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    Blockage Development in a Transonic, Axial Compressor Rotor 

    Source: Journal of Turbomachinery:;1998:;volume( 120 ):;issue: 003:;page 465
    Author(s): K. L. Suder
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A detailed experimental investigation to understand and quantify the development of blockage in the flow field of a transonic, axial flow compressor rotor (NASA Rotor 37) has been undertaken. ...
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    Experimental and Computational Investigation of the Tip Clearance Flow in a Transonic Axial Compressor Rotor 

    Source: Journal of Turbomachinery:;1996:;volume( 118 ):;issue: 002:;page 218
    Author(s): K. L. Suder; M. L. Celestina
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Experimental and computational techniques are used to investigate tip clearance flows in a transonic axial compressor rotor at design and part-speed conditions. Laser anemometer data acquired in ...
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    An Improved Aspirating Probe for Total-Temperature and Total-Pressure Measurements in Compressor Flows 

    Source: Journal of Turbomachinery:;1995:;volume( 117 ):;issue: 004:;page 642
    Author(s): D. E. Van Zante; K. L. Suder; T. H. Okiishi; A. J. Strazisar
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The aspirating probe originally designed by Epstein and Ng at MIT was modified by replacing the two platinum-coated tungsten hot wires normally used with platinum–iridium alloy wires. The resulting ...
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    The Effect of Adding Roughness and Thickness to a Transonic Axial Compressor Rotor 

    Source: Journal of Turbomachinery:;1995:;volume( 117 ):;issue: 004:;page 491
    Author(s): K. L. Suder; W. B. Roberts; R. V. Chima; A. J. Strazisar
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The performance deterioration of a high-speed axial compressor rotor due to surface roughness and airfoil thickness variations is reported. A 0.025 mm (0.001 in.) thick rough coating with a ...
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    Rotating Stall Control in a High-Speed Stage With Inlet Distortion: Part II—Circumferential Distortion 

    Source: Journal of Turbomachinery:;1999:;volume( 121 ):;issue: 003:;page 517
    Author(s): Z. S. Spakovszky; C. M. van Schalkwyk; H. J. Weigl; K. L. Suder; M. M. Bright; J. D. Paduano
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents the first attempt to stabilize rotating stall in a single-stage transonic axial flow compressor with inlet distortion using active feedback control. The experiments were ...
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    Rotating Stall Control in a High-Speed Stage With Inlet Distortion: Part I—Radial Distortion 

    Source: Journal of Turbomachinery:;1999:;volume( 121 ):;issue: 003:;page 510
    Author(s): Z. S. Spakovszky; C. M. van Schalkwyk; K. L. Suder; M. M. Bright; H. J. Weigl; J. D. Paduano
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents the first attempt to stabilize rotating stall in a single-stage transonic axial flow compressor with inlet distortion using active feedback control. The experiments were ...
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