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    Discussion: “An Experimental Study of Three-Dimensional Turbulent Boundary Layer and Turbulence Characteristics Inside a Turbomachinery Rotor Passage” (Anand, A. K., and Lakshminarayana, B., 1978, ASME J. Eng. Power, 100, pp. 676–687) 

    Source: Journal of Engineering for Gas Turbines and Power:;1978:;volume( 100 ):;issue: 004:;page 688
    Author(s): P. Kool; Ch. Hirsch
    Publisher: The American Society of Mechanical Engineers (ASME)
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    Measurement of the Three-Dimensional Flow Field Behind an Axial Compressor Stage 

    Source: Journal of Engineering for Gas Turbines and Power:;1977:;volume( 099 ):;issue: 002:;page 168
    Author(s): Ch. Hirsch; P. Kool
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Hot wire instrumentation and a periodic sampling and averaging technique have been used in order to measure the three-dimensional flow field behind a rotor of an axial compressor stage. A ...
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    An Axial Compressor End-Wall Boundary Layer Calculation Method 

    Source: Journal of Engineering for Gas Turbines and Power:;1979:;volume( 101 ):;issue: 002:;page 233
    Author(s): J. De Ruyck; C. Hirsch; P. Kool
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An axial compressor end-wall boundary layer theory which requires the introduction of three-dimensional velocity profile models is described. The method is based on pitch-averaged boundary layer ...
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