Shock-Wave/Boundary-Layer Interaction in a Large-Aspect-Ratio Test Section
Author:
Affiliation:
1. Saint Louis University, St. Louis, Missouri 63103
2. The Boeing Company, St. Louis, Missouri 63042
3. The Boeing Company, St. Louis, Missouri 63166
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J055592
Reference27 articles.
1. Can Fundamental Shock-Wave/Boundary-Layer Interaction Research be Relevant to Inlet Aerodynamics?
2. A Perspective on Mixed-Compression Inlets and the Use of CFD and Flow Control in the Design Process
3. Passive Device Flow Control for Normal Shock/Boundary Layer Interactions in External Compression Inlets
4. Control of a Shock-Wave/Boundary-Layer Interaction and Subsequent Subsonic Diffuser Using a Combination of Vortex Generators and Bleed
5. Experimental Investigation of Normal Shock Boundary-Layer Interaction with Hybrid Flow Control
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