all aspects of the forced response of an airfoil ...
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