Investigation of Unsteady Boundary Layer Developed on a Rotationally Oscillating Circular Cylinder
Author:
Affiliation:
1. McGill University, Montreal, Quebec H3A 2K6, Canada
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.734
Reference35 articles.
1. Periodic Flow Phenomena
2. Vortex Shedding from Oscillating Bluff Bodies
3. Review—Vortex Shedding Lock-on and Flow Control in Bluff Body Wakes
4. Effect of moving surfaces on the airfoil boundary-layer control
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