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    A Comparison Between the Design Point and Near-Stall Performance of an Axial Compressor 

    Source: Journal of Turbomachinery:;1990:;volume( 112 ):;issue: 001:;page 109
    Author(s): N. M. McDougall
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Detailed measurements have been made within an axial compressor operating both at design point and near stall. Rotor tip clearance was found to control the performance of the machine by ...
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    Stall Inception in Axial Compressors 

    Source: Journal of Turbomachinery:;1990:;volume( 112 ):;issue: 001:;page 116
    Author(s): N. M. McDougall; N. A. Cumpsty; T. P. Hynes
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Detailed measurements have been made of the transient stalling process in an axial compressor stage. The stage is of high hub-casing ratio and stall is initiated in the rotor. If the rotor ...
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    Closure to “Discussion of ‘Stall Inception in Axial Compressors’” (1990, ASME J. Turbomach., 112, pp. 124–125) 

    Source: Journal of Turbomachinery:;1990:;volume( 112 ):;issue: 001:;page 124
    Author(s): N. M. McDougall; N. A. Cumpsty; T. P. Hynes
    Publisher: The American Society of Mechanical Engineers (ASME)
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