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    An Investigation of the Effect of Cascade Area Ratios on Transonic Compressor Performance 

    Source: Journal of Turbomachinery:;1996:;volume( 118 ):;issue: 004:;page 760
    Author(s): A. R. Wadia; W. W. Copenhaver
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Transonic compressor rotor performance is highly sensitive to variations in cascade area ratios. This paper reports on the design, experimental evaluation, and three-dimensional viscous analysis ...
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    Flow Field Unsteadiness in the Tip Region of a Transonic Compressor Rotor 

    Source: Journal of Fluids Engineering:;1997:;volume( 119 ):;issue: 001:;page 122
    Author(s): S. L. Puterbaugh; W. W. Copenhaver
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An experimental investigation concerning tip flow field unsteadiness was performed for a high-performance, state-of-the-art transonic compressor rotor. Casing-mounted high frequency response pressure ...
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    Closure to “Discussion of ‘Three-Dimensional Flow Phenomena in a Transonic, High-Throughflow, Axial-Flow Compressor Stage’” (1993, ASME J. Turbomach., 115, p. 248) 

    Source: Journal of Turbomachinery:;1993:;volume( 115 ):;issue: 002:;page 248
    Author(s): W. W. Copenhaver; C. Hah; S. L. Puterbaugh
    Publisher: The American Society of Mechanical Engineers (ASME)
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    Three-Dimensional Flow Phenomena in a Transonic, High-Throughflow, Axial-Flow Compressor Stage 

    Source: Journal of Turbomachinery:;1993:;volume( 115 ):;issue: 002:;page 240
    Author(s): W. W. Copenhaver; C. Hah; S. L. Puterbaugh
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A detailed aerodynamic study of a transonic, high-throughflow, single-stage compressor is presented. The compressor stage was comprised of a low-aspect-ratio rotor combined alternately with two ...
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    A Shock Loss Model for Supersonic Compressor Cascades 

    Source: Journal of Turbomachinery:;1999:;volume( 121 ):;issue: 001:;page 28
    Author(s): G. S. Bloch; W. F. O’Brien; W. W. Copenhaver
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Loss models used in compression system performance prediction codes are often developed from the study of two-dimensional cascades. In this paper, compressible fluid mechanics has been applied ...
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    A Three-Dimensional Shock Loss Model Applied to an Aft-Swept, Transonic Compressor Rotor 

    Source: Journal of Turbomachinery:;1997:;volume( 119 ):;issue: 003:;page 452
    Author(s): S. L. Puterbaugh; C. Hah; A. J. Wennerstrom; W. W. Copenhaver
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An analysis of the effectiveness of a three-dimensional shock loss model used in transonic compressor rotor design is presented. The model was used during the design of an aft-swept, transonic ...
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    The Effect of Tip Clearance on a Swept Transonic Compressor Rotor 

    Source: Journal of Turbomachinery:;1996:;volume( 118 ):;issue: 002:;page 230
    Author(s): W. W. Copenhaver; C. Hah; A. R. Wadia; E. R. Mayhew
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An experimental and numerical investigation of detailed tip clearance flow structures and their effects on the aerodynamic performance of a modern low-aspect-ratio, high-throughflow, axial transonic ...
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