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    Active Stabilization of Axial Compressors With Circumferential Inlet Distortion 

    Source: Journal of Turbomachinery:;1998:;volume( 120 ):;issue: 003:;page 431
    Author(s): C. M. van Schalkwyk; J. D. Paduano; E. M. Greitzer; A. H. Epstein
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper describes the first experimental validation of transfer function modeling and active stabilization for axial compressors with circumferential inlet distortion. The inlet distortion ...
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    Rotating Stall Control in a High-Speed Stage With Inlet Distortion: Part II—Circumferential Distortion 

    Source: Journal of Turbomachinery:;1999:;volume( 121 ):;issue: 003:;page 517
    Author(s): Z. S. Spakovszky; C. M. van Schalkwyk; H. J. Weigl; K. L. Suder; M. M. Bright; J. D. Paduano
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents the first attempt to stabilize rotating stall in a single-stage transonic axial flow compressor with inlet distortion using active feedback control. The experiments were ...
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    Rotating Stall Control in a High-Speed Stage With Inlet Distortion: Part I—Radial Distortion 

    Source: Journal of Turbomachinery:;1999:;volume( 121 ):;issue: 003:;page 510
    Author(s): Z. S. Spakovszky; C. M. van Schalkwyk; K. L. Suder; M. M. Bright; H. J. Weigl; J. D. Paduano
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents the first attempt to stabilize rotating stall in a single-stage transonic axial flow compressor with inlet distortion using active feedback control. The experiments were ...
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