Control of Transitional Shock Boundary Layer Interaction using Surface Morphing
Author:
Affiliation:
1. Ohio State University
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2019-1895
Reference67 articles.
1. Progress in shock wave/boundary layer interactions
2. Some physical aspects of shock wave/boundary layer interactions
3. Fifty Years of Shock-Wave/Boundary-Layer Interaction Research: What Next?
4. Oblique Shock Impinging on a Turbulent Boundary Layer: Low-Frequency Mechanisms.
5. Mechanism of shock unsteadiness in separated shock/boundary-layer interactions
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2. Supersonic Turbulent Boundary-Layer Separation Control Using a Morphing Surface;AIAA Journal;2021-03
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4. A numerical study on controlling flow separation via surface morphing in the form of backward traveling waves;AIAA Aviation 2019 Forum;2019-06-15
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