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    European Report 

    Source: Journal of Fluids Engineering:;1975:;volume( 097 ):;issue: 004:;page 398
    Author(s): J. H. Horlock
    Publisher: The American Society of Mechanical Engineers (ASME)
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    The Rational Efficiency of Power Plants and Their Components 

    Source: Journal of Engineering for Gas Turbines and Power:;1992:;volume( 114 ):;issue: 004:;page 603
    Author(s): J. H. Horlock
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The use of a rational efficiency for a power plant (the work output divided by the maximum possible reversible work output) is well established for conventional and combined plants. However, ...
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    On Entropy Production in Adiabatic Flow in Turbomachines 

    Source: Journal of Fluids Engineering:;1971:;volume( 093 ):;issue: 004:;page 587
    Author(s): J. H. Horlock
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In three recent papers, Smith [1], Marsh [2], and Novak [3] have given general equations for the flow in turbomachines and methods for their solution. Each author has worked from momentum ...
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    European Report: Finite Element Methods in Flow Problems 

    Source: Journal of Fluids Engineering:;1974:;volume( 096 ):;issue: 003:;page 197
    Author(s): J. H. Horlock
    Publisher: The American Society of Mechanical Engineers (ASME)
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    European Report 

    Source: Journal of Fluids Engineering:;1974:;volume( 096 ):;issue: 001:;page 3
    Author(s): J. H. Horlock
    Publisher: The American Society of Mechanical Engineers (ASME)
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    The Use of Circumferentially Varying Stagger Guide Vanes in an Axial Flow Pump or Compressor 

    Source: Journal of Turbomachinery:;1990:;volume( 112 ):;issue: 002:;page 294
    Author(s): J. H. Horlock
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An actuator disk analysis is given of the flow through a guide vane and rotor combination. It is shown that changes in total pressure across the rotor are in general related to circumferential ...
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    Discussion: “A Study of Stall in a Low Hub–Tip Ratio Fan” (Soundranayagam, M., and Elder, R. L., 1993, ASME J. Turbomach., 115, pp. 10–16) 

    Source: Journal of Turbomachinery:;1993:;volume( 115 ):;issue: 001:;page 17
    Author(s): J. H. Horlock
    Publisher: The American Society of Mechanical Engineers (ASME)
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    Flow Through a Repeating Stage in an Axial Compressor: A Reconsideration 

    Source: Journal of Turbomachinery:;2004:;volume( 126 ):;issue: 004:;page 677
    Author(s): J. H. Horlock
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A simple thermo-fluid-dynamic analysis is presented for the ultimate steady flow in a repeating stage of an axial-flow compressor.
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    Fluctuating Lift Forces on Aerofoils Moving Through Transverse and Chordwise Gusts 

    Source: Journal of Fluids Engineering:;1968:;volume( 090 ):;issue: 004:;page 494
    Author(s): J. H. Horlock
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An analysis is given for determining the lift fluctuation on an aerofoil due to a gust parallel to the undisturbed flow. By combining the new analysis with an established theory for “transverse” ...
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    The Determination of End-Wall Blockage in Axial Compressors: A Comparison Between Various Approaches 

    Source: Journal of Turbomachinery:;2000:;volume( 122 ):;issue: 002:;page 218
    Author(s): J. H. Horlock
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The end-wall blockage in axial compressors has been the subject of several investigations over a period of many years. This paper reviews and compares various approaches to determining the ...
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