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    The Effect of Disk Geometry on Heat Transfer in a Rotating Cavity With a Radial Outflow of Fluid 

    Source: Journal of Engineering for Gas Turbines and Power:;1988:;volume( 110 ):;issue: 001:;page 70
    Author(s): P. R. Farthing; J. M. Owen
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Flow visualization and heat transfer measurements have been made in a cavity comprising two nonplane disks of 762 mm diameter and a peripheral shroud, all of which could be rotated up to ...
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    The Use of Deswirl Nozzles to Reduce the Pressure Drop in a Rotating Cavity With a Radial Inflow 

    Source: Journal of Turbomachinery:;1991:;volume( 113 ):;issue: 001:;page 106
    Author(s): P. R. Farthing; J. W. Chew; J. M. Owen
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A combined theoretical and experimental study is described in which deswirl nozzles were used to reduce the radial pressure drop in a rotating cavity with a radial inflow of air. The nozzles, ...
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    The Use of Fins to Reduce the Pressure Drop in a Rotating Cavity With a Radial Inflow 

    Source: Journal of Turbomachinery:;1989:;volume( 111 ):;issue: 003:;page 349
    Author(s): J. W. Chew; P. R. Farthing; B. Stratford; J. M. Owen
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A combined theoretical and experimental study of radial inflow through a rotating cavity is reported. It is shown that radial fins attached to one of the disks are effective in reducing the ...
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    Rotating Cavity With Axial Throughflow of Cooling Air: Heat Transfer 

    Source: Journal of Turbomachinery:;1992:;volume( 114 ):;issue: 001:;page 229
    Author(s): P. R. Farthing; C. A. Long; J. M. Owen; J. R. Pincombe
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Heat transfer measurements were made in two rotating cavity rigs, in which cooling air passed axially through the center of the disks, for a wide range of flow rates, rotational speeds, and ...
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    Rotating Cavity With Axial Throughflow of Cooling Air: Flow Structure 

    Source: Journal of Turbomachinery:;1992:;volume( 114 ):;issue: 001:;page 237
    Author(s): P. R. Farthing; C. A. Long; J. M. Owen; J. R. Pincombe
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A rotating cavity with an axial throughflow of cooling air is used to provide a simplified model for the flow that occurs between adjacent corotating compressor disks inside a gas turbine ...
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