Wake Dynamics Resulting from Trailing-Edge Spanwise Sinusoidal Perturbation
Author:
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J055048
Reference38 articles.
1. Control of Flow Over a Bluff Body
2. On the Wake and Drag of Bluff Bodies
3. Investigation of the flow behind a two-dimensional model with a blunt trailing edge and fitted with splitter plates
4. The Effect of Base Bleed on the Flow behind a Two-Dimensional Model with a Blunt Trailing Edge
5. A Method for Reducing the Base Drag of Wings with Blunt Trailing Edge
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