Experimental Investigation of Normal Shock Boundary-Layer Interaction with Hybrid Flow Control
Author:
Affiliation:
1. NASA Glenn Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2012-48
Reference6 articles.
1. 1Anderson, B. H., Tinapple, J., Surber, L. "Optimal Control of Shock Wave Turbulent Boundary Layer Interactions using Micro-ArrayActuation,"AIAA-2006-3197,2006.
2. 3Galbraith, M. C., Orkwis, P. D., Benek, J. A. "Multi-Row Micro-Ramp Actuators for Shock Wave Boundary-Layer Interaction Control," AIAAPaper2009-321,2009.
3. 5Herges,T.,Kroeker,E.,Elliott,G.,Dutton,C."Micro-RampFlowControlofNormalShock/Boundary-Layer Interactions," AIAAPaper 2009-920,2009.
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