Plasma Control of a Turbulent Shock Boundary-Layer Interaction
Author:
Affiliation:
1. RQAC, U.S. Air Force Research Laboratory, Wright-Patterson Air Force Base, 45433-7512 Ohio
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J052248
Reference73 articles.
1. Shock Wave Oscillation Driven by Turbulent Boundary-Layer Fluctuations
2. Experimental evidence for Plotkin model of shock unsteadiness in separated flow
3. Low-order stochastic modelling of low-frequency motions in reflected shock-wave/boundary-layer interactions
4. SBLI control for wings and inlets
5. Review of research on low-profile vortex generators to control boundary-layer separation
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