Wake of a Compressor Cascade with Tip Gap, Part 1: Mean Flow and Turbulence Structure
Author:
Affiliation:
1. Virginia Polytechnic Institute and State University, Blacksburg, Virginia 24061
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.5270
Reference15 articles.
1. Interaction of Compressor Rotor Blade Wake With Wall Boundary Layer/Vortex in the End-Wall Region
2. Characteristics of the flow in the annulus-wall region of an axial-flow compressor rotor blade passage
3. Investigation of the Tip Clearance Flow Inside and at the Exit of a Compressor Rotor Passage—Part I: Mean Velocity Field
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