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    A New Stage Stacking Technique for Axial-Flow Compressor Performance Prediction 

    Source: Journal of Engineering for Gas Turbines and Power:;1978:;volume( 100 ):;issue: 004:;page 698
    Author(s): A. R. Howell; W. J. Calvert
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Modern through-flow solutions, with allowances for losses, etc., give good predictions around design conditions. They are more difficult to apply effectively when individual blade rows are operating ...
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    The Design of an Advanced Civil Fan Rotor 

    Source: Journal of Turbomachinery:;1987:;volume( 109 ):;issue: 003:;page 340
    Author(s): R. B. Ginder; W. J. Calvert
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A recent ASME paper by the authors described a quasi-three-dimensional calculation system for transonic compressor blade rows. The system predicts both the internal flow field and the overall ...
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    Detailed Flow Measurements and Predictions for a Three-Stage Transonic Fan 

    Source: Journal of Turbomachinery:;1994:;volume( 116 ):;issue: 002:;page 298
    Author(s): W. J. Calvert; A. W. Stapleton
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Detailed flow measurements were taken at DRA Pyestock on a Rolls-Royce three-stage transonic research fan using advanced laser transit velocimetry and holography techniques to supplement the fixed ...
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