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    Performance of Two Transonic Axial Compressor Rotors Incorporating Inlet Counterswirl 

    Source: Journal of Turbomachinery:;1987:;volume( 109 ):;issue: 001:;page 142
    Author(s): C. H. Law; A. J. Wennerstrom
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A single-stage axial-flow compressor which incorporates rotor inlet counterswirl to improve stage performance is discussed. Results for two rotor configurations are presented, including design and ...
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    Low Aspect Ratio Transonic Rotors: Part 1—Baseline Design and Performance 

    Source: Journal of Turbomachinery:;1993:;volume( 115 ):;issue: 002:;page 218
    Author(s): C. H. Law; A. R. Wadia
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The analytical design and experimental test of a single-stage transonic axial-flow compressor are described. This design is the baseline of a compressor design study in which several blade design ...
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    Low Aspect Ratio Transonic Rotors: Part 2—Influence of Location of Maximum Thickness on Transonic Compressor Performance 

    Source: Journal of Turbomachinery:;1993:;volume( 115 ):;issue: 002:;page 226
    Author(s): A. R. Wadia; C. H. Law
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Transonic compressor rotor performance is sensitive to variations in several known design parameters. One such parameter is the chordwise location of maximum thickness. This article reports on ...
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