Sharp-Fin Induced Shock Wave/Turbulent Boundary Layer Interactions in an Axisymmetric Configuration
Author:
Affiliation:
1. North Carolina State University
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2017-4314
Reference29 articles.
1. Details of a Shock-Separated Turbulent Boundary Layer at a Compression Corner
2. Structure of supersonic turbulent flow past a sharp fin
3. Numerical Prediction of Planar Shock Wave Interaction with a Cylindrical Body
4. Fifty Years of Shock-Wave/Boundary-Layer Interaction Research: What Next?
5. Supersonic and hypersonic shock/boundary-layer interaction database
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1. Flow features of swept shock/turbulent boundary-layer interaction due to a gap beneath a sharp fin;Aerospace Science and Technology;2022-11
2. Investigation of Surface Curvature Effects on Unseparated Fin Shock-Wave/Boundary-Layer Interactions;AIAA Journal;2020-02
3. Fin-Generated Shock Wave/Turbulent Boundary Layer Interactions on a Cylindrical Surface with a Distorted Incoming Boundary Layer;2018 Fluid Dynamics Conference;2018-06-24
4. Gas density field imaging in shock dominated flows using planar laser scattering;Experiments in Fluids;2018-06-05
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