Vortex shedding from yawed cylinders.
Author:
Affiliation:
1. Litton Systems, Inc., Minneapolis, Minn.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference8 articles.
1. INVESTIGATION OF BOUNDARY-LAYER TRANSITION ON SWEPT WINGS AT MACH NUMBERS 2.5 TO 5
2. Hot-wire investigation of the wake behind cylinders at low Reynolds numbers
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