Three-Component LDV Measurements in the Wake of a Compressor Cascade With Flow Separation
Author:
Affiliation:
1. Department of Aeronautics and Astronautics, Turbopropulsion Laboratory, Naval Postgraduate School, Monterey, CA 93943
Abstract
Publisher
ASME International
Subject
Mechanical Engineering
Link
http://asmedigitalcollection.asme.org/turbomachinery/article-pdf/doi/10.1115/1.2364883/5582456/011008_1.pdf
Reference15 articles.
1. Three-Dimensional Flows and Loss Reduction in Axial Compressors;Dong;ASME J. Turbomach.
2. Enomoto, S., Hah, C., and Hobson, G. V., 2000, “Numerical and Experimental Investigation of Low Reynolds Number Effects on Laminar Flow Separation and Transition in a Cascade of Compressor Blades,” ASME Paper No. 2000-GT-0276.
3. Secondary Flow and Losses in a Turbine Cascade;Gregory-Smith
4. Secondary Flows and Losses Downstream of a Turbine Cascade;Moore;ASME J. Eng. Gas Turbines Power
5. Reynolds Stresses and Dissipation Mechanisms Downstream of a Turbine Cascade;Moore;ASME J. Turbomach.
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2. Unsteady flow investigation in rotor-stator interface of a radial diffuser pump;Forschung im Ingenieurwesen;2010-10-30
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