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    Discussion: “Throughflow Theory for Nonaxisymmetric Turbomachinery Flow: Part I—Formulation” (Dring, R. P., and Oates, G. C., 1990, ASME J. Turbomach., 112, pp. 320–326) 

    Source: Journal of Turbomachinery:;1990:;volume( 112 ):;issue: 003:;page 326
    Author(s): C. Hirsch
    Publisher: The American Society of Mechanical Engineers (ASME)
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    Discussion: “A Quasi-Three-Dimensional Turbomachinery Blade Design System: Parts I and II” (Jennions, I. K., and Stow, P., 1985, ASME J. Eng. Gas Turbines Power, 107, pp. 301–314) 

    Source: Journal of Engineering for Gas Turbines and Power:;1985:;volume( 107 ):;issue: 002:;page 314
    Author(s): C. Hirsch
    Publisher: The American Society of Mechanical Engineers (ASME)
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    Closure to “Discussion of ‘Experimental Study on the Three-Dimensional Flow Within a Compressor Cascade With Tip Clearance: Part II—The Tip Leakage Vortex’” (1993, ASME J. Turbomach., 115, pp. 450–451) 

    Source: Journal of Turbomachinery:;1993:;volume( 115 ):;issue: 003:;page 451
    Author(s): S. Kang; C. Hirsch
    Publisher: The American Society of Mechanical Engineers (ASME)
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    Experimental Study on the Three-Dimensional Flow Within a Compressor Cascade With Tip Clearance: Part I—Velocity and Pressure Fields 

    Source: Journal of Turbomachinery:;1993:;volume( 115 ):;issue: 003:;page 435
    Author(s): S. Kang; C. Hirsch
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Experimental results from a study of the three-dimensional flow in a linear compressor cascade with stationary endwall at design conditions are presented for tip clearance levels of 1.0, 2.0, ...
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    Experimental Study on the Three-Dimensional Flow Within a Compressor Cascade With Tip Clearance: Part II—The Tip Leakage Vortex 

    Source: Journal of Turbomachinery:;1993:;volume( 115 ):;issue: 003:;page 444
    Author(s): S. Kang; C. Hirsch
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An analysis of the experimental data of a linear compressor cascade with tip clearance is presented with special attention to the development of the tip leakage vortex. A method for determining ...
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    Tip Leakage Flow in Linear Compressor Cascade 

    Source: Journal of Turbomachinery:;1994:;volume( 116 ):;issue: 004:;page 657
    Author(s): S. Kang; C. Hirsch
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Tip leakage flow in a linear compressor cascade of NACA 65-1810 profiles is investigated, for tip clearance levels of 1.0, 2.0, and 3.25 percent of chord at design and off-design flow conditions. ...
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    Closure to “Discussion of ‘Numerical Simulation of Three-Dimensional Viscous Flow in a Linear Compressor Cascade With Tip Clearance’” (1996, ASME J. Turbomach., 118, pp. 502–503) 

    Source: Journal of Turbomachinery:;1996:;volume( 118 ):;issue: 003:;page 503
    Author(s): S. Kang; C. Hirsch
    Publisher: The American Society of Mechanical Engineers (ASME)
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    Numerical Simulation of Three-Dimensional Viscous Flow in a Linear Compressor Cascade With Tip Clearance 

    Source: Journal of Turbomachinery:;1996:;volume( 118 ):;issue: 003:;page 492
    Author(s): S. Kang; C. Hirsch
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A Navier–Stokes solver is applied to investigate the three-dimensional viscous flow in a low-speed linear compressor cascade with tip clearance at design and off-design conditions with two different ...
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    Transition Over C4 Leading Edge and Measurement of Intermittency Factor Using PDF of Hot-Wire Signal 

    Source: Journal of Turbomachinery:;1997:;volume( 119 ):;issue: 003:;page 412
    Author(s): B. K. Hazarika; C. Hirsch
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The variation of intermittency factors in the transition region of a C4 leading edge flat plate is measured at three incidence angles in a low-turbulence free stream. During the determination ...
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    Through-Flow Models for Mass and Momentum-Averaged Variables 

    Source: Journal of Turbomachinery:;1987:;volume( 109 ):;issue: 003:;page 362
    Author(s): C. Hirsch; R. P. Dring
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The turbomachinery through-flow equations are reformulated for mass and momentum-averaged quantities. The background of this analysis is the need for an improved assessment of the accuracy of ...
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