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    Application of Model Order Reduction to Compressor Aeroelastic Models 

    Source: Journal of Engineering for Gas Turbines and Power:;2002:;volume( 124 ):;issue: 002:;page 332
    Author(s): K. Willcox; J. Peraire; J. D. Paduano
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A model order reduction technique that yields low-order models of blade row unsteady aerodynamics is introduced. The technique is applied to linearized unsteady Euler CFD solutions in such a ...
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    Controls and Diagnostics Committee Best 1994 Paper Award: Modeling for Control of Rotating Stall in High-Speed Multistage Axial Compressors 

    Source: Journal of Turbomachinery:;1996:;volume( 118 ):;issue: 001:;page 1
    Author(s): M. R. Feulner; J. D. Paduano; G. J. Hendricks
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Using a two-dimensional compressible flow representation of axial compressor dynamics, a control-theoretic input–output model is derived, which is of general utility in rotating stall/surge active ...
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    Active Stabilization of Surge in an Axicentrifugal Turboshaft Engine 

    Source: Journal of Turbomachinery:;2000:;volume( 122 ):;issue: 003:;page 485
    Author(s): E. B. Nelson; J. D. Paduano; A. H. Epstein
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Active stabilization of surge was implemented on an Allied Signal LTS-101 axicentrifugal gas producer, reducing the surging mass flow by 1 percent, for an operating range increase of 11 percent. ...
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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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    Prestall Behavior of Several High-Speed Compressors 

    Source: Journal of Turbomachinery:;1995:;volume( 117 ):;issue: 001:;page 62
    Author(s): M. Tryfonidis; G. J. Hendricks; O. Etchevers; J. D. Paduano; A. H. Epstein
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: High-speed compressor data immediately prior to rotating stall inception are analyzed and compared to stability theory. New techniques for the detection of small-amplitude rotating waves in the ...
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    Stall Precursor Identification in High-Speed Compressor Stages Using Chaotic Time Series Analysis Methods 

    Source: Journal of Turbomachinery:;1997:;volume( 119 ):;issue: 003:;page 491
    Author(s): M. M. Bright; H. K. Qammar; H. J. Weigl; J. D. Paduano
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents a new technique for precursor identification in high-speed compressors. The technique is a pseudo-correlation integral method referred to as the correlation method. To provide ...
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    Closure to “Discussion of ‘Stall Precursor Identification in High-Speed Compressor Stages Using Chaotic Time Series Analysis Methods’” (1997, ASME J. Turbomach., 119, p. 499) 

    Source: Journal of Turbomachinery:;1997:;volume( 119 ):;issue: 003:;page 499
    Author(s): M. M. Bright; H. K. Qammar; H. J. Weigl; J. D. Paduano
    Publisher: The American Society of Mechanical Engineers (ASME)
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    Tip Clearance Actuation With Magnetic Bearings for High-Speed Compressor Stall Control 

    Source: Journal of Turbomachinery:;2001:;volume( 123 ):;issue: 003:;page 464
    Author(s): Z. S. Spakovszky; R. Larsonneur; M. M. Bright; A. Traxler; J. D. Paduano
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Magnetic bearings are widely used as active suspension devices in rotating machinery, mainly for active vibration control purposes. The concept of active tip-clearance control suggests a new ...
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    Active Control of Rotating Stall in a Low-Speed Axial Compressor 

    Source: Journal of Turbomachinery:;1993:;volume( 115 ):;issue: 001:;page 48
    Author(s): J. D. Paduano; A. H. Epstein; L. Valavani; J. P. Longley; E. M. Greitzer; G. R. Guenette
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The onset of rotating stall has been delayed in a low-speed, single-stage, axial research compressor using active feedback control. Control was implemented using a circumferential array of hot ...
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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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