An Experimental Investigation of Wake Edge
Author:
Affiliation:
1. Northrop Aircraft Company, Hawthorne, California
2. Colorado State University, Fort Collins, Colorado
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference9 articles.
1. Self-Sustained Oscillations of Impinging Free Shear Layers
2. Aerodynamic sound generation due to the interaction of an unsteady wake with a rigid surface
3. Effects of sound on separated flows
4. Low Reynolds Number Flow Between Interrupted Flat Plates
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