Experimental Investigation of the Application of Microramp Flow Control to an Oblique Shock Interaction
Author:
Affiliation:
1. NASA Glenn Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2009-919
Reference15 articles.
1. 1Anderson B.H., Tinapple, J., Surber, L. "Optimal Control of Shock Wave Turbulent Boundary Layer Interactions using Micro-ArrayActuation", AIAA-2006-3197, June2006.
2. Review of research on low-profile vortex generators to control boundary-layer separation
3. 4Fukuda,M.K.,Hingst,W. G.,Reshotko,E. "ControlofShockWave-BoundaryLayer InteractionsbyBleed inSupersonic Mixed Compression Inlets", NASACR-2595,1975.
4. Separation Criterion for Turbulent Boundary Layers Via Similarity Analysis
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