Rotor-wake influence on axial-compressor-stator boundary layers
Author:
Affiliation:
1. General Motors Corporation, Indianapolis, Indiana
2. Iowa State University, Ames, Iowa
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.23119
Reference24 articles.
1. An Investigation Into Unsteady Blade Forces in Turbomachines
2. Wake Dispersion in Turbomachines
3. Intra-Stator Transport of Rotor Wakes and Its Effect on Compressor Performance
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1. Unsteady Vane Boundary Layer Response to Rotor–Rotor Interactions in a Multistage Compressor;Journal of Propulsion and Power;2014-03
2. Tip Flow Unsteadiness and Blade Row Interactions for a Low-Speed Compressor Rotor;Journal of Propulsion and Power;2013-11
3. Unsteady Vane Boundary Layer Response to Rotor-Rotor Interactions in an Embedded Compressor Stage;51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2013-01-05
4. Incidence Effects on Wake-Induced Transition on an Axial Compressor Blade;Journal of Propulsion and Power;2000-05
5. M. J. Hartmann Memorial Session Paper: Some Results of NASA-Iowa State University Research on Axial-Flow Pumps;Journal of Turbomachinery;1994-10-01
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