Effects of Rotation and Blade Incidence on Properties of Turbomachinery Rotor Wake
Author:
Affiliation:
1. The Pennsylvania State University, University Park, Pa.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference10 articles.
1. Characteristics of the Near Wake of a Compressor of a Fan Rotor Blade
2. Mean Velocity and Decay Characteristics of the Near and Far-Wake of a Compressor Rotor Blade of Moderate Loading
3. The experimental verification of a streamline curvature numerical analysis method applied to the flow through an axial flow fan
4. Techniques for Aerodynamic and Turbulence Measurements in Turbomachinery Rotors
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1. Advanced analysis of fan noise measurements supported by theoretical source models;International Journal of Aeroacoustics;2022-04-25
2. Theoretical Acoustic Prediction of the Aerodynamic Interaction for Contra-Rotating Fans;AIAA Journal;2018-05
3. Stereoscopic particle image velocimetry of the flow field in the rotor exit region of a forward-blade centrifugal turbomachine;Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy;2011-12-15
4. Flow Measurement Techniques in Turbomachinery;Springer Handbook of Experimental Fluid Mechanics;2007
5. Decomposition of the spatially filtered and ensemble averaged kinetic energy, the associated fluxes and scaling trends in a rotor wake;Physics of Fluids;2005-08
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