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    Verification of Compressor Data Accuracy by Uncertainty Analysis and Testing Methods 

    Source: Journal of Turbomachinery:;1988:;volume( 110 ):;issue: 002:;page 265
    Author(s): N. D. Poti; D. C. Rabe
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A transonic compressor designed and instrumented by the General Electric Company was recently evaluated during several test programs in the Compressor Research Facility at Wright-Patterson Air ...
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    Characterization of Shock Wave–Endwall Boundary Layer Interactions in a Transonic Compressor Rotor 

    Source: Journal of Turbomachinery:;1988:;volume( 110 ):;issue: 003:;page 386
    Author(s): D. C. Rabe; W. F. O’Brien; A. J. Wennerstrom
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The passage shock wave–endwall boundary layer interaction in a transonic compressor was investigated with a laser transit anemometer. The transonic compressor used in this investigation was developed ...
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    Experimental Investigation of Stepped Tip Gap Effects on the Performance of a Transonic Axial-Flow Compressor Rotor 

    Source: Journal of Turbomachinery:;1998:;volume( 120 ):;issue: 003:;page 477
    Author(s): D. W. Thompson; D. C. Rabe; P. I. King
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The effects of stepped-tip gaps and clearance levels on the performance of a transonic axial-flow compressor rotor were experimentally determined. A two-stage compressor with no inlet guide vanes ...
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    Experimental and Numerical Study of Stall Flutter in a Transonic Low-Aspect Ratio Fan Blisk 

    Source: Journal of Turbomachinery:;2004:;volume( 126 ):;issue: 001:;page 166
    Author(s): A. J. Sanders; D. C. Rabe; K. K. Hassan
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Experiments are performed on a modern design transonic shroudless low-aspect ratio fan blisk that experienced both subsonic/transonic and supersonic stall-side flutter. High-response flush mounted ...
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    Structures and Dynamics Committee Best Paper of 1996 Award: Inlet Distortion Generated Forced Response of a Low-Aspect-Ratio Transonic Fan 

    Source: Journal of Turbomachinery:;1997:;volume( 119 ):;issue: 004:;page 665
    Author(s): S. R. Manwaring; D. C. Rabe; C. B. Lorence; A. R. Wadia
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper describes a portion of an experimental and computational program (ADLARF), which incorporates, for the first time, measurements of all aspects of the forced response of an airfoil ...
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    Effects of Inlet Distortion on the Flow Field in a Transonic Compressor Rotor 

    Source: Journal of Turbomachinery:;1998:;volume( 120 ):;issue: 002:;page 233
    Author(s): C. Hah; D. C. Rabe; T. J. Sullivan; A. R. Wadia
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The effects of circumferential distortions in inlet total pressure on the flow field in a low-aspect-ratio, high-speed, high-pressure-ratio, transonic compressor rotor are investigated in this ...
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