Cylindrical and conical upstream influence regimes of 3D shock/turbulent boundary layer interactions
Author:
Affiliation:
1. Princeton University, Princeton, NJ
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1982-987
Reference19 articles.
1. Analysis of Two-Dimensional Interactions Between Shock Waves and Boundary Layers
2. Investigation of Three-Dimensional Shock/Boundary-Layer Interactions at Swept Compression Corners
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1. Investigations on the complex flows induced by dual-swept/dual-ramp wedges in supersonic flows;Scientific Reports;2020-06-12
2. Supersonic and hypersonic shock/boundary-layer interaction database;AIAA Journal;1994-07
3. Supersonic viscous-inviscid interaction of a swept compression ramp with a turbulent boundary layer;18th Fluid Dynamics and Plasmadynamics and Lasers Conference;1985-07-16
4. Simulation of blunt-fin-induced shock-wave and turbulent boundary-layer interaction;Journal of Fluid Mechanics;1985-05
5. Conical similarity of shock/boundary layer interactions generated byswept fins;16th Fluid and Plasmadynamics Conference;1983-07-12
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