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RISThree-Dimensional Relief in Turbomachinery Blading
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: The leading edge region of turbomachinery blading in the vicinity of the endwalls is typically characterized by an abrupt increase in the inlet flow angle and a reduction in total pressure ...
Closure to “Discussion of ‘Three-Dimensional Relief in Turbomachinery Blading’” (1990, ASME J. Turbomach., 112, pp. 596–598)
Publisher: The American Society of Mechanical Engineers (ASME)
Unsteady Flow and Whirl-Inducing Forces in Axial-Flow Compressors: Part I—Experiment
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: An experimental and theoretical investigation has been conducted to evaluate the effects seen in axial-flow compressors when the centerline of the rotor is displaced from the centerline of the ...
Unsteady Flow and Whirl-Inducing Forces in Axial-Flow Compressors: Part II—Analysis
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: An experimental and theoretical investigation was conducted to evaluate the effects seen in axial-flow compressors when the centerline of the rotor becomes displaced from the centerline of the ...