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    Comparison of Test Results Obtained on Plane and Annular, Fixed or Rotating Supersonic Blade Cascades 

    Source: Journal of Engineering for Gas Turbines and Power:;1975:;volume( 097 ):;issue: 002:;page 245
    Author(s): J. Paulon; J. Reboux; R. Sovrano
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Results of an experimental research on the comparison of flow patterns in linear and annular, fixed and rotating supersonic blade cascades are presented. The fixed plane cascade and the fixed ...
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    Theoretical and Experimental Determination of Pressure Losses in a Single-Stage Axial Flow Compressor 

    Source: Journal of Engineering for Gas Turbines and Power:;1970:;volume( 092 ):;issue: 004:;page 407
    Author(s): Y. Le Bot; J. Paulon; P. Belaygue
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A single, isolated, test axial compressor rotor in a constant section annular duct is used for determination of off-design pressure losses. The results obtained are interpreted by means of loss ...
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    Influence of Unsteady Effects on the Measurements in a Transonic Axial Compressor 

    Source: Journal of Turbomachinery:;1992:;volume( 114 ):;issue: 003:;page 510
    Author(s): J. Paulon; Zhifang Zhang; Pingfang Jia; Jingfei Meng
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Interaction phenomena between rotor and stator are unavoidable in advanced compressors and their effects increase with the performance of the turbomachines. Until now, it was not possible to ...
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