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    The Unstable Behavior of Low and High-Speed Compressors 

    Source: Journal of Turbomachinery:;1994:;volume( 116 ):;issue: 002:;page 194
    Author(s): I. J. Day; C. Freeman
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: By far the greater part of our understanding about stall and surge in axial compressors comes from work on low-speed laboratory machines. As a general rule, these machines do not model the ...
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    High-Speed Compressor Surge With Application to Active Control 

    Source: Journal of Turbomachinery:;1991:;volume( 113 ):;issue: 002:;page 303
    Author(s): A. M. Cargill; C. Freeman
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper discusses the mechanics of surge as observed on the high-speed axial compressors of modern aero-engines. It argues that the initial stage of the instability consists of a high-amplitude ...
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    Stall Inception and Development in an Axial Flow Aeroengine 

    Source: Journal of Turbomachinery:;1994:;volume( 116 ):;issue: 002:;page 216
    Author(s): A. G. Wilson; C. Freeman
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper describes the phenomenon of stall and surge in an axial flow aeroengine using fast response static pressure measurements from the compressor of a Rolls-Royce VIPER engine. It details ...
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    On the Use of Atmospheric Boundary Conditions for Axial-Flow Compressor Stall Simulations 

    Source: Journal of Turbomachinery:;2005:;volume( 127 ):;issue: 002:;page 349
    Author(s): M. Vahdati; C. Freeman; M. Imregun; A. I. Sayma
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper describes a novel way of prescribing computational fluid dynamics (CFD) boundary conditions for axial-flow compressors. The approach is based on extending the standard single passage ...
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    Experiments in Active Control of Stall on an Aeroengine Gas Turbine 

    Source: Journal of Turbomachinery:;1998:;volume( 120 ):;issue: 004:;page 637
    Author(s): C. Freeman; I. J. Day; M. A. Swinbanks; A. G. Wilson
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper describes work carried out between 1989 and 1994 to investigate the application of “Active Stall Control” to a Rolls-Royce Viper turbojet. The results demonstrate that stall control ...
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    Combustion Instability Investigations on the BR710 Jet Engine 

    Source: Journal of Engineering for Gas Turbines and Power:;1998:;volume( 120 ):;issue: 001:;page 34
    Author(s): W. Konrad; F. Kameier; C. Freeman; I. J. Day; N. Brehm
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: During the development of the BR710 jet engine, audible combustor instabilities (termed “rumble”) occurred. Amplitudes measured with test cell microphones were up to 130 dB at around 100 Hz. ...
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