Active Control of Supersonic Base Flows with Electric Arc Plasma Actuators
Author:
Affiliation:
1. Department of Aerospace Engineering, University of Illinois at Urbana-Champaign, Urbana, Illinois 61801
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J052585
Reference50 articles.
1. Measurement of inflight base-pressure on an artillery-fired projectile
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4. Detached-Eddy Simulation With Compressibility Corrections Applied to a Supersonic Axisymmetric Base Flow
5. Application of the RNG turbulence model to the simulation of axisymmetric supersonic separated base flows
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