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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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    Unsteady Three-Dimensional Flow in a Single-Stage Transonic Fan: Part II—Unsteady Stator Exit Flow Field 

    Source: Journal of Turbomachinery:;1995:;volume( 117 ):;issue: 004:;page 514
    Author(s): M. A. Cherrett; J. D. Bryce; R. B. Ginder
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Detailed unsteady aerodynamic measurements have been taken in a single-stage transonic fan with a very high stage-hub loading. Two-dimensional dynamic yawmeter probes, capable of measuring mean ...
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    Unsteady Three-Dimensional Flow in a Single-Stage Transonic Fan: Part I—Unsteady Rotor Exit Flow Field 

    Source: Journal of Turbomachinery:;1995:;volume( 117 ):;issue: 004:;page 506
    Author(s): M. A. Cherrett; J. D. Bryce; R. B. Ginder
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Detailed unsteady aerodynamic measurements have been taken in a single-stage transonic fan with a very high stator-hub loading. Two-dimensional dynamic yawmeter probes, capable of measuring mean ...
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