Aerodynamic Flow Control of Axisymmetric Bluff Body by Coupled Wake Interactions
Author:
Affiliation:
1. Georgia Institute of Technology, Atlanta, Georgia 30332-0405
Funder
Georgia Institute of Technology
Army Research Office
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/am-pdf/10.2514/1.J056782
Reference32 articles.
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3. Dispersion Reduction of a Direct Fire Rocket Using Lateral Pulse Jets
4. Microadaptive Flow Control Applied to a Spinning Projectile
5. Unsteady CFD modeling of micro-adaptive flow control for an axisymmetric body
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