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    Preparing for the Future: Reducing Gas Turbine Environmental Impact—IGTI Scholar Lecture 

    Source: Journal of Turbomachinery:;2010:;volume( 132 ):;issue: 004:;page 41017
    Author(s): Nicholas A. Cumpsty
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In the long term, the price of fuel will rise and it is now urgent to reduce carbon dioxide emissions to avoid catastrophic climate change. This lecture looks at power plant for electricity ...
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    Interaction of Tip Clearance Flow and Three-Dimensional Separations in Axial Compressors 

    Source: Journal of Turbomachinery:;2007:;volume( 129 ):;issue: 004:;page 679
    Author(s): Semiu A. Gbadebo; Nicholas A. Cumpsty; Tom P. Hynes
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper considers the interaction of tip clearance flow with three-dimensional (3D) separations in the corner region of a compressor cascade. Three-dimensional numerical computations were carried ...
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    Control of Three-Dimensional Separations in Axial Compressors by Tailored Boundary Layer Suction 

    Source: Journal of Turbomachinery:;2008:;volume( 130 ):;issue: 001:;page 11004
    Author(s): Semiu A. Gbadebo; Nicholas A. Cumpsty; Tom P. Hynes
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: One of the important ways of improving turbomachinery compressor performance is to control three-dimensional (3D) separations, which form over the suction surface and end wall corner of the blade ...
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    Influence of Surface Roughness on Three-Dimensional Separation in Axial Compressors 

    Source: Journal of Turbomachinery:;2004:;volume( 126 ):;issue: 004:;page 455
    Author(s): Semiu A. Gbadebo; Nicholas A. Cumpsty; Tom P. Hynes
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Surface roughness on a stator blade was found to have a major effect on the three-dimensional (3D) separation at the hub of a single-stage low-speed axial compressor. The change in the ...
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    Three-Dimensional Separations in Axial Compressors 

    Source: Journal of Turbomachinery:;2005:;volume( 127 ):;issue: 002:;page 331
    Author(s): Semiu A. Gbadebo; Nicholas A. Cumpsty; Tom P. Hynes
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Flow separations in the corner regions of blade passages are common. The separations are three dimensional and have quite different properties from the two-dimensional separations that are ...
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    The Use of Sweep and Dihedral in Multistage Axial Flow Compressor Blading—Part I: University Research and Methods Development 

    Source: Journal of Turbomachinery:;2002:;volume( 124 ):;issue: 004:;page 521
    Author(s): Simon J. Gallimore; John J. Bolger; Nicholas A. Cumpsty; Mark J. Taylor; Peter I. Wright; James M. M. Place
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper describes the introduction of 3-D blade designs into the core compressors for the Rolls-Royce Trent engine with particular emphasis on the use of sweep and dihedral in the rotor ...
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    The Use of Sweep and Dihedral in Multistage Axial Flow Compressor Blading—Part II: Low and High-Speed Designs and Test Verification 

    Source: Journal of Turbomachinery:;2002:;volume( 124 ):;issue: 004:;page 533
    Author(s): Simon J. Gallimore; John J. Bolger; Nicholas A. Cumpsty; Mem. Asme; Mark J. Taylor; Peter I. Wright; James M. M. Place
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper describes the introduction of 3-D blade designs into the core compressors of the Rolls-Royce Trent engine series with particular emphasis on the use of sweep and dihedral in the ...
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