What is it about?
A series of experiments were performed to study the interaction of a shock wave with the flow over a cylindrical body under a variety of conditions.
Featured Image
Read the Original
This page is a summary of: Planar Shock Wave Interactions on Turbulent Boundary Layer over Cylindrical Body, AIAA Journal, May 2025, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j063616.
You can read the full text:
Contributors
The following have contributed to this page
