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    Three-Dimensional Boundary-Layer Computation on the Stationary End-Walls of Centrifugal Turbomachinery 

    Source: Journal of Fluids Engineering:;1976:;volume( 098 ):;issue: 003:;page 431
    Author(s): W. R. Davis
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An integral entrainment computation technique is presented for the three-dimensional boundary-layer growth on the stationary end-walls of centrifugal turbomachinery. The analytical model assumes ...
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    A Comparison of the Matrix and Streamline Curvature Methods of Axial Flow Turbomachinery Analysis, From a User’s Point of View 

    Source: Journal of Engineering for Gas Turbines and Power:;1975:;volume( 097 ):;issue: 004:;page 549
    Author(s): W. R. Davis; D. A. J. Millar
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In recent years two general methods for flow analysis in turbomachinery have been developed, one generally called the Streamline Curvature Method, the other the Matrix Through-Flow Method. Both ...
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    Suppressing the Infrared Signatures of Marine Gas Turbines 

    Source: Journal of Engineering for Gas Turbines and Power:;1989:;volume( 111 ):;issue: 001:;page 123
    Author(s): A. M. Birk; W. R. Davis
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The exhaust plumes and visible areas of the engine exhaust ducting associated with marine gas turbines are major sources of infrared (IR) radiation on ships. These high-radiance sources make ...
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