Quasi-Conical Free Interaction in Fin-Induced Shock Wave/Laminar Boundary-Layer Interactions
Author:
Affiliation:
1. University of Texas at Arlington, Arlington, Texas 76019
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J060243
Reference48 articles.
1. FerriA. “Experimental Results with Airfoils Tested in the High-Speed Tunnel at Guidonia,” NACA TM-946, 1940.
2. The Interaction Between Boundary Layer and Shock Waves in Transonic Flow
3. AckeretJ.FeldmannF.RottN. “Investigations of Compression Shocks and Boundary Layers in Gases Moving at High Speed,” NACA TN-1113, 1947.
4. Interactions between shock waves and turbulent boundary layers
5. Review of the physics of swept-shock/boundary layer interactions
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