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Verification of Compressor Data Accuracy by Uncertainty Analysis and Testing Methods
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 ...
Characterization of Shock Wave–Endwall Boundary Layer Interactions in a Transonic Compressor Rotor
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 ...
Experimental Investigation of Stepped Tip Gap Effects on the Performance of a Transonic Axial-Flow Compressor Rotor
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 ...
Experimental and Numerical Study of Stall Flutter in a Transonic Low-Aspect Ratio Fan Blisk
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 ...
Structures and Dynamics Committee Best Paper of 1996 Award: Inlet Distortion Generated Forced Response of a Low-Aspect-Ratio Transonic Fan
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 ...
Effects of Inlet Distortion on the Flow Field in a Transonic Compressor Rotor
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 ...