High-Speed Schlieren Imaging and Hot-wire Characterization of Cylinder-Induced Hypersonic Shock Boundary Layer Interactions
Author:
Affiliation:
1. Texas A&M University
2. University of Tennessee, Tullahoma
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-3703
Reference25 articles.
1. Fifty Years of Shock-Wave/Boundary-Layer Interaction Research: What Next?
2. Shock/Turbulent Boundary Layer Interactions: Review of Recent Work on Sources of Unsteadiness (Invited)
3. Supersonic and hypersonic shock/boundary-layer interaction database
4. A review of the aerothermal characteristics of laminar, transitional, and turbulent shock/shock interaction regions in hypersonic flows
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1. Experimental Investigation of the Hypersonic Boundary-Layer Transition Induced by the Wall-Mounted Cylinder;Journal of Thermophysics and Heat Transfer;2023-10
2. Tunnel Noise Effects on Hypersonic Cylinder-Induced Transitional Shock-Wave/Boundary-Layer Interactions;AIAA Journal;2021-07
3. High-Speed Schlieren Imaging of Cylinder-Induced Hypersonic-Shock-Wave–Boundary-Layer Interactions;AIAA Journal;2020-07
4. Freestream Disturbance Effects on Boundary Layer Instability and Transition on the AFOSR BOLT Geometry;AIAA Scitech 2019 Forum;2019-01-06
5. Cylinder-Induced Hypersonic Transitional Shock Wave Boundary Layer Interactions: Pressure Fluctuations and Thermal Loading;22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference;2018-09-15
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