Numerical Investigation of Three-dimensional Scramjet Inlet Flowfield with Porous Bleed Models at Mach 5
Author:
Affiliation:
1. Seoul National University
2. Korea Aerospace Research Institute
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2022-0465
Reference13 articles.
1. Microramp Control of Supersonic Oblique Shock-Wave/Boundary-Layer Interactions
2. Impact of Ramped Vanes on Normal Shock Boundary Layer Interaction
3. Boundary-Layer Control for Effective Hypersonic Intake
4. Control of Severe Shock-Wave/Boundary-Layer Interactions in Hypersonic Inlets
5. Shock wave/turbulent boundary layer interaction and its control
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